From 70e2925e994baf4d15740468d95fe608f2573e9f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 17:44:12 -0500 Subject: [PATCH 001/151] Update README.md --- spacecraft/README.md | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/README.md b/spacecraft/README.md index 9c364522..ead2952f 100644 --- a/spacecraft/README.md +++ b/spacecraft/README.md @@ -1,6 +1,6 @@ These files are for FoxTelem, the AMSAT software by Chris Thompson AC3CZ/G0KLA for decoding and displaying Fox-1 series CubeSat telemetry. -To use FoxTelem with the CubeSat Simulator, you will need to download the latest version number listed in this directory. +To use FoxTelem with the CubeSat Simulator, you will need to download the 1.09m version from: https://www.g0kla.com/foxtelem/downloads/test/ From eb630a80aef24d18693053edd6609d97bc4c296b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 19:19:50 -0500 Subject: [PATCH 002/151] partial add of STEM Payload sensors, missing rotation linear changes --- afsk/main.c | 11 +++++++++++ 1 file changed, 11 insertions(+) diff --git a/afsk/main.c b/afsk/main.c index 9765560b..d0ff0274 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1113,7 +1113,14 @@ if (payload == ON) encodeA(b, 0 + head_offset, batt_a_v); encodeB(b, 1 + head_offset, batt_b_v); encodeA(b, 3 + head_offset, batt_c_v); + + encodeB(b, 4 + head_offset,negXv); // Xaccel + encodeA(b, 6 + head_offset,posYv); //Yaccel + encodeB(b, 7 + head_offset,negYv); //Zaccel + encodeA(b, 9 + head_offset, battCurr); + + encodeB(b, 10 + head_offset,negYv); // Temp if (mode == FSK) { @@ -1149,6 +1156,10 @@ if (payload == ON) } encodeA(b, 30 + head_offset,PSUVoltage); + + encodeA(b, 33 + head_offset,PSUVoltage); // Pressure + encodeB(b, 34 + head_offset,PSUVoltage); // Altitude + encodeB(b, 46 + head_offset,PSUCurrent); encodeA(b, 36 + head_offset, RXTemperature); From e5ddfcc13ce7828c25c7e1a07019cf91aa75e930 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:13:45 -0500 Subject: [PATCH 003/151] Added Temp, Pressure, Altitude from STEM Payload Board --- .../FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 12 ++++++------ 1 file changed, 6 insertions(+), 6 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 0f68efd1..78cedb54 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -2,11 +2,11 @@ 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,3,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) -3,RT,BATT_A_T,12,C,8,NONE,0,0,3,Temperature A,Battery pair A temperature -4,RT,BATT_B_T,12,C,8,NONE,0,0,3,Temperature B,Battery pair B temperature -5,RT,BATT_C_T,12,C,8,NONE,0,0,3,Temperature C,Battery pair C temperature +3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,6,4,3,Acceleration,Acceleration around X Axis +4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis +5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,3,2,3,Current,Total Battery DC current -7,RT,BATTBoardTemperature,12,C,8,NONE,0,0,3,Board Temp,Battery Card Temperature +7,RT,Temperature,12,C,8,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature 8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,6,2,3,Voltage,+X Panel 9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,9,2,3,Voltage,-X Panel 10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,7,2,3,Voltage,+YPanel @@ -21,8 +21,8 @@ 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells -22,RT,TXPACurrent,12,mA,10,NONE,1,0,3,PA Current,Transmit power amplifier current -23,RT,TXTemperature,12,C,7,NONE,1,0,3,TX Temperature,Transmitter card temperature +22,RT,Pressure,12,bar,10,Experiments,5,2,4,3,Pressure,STEM Payload Sensor Pressure +23,RT,Altitude,12,m,7,Experiments,5,2,5,3,Altitude,STEM Payload Sensor Altitude 24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature 25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU From 1d055bcc500de68dceb833d2681b00206345f5ff Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:16:13 -0500 Subject: [PATCH 004/151] Update CubeSatSim_rttelemetryFM.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 78cedb54..a89730f4 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -21,8 +21,8 @@ 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells -22,RT,Pressure,12,bar,10,Experiments,5,2,4,3,Pressure,STEM Payload Sensor Pressure -23,RT,Altitude,12,m,7,Experiments,5,2,5,3,Altitude,STEM Payload Sensor Altitude +22,RT,Pressure,12,bar,10,Experiments,5,2,4,Pressure,STEM Payload Sensor Pressure +23,RT,Altitude,12,m,7,Experiments,5,2,5,Altitude,STEM Payload Sensor Altitude 24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature 25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU From bc4c7f9415d641f70795590e991e46afb17ff033 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:17:48 -0500 Subject: [PATCH 005/151] Update CubeSatSim_rttelemetryFM.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index a89730f4..afef8781 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -21,8 +21,8 @@ 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells -22,RT,Pressure,12,bar,10,Experiments,5,2,4,Pressure,STEM Payload Sensor Pressure -23,RT,Altitude,12,m,7,Experiments,5,2,5,Altitude,STEM Payload Sensor Altitude +22,RT,Pressure,12,bar,10,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure +23,RT,Altitude,12,m,7,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude 24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature 25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU From bc583484414e06ccfb6316dfa08bb71a9a8cfd8b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:25:05 -0500 Subject: [PATCH 006/151] fixed new variables for pressure, temp, alt, and accel --- afsk/main.c | 13 +++++++------ 1 file changed, 7 insertions(+), 6 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index d0ff0274..176ef44e 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -884,6 +884,7 @@ int get_tlm_fox() { // int xAngularVelocity = (-0.69)*(-10)*(-10) + 45.3 * (-10) + 2078, yAngularVelocity = (-0.69)*(-6)*(-6) + 45.3 * (-6) + 2078, zAngularVelocity = (-0.69)*(6)*(6) + 45.3 * (6) + 2078; // XAxisAngularVelocity int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; + int xAccel = 2048, yAccel = 2048, zAccel = 2048, temp = 2240, pressure = 1000, altitude = 1000; short int buffer_test[bufLen]; int buffSize; @@ -1114,13 +1115,13 @@ if (payload == ON) encodeB(b, 1 + head_offset, batt_b_v); encodeA(b, 3 + head_offset, batt_c_v); - encodeB(b, 4 + head_offset,negXv); // Xaccel - encodeA(b, 6 + head_offset,posYv); //Yaccel - encodeB(b, 7 + head_offset,negYv); //Zaccel + encodeB(b, 4 + head_offset,xAccel); // Xaccel + encodeA(b, 6 + head_offset,yAccel); //Yaccel + encodeB(b, 7 + head_offset,zAccel); //Zaccel encodeA(b, 9 + head_offset, battCurr); - encodeB(b, 10 + head_offset,negYv); // Temp + encodeB(b, 10 + head_offset,temp); // Temp if (mode == FSK) { @@ -1157,8 +1158,8 @@ if (payload == ON) encodeA(b, 30 + head_offset,PSUVoltage); - encodeA(b, 33 + head_offset,PSUVoltage); // Pressure - encodeB(b, 34 + head_offset,PSUVoltage); // Altitude + encodeA(b, 33 + head_offset,pressure); // Pressure + encodeB(b, 34 + head_offset,altitude); // Altitude encodeB(b, 46 + head_offset,PSUCurrent); From 98d6d220401cf3ec5cf0386c40fb4761ff582631 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:34:40 -0500 Subject: [PATCH 007/151] added back in linear angular velocity --- afsk/main.c | 13 +++++++++---- 1 file changed, 9 insertions(+), 4 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 176ef44e..88e86639 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -882,7 +882,8 @@ int get_tlm_fox() { int posXi = 0, negXi = 0, posYi = 0, negYi = 0, posZi = 0, negZi = 0; int head_offset = 0; // int xAngularVelocity = (-0.69)*(-10)*(-10) + 45.3 * (-10) + 2078, yAngularVelocity = (-0.69)*(-6)*(-6) + 45.3 * (-6) + 2078, zAngularVelocity = (-0.69)*(6)*(6) + 45.3 * (6) + 2078; // XAxisAngularVelocity - int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0 +// int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0 + int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; int xAccel = 2048, yAccel = 2048, zAccel = 2048, temp = 2240, pressure = 1000, altitude = 1000; @@ -1106,9 +1107,13 @@ if (payload == ON) printf("gyroZ %f \n", gyroZ); } - xAngularVelocity = (-0.69)*(gyroX)*(gyroX) + 45.3 * (gyroX) + 2078; - yAngularVelocity = (-0.69)*(gyroY)*(gyroY) + 45.3 * (gyroY) + 2078; - zAngularVelocity = (-0.69)*(gyroZ)*(gyroZ) + 45.3 * (gyroZ) + 2078; +// xAngularVelocity = (-0.69)*(gyroX)*(gyroX) + 45.3 * (gyroX) + 2078; +// yAngularVelocity = (-0.69)*(gyroY)*(gyroY) + 45.3 * (gyroY) + 2078; +// zAngularVelocity = (-0.69)*(gyroZ)*(gyroZ) + 45.3 * (gyroZ) + 2078; + + xAngularVelocity = 1 * (gyroX) + 2048; + yAngularVelocity = 1 * (gyroY) + 2048; + zAngularVelocity = 1 * (gyroZ) + 2048; } encodeA(b, 0 + head_offset, batt_a_v); From 02d6e9e990518d83c8cca3b0614721cf66d64d8a Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:43:32 -0500 Subject: [PATCH 008/151] Added extra Sensor 1 and 2 --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index afef8781..3c036da6 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -29,9 +29,9 @@ 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis -30,RT,EXP4Temperature,12,C,7,NONE,5,0,0,EXP4 Temperature,Not used +30,RT,Sensor1,12,raw,7,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current -32,RT,IHUDiagnosticData,32,-,18,NONE,2,7,0,Diagnostic Info,Diagnostic Data on IHU Performance +32,RT,Sensor2,12,raw,7,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status 34,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 35,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used From d45036d1950038b9f58ca8894c0fa1eb496e8286 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:48:42 -0500 Subject: [PATCH 009/151] added 20 octets unused --- .../CubeSatSim_rttelemetryFM.csv | 21 ++++++++++--------- 1 file changed, 11 insertions(+), 10 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 3c036da6..19e5089d 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -32,14 +32,15 @@ 30,RT,Sensor1,12,raw,7,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current 32,RT,Sensor2,12,raw,7,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status -34,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -35,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -36,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -37,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator -38,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator -39,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator -40,RT,NumberofGroundCommandedTLMResets,4,-,1,Computer,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -41,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status -42,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status +33,RT,Unused,20,na,7,NONE,0,0,0,Unused,Unused +34,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status +35,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +36,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +37,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +38,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator +39,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator +40,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator +41,RT,NumberofGroundCommandedTLMResets,4,-,1,Computer,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +42,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status +43,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status 43,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE From 2b633f5bf9406cb145c3526a4e467d868d7d92a4 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:50:09 -0500 Subject: [PATCH 010/151] Update CubeSatSim_rttelemetryFM.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 19e5089d..30da0f13 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -43,4 +43,4 @@ 41,RT,NumberofGroundCommandedTLMResets,4,-,1,Computer,2,6,0,Ground Resets,Number of times command stations reset stored telemetry 42,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status 43,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status -43,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE +44,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE From 0c4d7eca8dc5e72d34eb5299291e3bbde358cdd5 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:51:49 -0500 Subject: [PATCH 011/151] fixed number of rows to 45 --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 30da0f13..2729972e 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,4 +1,4 @@ -44,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +45,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,3,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) From c935da2f131857f0c673e0cd80d213e9968dc605 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 22:57:26 -0500 Subject: [PATCH 012/151] removed ground resets --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 2729972e..b2369adb 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -40,7 +40,7 @@ 38,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator 39,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator 40,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator -41,RT,NumberofGroundCommandedTLMResets,4,-,1,Computer,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +41,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry 42,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status 43,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status 44,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE From a130788bf9415d6b232839059649f610939f1532 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 23:01:49 -0500 Subject: [PATCH 013/151] added Sensor 1 and Sensor 2 conversions --- spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv | 2 ++ 1 file changed, 2 insertions(+) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv index ab54325a..a3f2008e 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv @@ -4,3 +4,5 @@ cubesatsim_ina219_current,-2048,1,0,0,0,0,Converts positive and negative current cubesatsim_temperature,0,0.1,0,0,0,0,Converts temperature of Pi cubesatsim_rotation,-2048,1,0,0,0,0,Converts positive and negative dps rotation cubesatsim_acceleration,-2048,0.01,0,0,0,0,Converts positive and negative g acceleration +cubesatsim_sensor1,0,1,0,0,0,0,Integer conversion of Sensor 1 +cubesatsim_sensor2,-2048,1,0,0,0,0,Integer conversion of Sensor 2 From dd83aa05311f03a7271d15edc2dabaacf000d7db Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 23:06:11 -0500 Subject: [PATCH 014/151] added altitude, pressure, and sensor 1 and 2 conversions --- spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv | 2 ++ 1 file changed, 2 insertions(+) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv index a3f2008e..087a4af3 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv @@ -4,5 +4,7 @@ cubesatsim_ina219_current,-2048,1,0,0,0,0,Converts positive and negative current cubesatsim_temperature,0,0.1,0,0,0,0,Converts temperature of Pi cubesatsim_rotation,-2048,1,0,0,0,0,Converts positive and negative dps rotation cubesatsim_acceleration,-2048,0.01,0,0,0,0,Converts positive and negative g acceleration +cubesatsim_altitude,0,0.1,0,0,0,0,Converts altitude +cubesatsim_pressure,0,1,0,0,0,0,Converts pressure cubesatsim_sensor1,0,1,0,0,0,0,Integer conversion of Sensor 1 cubesatsim_sensor2,-2048,1,0,0,0,0,Integer conversion of Sensor 2 From 522d07b5e86fb7196b76aaf113fafedc43671f14 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 23:07:35 -0500 Subject: [PATCH 015/151] fixed conversions for sensors --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 10 +++++----- 1 file changed, 5 insertions(+), 5 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index b2369adb..1602cf7d 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -6,7 +6,7 @@ 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis 5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,3,2,3,Current,Total Battery DC current -7,RT,Temperature,12,C,8,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature +7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature 8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,6,2,3,Voltage,+X Panel 9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,9,2,3,Voltage,-X Panel 10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,7,2,3,Voltage,+YPanel @@ -21,17 +21,17 @@ 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells -22,RT,Pressure,12,bar,10,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure -23,RT,Altitude,12,m,7,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude +22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure +23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude 24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature 25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis -30,RT,Sensor1,12,raw,7,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1 +30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current -32,RT,Sensor2,12,raw,7,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 +32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Unused,20,na,7,NONE,0,0,0,Unused,Unused 34,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status 35,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used From 0d69a8e72ee708a83e081145d14326d924ded67a Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 23:12:39 -0500 Subject: [PATCH 016/151] added sensor1 and sensor 2 values --- afsk/main.c | 10 +++++++--- 1 file changed, 7 insertions(+), 3 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 88e86639..6f3535b0 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -885,7 +885,8 @@ int get_tlm_fox() { // int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0 int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; - int xAccel = 2048, yAccel = 2048, zAccel = 2048, temp = 2240, pressure = 1000, altitude = 1000; + int xAccel = 2048, yAccel = 2048, zAccel = 2048, temp = 224, pressure = 1000, altitude = 1000; + int sensor1 = 0, sensor2 = 2048; short int buffer_test[bufLen]; int buffSize; @@ -1166,14 +1167,17 @@ if (payload == ON) encodeA(b, 33 + head_offset,pressure); // Pressure encodeB(b, 34 + head_offset,altitude); // Altitude - encodeB(b, 46 + head_offset,PSUCurrent); - encodeA(b, 36 + head_offset, RXTemperature); encodeA(b, 39 + head_offset, IHUcpuTemp); encodeB(b, 40 + head_offset, xAngularVelocity); encodeA(b, 42 + head_offset, yAngularVelocity); encodeB(b, 43 + head_offset, zAngularVelocity); + + encodeA(b, 45 + head_offset, sensor1); + encodeB(b, 46 + head_offset,PSUCurrent); + encodeA(b, 47 + head_offset, sensor2); + encodeB(b, 51 + head_offset, STEMBoardFailure); From 53c5ff2edfc1ad3d1ad3c4e00c22a67aad12cb04 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Wed, 25 Nov 2020 23:14:55 -0500 Subject: [PATCH 017/151] fixed sensor2 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 6f3535b0..0db1befd 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1176,7 +1176,7 @@ if (payload == ON) encodeA(b, 45 + head_offset, sensor1); encodeB(b, 46 + head_offset,PSUCurrent); - encodeA(b, 47 + head_offset, sensor2); + encodeA(b, 48 + head_offset, sensor2); encodeB(b, 51 + head_offset, STEMBoardFailure); From caa2ddb61373acd9006666d37e965f9ecffbdeb9 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 08:34:05 -0500 Subject: [PATCH 018/151] started updating for sensor fields --- .../FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv | 12 ++++++------ 1 file changed, 6 insertions(+), 6 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv index 495413f1..0831221c 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv @@ -2,11 +2,11 @@ 0,realTime,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,realTime,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) -3,realTime,battAtemp,12,C,8,NONE,4,4,3,Temperature A,Battery pair A temperature -4,realTime,battBtemp,12,C,8,NONE,4,5,3,Temperature B,Battery pair B temperature -5,realTime,battCtemp,12,C,8,NONE,4,6,3,Temperature C,Battery pair C temperature +3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,6,4,3,Acceleration,Acceleration around X Axis +4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis +5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis 6,realTime,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current -7,realTime,battCardTemp,12,C,8,NONE,4,8,3,Board Temp,Battery Card Temperature +7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature 8,realTime,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage 9,realTime,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage 10,realTime,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage @@ -21,8 +21,8 @@ 19,realTime,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current 20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,2,3,Board Voltage,Power Supply Voltage 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,realTime,TxPAi,12,mA,38,Radio,1,2,3,PA Current,Transmit power amplifier current -23,realTime,TxTemp,12,C,37,Radio,1,1,3,TX Temperature,Transmitter card temperature +22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure +23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude 24,realTime,FwdPower,12,mW,40,Radio,1,4,3,Fwd Power,Receiver card temperature 25,realTime,rssi,12,dBm,14,Radio,1,3,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU From bff66ada5d920fa004bae09222e297244538faf2 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 09:08:03 -0500 Subject: [PATCH 019/151] changed RT to realTime and turned off Software values --- .../cubesatsim_psk_rttelemetry.csv | 16 ++++++++-------- 1 file changed, 8 insertions(+), 8 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv index 0831221c..9253c06c 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv @@ -2,11 +2,11 @@ 0,realTime,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,realTime,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) -3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,6,4,3,Acceleration,Acceleration around X Axis -4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis -5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis +3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,6,4,3,Acceleration,Acceleration around X Axis +4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis +5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis 6,realTime,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current -7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature +7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature 8,realTime,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage 9,realTime,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage 10,realTime,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage @@ -21,8 +21,8 @@ 19,realTime,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current 20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,2,3,Board Voltage,Power Supply Voltage 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure -23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude +22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure +23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude 24,realTime,FwdPower,12,mW,40,Radio,1,4,3,Fwd Power,Receiver card temperature 25,realTime,rssi,12,dBm,14,Radio,1,3,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU @@ -41,7 +41,7 @@ 39,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR 40,realTime,LtVGACtl,12,V,42,Radio,1,6,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused -42,realTime,IHUdiagData,32,-,18,Computer Software,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance 43,realTime,expFailure0,1,-,17,Experiments,6,2,0,Vanderbilt Radiation,Vanderbilt University Vulcan Experiment Indicator 44,realTime,expFailure1,1,-,17,Experiments,6,3,0,Exp 1,Experiment 1 Failure Indicator 45,realTime,expFailure2,1,-,17,Experiments,6,4,0,Exp 2,Experiment 2 Failure Indicator @@ -54,7 +54,7 @@ 52,realTime,TxAntDeploy,2,-,16,Radio,1,7,0,TX Antenna,70cm Antenna status 53,realTime,I2CfailureRF,1,-,17,Computer Hardware,2,5,0,RF I2C,RF I2C Bus failure indicator 54,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler -55,realTime,wodSize,8,000s,36,Computer Software,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +55,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds 56,realTime,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information 57,realTime,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset 58,realTime,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset From dc813d3645d6dc946436a88d9837026f8dc55908 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 09:12:43 -0500 Subject: [PATCH 020/151] Fixed Radio numbering --- spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv index 9253c06c..36765bd9 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv @@ -23,15 +23,15 @@ 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude -24,realTime,FwdPower,12,mW,40,Radio,1,4,3,Fwd Power,Receiver card temperature -25,realTime,rssi,12,dBm,14,Radio,1,3,3,RSSI,Received Signal Strength Indication +24,realTime,FwdPower,12,mW,40,Radio,1,2,3,Fwd Power,Receiver card temperature +25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,realTime,Exp4Temp,12,C,7,Experiments,6,1,3,EXP4 Temp,Experiment 4 card temperature 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current -32,realTime,ReflectedPwr,12,mW,41,Radio,1,5,3,Ref Power,Reflected Power from the Transmit Antenna +32,realTime,ReflectedPwr,12,mW,41,Radio,1,3,3,Ref Power,Reflected Power from the Transmit Antenna 33,realTime,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V 34,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 35,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V @@ -39,7 +39,7 @@ 37,realTime,rf6,12,-,0,NONE,0,0,0,None,None 38,realTime,rf7,12,-,0,NONE,0,0,0,None,None 39,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR -40,realTime,LtVGACtl,12,V,42,Radio,1,6,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +40,realTime,LtVGACtl,12,V,42,Radio,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused 42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance 43,realTime,expFailure0,1,-,17,Experiments,6,2,0,Vanderbilt Radiation,Vanderbilt University Vulcan Experiment Indicator From 620e3d31e1a817cdd326c5201810aa14746f4cbd Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 09:14:13 -0500 Subject: [PATCH 021/151] more Radio --- spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv index 36765bd9..61203393 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv @@ -50,8 +50,8 @@ 48,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 49,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 50,realTime,TLMresets,4,-,1,Computer Hardware,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -51,realTime,RxAntDeploy,1,-,16,Radio,1,8,0,RX Antenna,2m Antenna status -52,realTime,TxAntDeploy,2,-,16,Radio,1,7,0,TX Antenna,70cm Antenna status +51,realTime,RxAntDeploy,1,-,16,Radio,1,6,0,RX Antenna,2m Antenna status +52,realTime,TxAntDeploy,2,-,16,Radio,1,5,0,TX Antenna,70cm Antenna status 53,realTime,I2CfailureRF,1,-,17,Computer Hardware,2,5,0,RF I2C,RF I2C Bus failure indicator 54,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler 55,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds From 9a6a79ba5706870dd6ad5ea17ee6c8142378a882 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:20:15 -0500 Subject: [PATCH 022/151] Created from FOX1E file --- .../CubeSatSim_PSK_maxtelemetry.csv | 52 +++++++++++++++++++ 1 file changed, 52 insertions(+) create mode 100644 spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv new file mode 100644 index 00000000..74f9a66e --- /dev/null +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv @@ -0,0 +1,52 @@ +51,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,MAX,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,MAX,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,MAX,BATT_C_V,12,V,4,NONE,4,3,3,Cell A + B + C,Battery pairs A+B+C voltage (0-5.0V scale) +3,MAX,battAtemp,12,C,8,NONE,4,4,3,Temperature A,Battery pair A temperature +4,MAX,battBtemp,12,C,8,NONE,4,5,3,Temperature B,Battery pair B temperature +5,MAX,battCtemp,12,C,8,NONE,4,6,3,Temperature C,Battery pair C temperature +6,MAX,battCurr,12,mA,9,NONE,4,7,3,Current,Total Battery DC current +7,MAX,battCardTemp,12,C,8,NONE,4,8,3,Board Temp,Battery Card Temperature +8,MAX,posXv,12,V,23,NONE,8,1,3,Voltage,+X solar Panel voltage +9,MAX,posYv,12,V,23,NONE,9,1,3,Voltage,+Y solar Panel voltage +10,MAX,posZv,12,V,23,NONE,10,1,3,Voltage,+Z solar Panel voltage +11,MAX,negXv,12,V,23,NONE,11,1,3,Voltage,-X solar Panel voltage +12,MAX,negYv,12,V,23,NONE,12,1,3,Voltage,-Y solar Panel voltage +13,MAX,negZv,12,V,23,NONE,13,1,3,Voltage,-Z solar Panel voltage +14,MAX,posXt,12,C,24,NONE,8,2,3,Temp,+X solar Panel temperature +15,MAX,posYt,12,C,24,NONE,9,2,3,Temp,+Y solar Panel temperature +16,MAX,posZt,12,C,24,NONE,10,2,3,Temp,+Z solar Panel temperature +17,MAX,negXt,12,C,24,NONE,11,2,3,Temp,-X solar Panel temperature +18,MAX,negYt,12,C,24,NONE,12,2,3,Temp,-Y solar Panel temperature +19,MAX,negZt,12,C,24,NONE,13,2,3,Temp,-Z solar Panel temperature +20,MAX,PSUTemp,12,C,8,NONE,5,2,3,Board Temp,Power Supply Card Temperature +21,MAX,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MAX,TxPAi,12,mA,38,NONE,1,2,3,PA Current,Transmit power amplifier current +23,MAX,TxTemp,12,C,37,NONE,1,1,3,TX Temperature,Transmitter card temperature +24,MAX,FwdPower,12,mW,40,NONE,1,4,3,Fwd Power,Receiver card temperature +25,MAX,rssi,12,dBm,14,NONE,1,3,3,RSSI,Received Signal Strength Indication +26,MAX,IHUcpuTemp,12,C,15,NONE,2,1,3,Temperature,Internal Temperature of IHU +27,MAX,SatelliteXAxisAngularVelocity,12,dps,13,NONE,8,3,3,Rotation,Angular Veolcity around X Axis +28,MAX,SatelliteYAxisAngularVelocity,12,dps,13,NONE,9,3,3,Rotation,Angular Veolcity around Y Axis +29,MAX,SatelliteZAxisAngularVelocity,12,dps,13,NONE,10,3,3,Rotation,Angular Veolcity around Z Axis +30,MAX,Exp4Temp,12,C,7,NONE,6,1,3,EXP4 Temp,Experiment 4 card temperature +31,MAX,PSUCurrent,12,mA,22,NONE,5,1,3,Current,Power Supply DC Current +32,MAX,ReflectedPwr,12,mW,41,NONE,1,5,3,Ref Power,Reflected Power from the Transmit Antenna +33,MAX,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V +34,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +35,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +36,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +37,MAX,rf6,12,-,0,NONE,0,0,0,None,None +38,MAX,rf7,12,-,0,NONE,0,0,0,None,None +39,MAX,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +40,MAX,LtVGACtl,12,V,42,NONE,1,6,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +41,MAX,pad,4,-,34,NONE,0,0,0,None,Unused +42,MAX,IHUhardError,32,-,19,NONE,2,7,0,IHU Hard Error Data,Reason for last reset +43,MAX,maxTimestampReset,16,s,1,NONE,0,0,0,MAX Timestamp Reset Count,Timestamp of last max change +44,MAX,maxTimestampUptime,25,s,1,NONE,0,0,0,MAX Timestamp Uptime,Timestamp of last max change +45,MAX,SafeModeIndication,1,-,21,NONE,3,4,0,Safe Mode,In safe mode? +46,MAX,AutoSafeModeActive,1,-,21,NONE,3,5,0,Auto Safe Mode,In Autosafe mode? +47,MAX,AutoSafeModeAllowed,1,-,21,NONE,3,6,0,Auto Safe Allowed,Autosafe enabled? +48,MAX,ScienceModeActive,1,-,21,NONE,3,7,0,Science Mode,In Science Mode? +49,MAX,pad1,19,-,0,NONE,0,0,0,NONE,Make it even +50,MAX,pad2,32,-,0,NONE,0,0,0,NONE,- From f551e19f77e83fa275ddfe72aa5d73812769e5bd Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:21:12 -0500 Subject: [PATCH 023/151] Copied from FOX1E file --- .../CubeSatSim_PSK_mintelemetry.csv | 52 +++++++++++++++++++ 1 file changed, 52 insertions(+) create mode 100644 spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv new file mode 100644 index 00000000..89fe9a7a --- /dev/null +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv @@ -0,0 +1,52 @@ +51,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,MIN,BATT_C_V,12,V,4,NONE,4,3,3,Cell A + B + C,Battery pairs A+B+C voltage (0-5.0V scale) +3,MIN,battAtemp,12,C,8,NONE,4,4,3,Temperature A,Battery pair A temperature +4,MIN,battBtemp,12,C,8,NONE,4,5,3,Temperature B,Battery pair B temperature +5,MIN,battCtemp,12,C,8,NONE,4,6,3,Temperature C,Battery pair C temperature +6,MIN,battCurr,12,mA,9,NONE,4,7,3,Current,Total Battery DC current +7,MIN,battCardTemp,12,C,8,NONE,4,8,3,Board Temp,Battery Card Temperature +8,MIN,posXv,12,V,23,NONE,8,1,3,Voltage,+X solar Panel voltage +9,MIN,posYv,12,V,23,NONE,9,1,3,Voltage,+Y solar Panel voltage +10,MIN,posZv,12,V,23,NONE,10,1,3,Voltage,+Z solar Panel voltage +11,MIN,negXv,12,V,23,NONE,11,1,3,Voltage,-X solar Panel voltage +12,MIN,negYv,12,V,23,NONE,12,1,3,Voltage,-Y solar Panel voltage +13,MIN,negZv,12,V,23,NONE,13,1,3,Voltage,-Z solar Panel voltage +14,MIN,posXt,12,C,24,NONE,8,2,3,Temp,+X solar Panel temperature +15,MIN,posYt,12,C,24,NONE,9,2,3,Temp,+Y solar Panel temperature +16,MIN,posZt,12,C,24,NONE,10,2,3,Temp,+Z solar Panel temperature +17,MIN,negXt,12,C,24,NONE,11,2,3,Temp,-X solar Panel temperature +18,MIN,negYt,12,C,24,NONE,12,2,3,Temp,-Y solar Panel temperature +19,MIN,negZt,12,C,24,NONE,13,2,3,Temp,-Z solar Panel temperature +20,MIN,PSUTemp,12,C,8,NONE,5,2,3,Board Temp,Power Supply Card Temperature +21,MIN,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MIN,TxPAi,12,mA,38,NONE,1,2,3,PA Current,Transmit power amplifier current +23,MIN,TxTemp,12,C,37,NONE,1,1,3,TX Temperature,Transmitter card temperature +24,MIN,FwdPower,12,mW,40,NONE,1,4,3,Fwd Power,Receiver card temperature +25,MIN,rssi,12,dBm,14,NONE,1,3,3,RSSI,Received Signal Strength Indication +26,MIN,IHUcpuTemp,12,C,15,NONE,2,1,3,Temperature,Internal Temperature of IHU +27,MIN,SatelliteXAxisAngularVelocity,12,dps,13,NONE,8,3,3,Rotation,Angular Veolcity around X Axis +28,MIN,SatelliteYAxisAngularVelocity,12,dps,13,NONE,9,3,3,Rotation,Angular Veolcity around Y Axis +29,MIN,SatelliteZAxisAngularVelocity,12,dps,13,NONE,10,3,3,Rotation,Angular Veolcity around Z Axis +30,MIN,Exp4Temp,12,C,7,NONE,6,1,3,EXP4 Temp,Experiment 4 card temperature +31,MIN,PSUCurrent,12,mA,22,NONE,5,1,3,Current,Power Supply DC Current +32,MIN,ReflectedPwr,12,mW,41,NONE,1,5,3,Ref Power,Reflected Power from the Transmit Antenna +33,MIN,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V +34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +37,MIN,rf6,12,-,0,NONE,0,0,0,None,None +38,MIN,rf7,12,-,0,NONE,0,0,0,None,None +39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +40,MIN,LtVGACtl,12,V,42,NONE,1,6,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused +42,MIN,IHUsoftError,32,-,39,NONE,3,8,0,Soft Error,Diagnostic Data on IHU Software Errors +43,MIN,minTimestampReset,16,s,1,NONE,0,0,0,NONE,Timestamp Resets +44,MIN,minTimestampUptime,25,s,1,NONE,0,0,0,NONE,Timestamp uptime +45,MIN,SafeModeIndication,1,-,21,NONE,0,0,0,NONE,In safe mode? +46,MIN,AutoSafeModeActive,1,-,21,NONE,0,0,0,NONE,In Autosafe mode? +47,MIN,AutoSafeModeAllowed,1,-,21,NONE,0,0,0,NONE,Autosafe enabled? +48,MIN,ScienceModeActive,1,-,21,NONE,0,0,0,Science Mode,In Science Mode? +49,MIN,pad1,19,-,0,NONE,0,0,0,NONE,Make it even +50,MIN,pad2,32,-,0,NONE,0,0,0,NONE,Make it even From 45b7dce1f860fdb283c8218fc3c528fcd9cbe48e Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:23:05 -0500 Subject: [PATCH 024/151] changed to CubeSatSim max and min --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 8ef9741f..2bf8fa66 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -30,11 +30,11 @@ frameLayout4.name=WOD Beacon numberOfLayouts=9 layout0.filename=FOX1A_debug.csv layout0.name=DEBUG -layout1.filename=FOX1E_maxtelemetry.csv +layout1.filename=CubeSatSim_PSK_maxtelemetry.csv layout1.name=maxtelemetry -layout2.filename=cubesatsim_psk_rttelemetry.csv +layout2.filename=CubeSatSim_PSK_rttelemetry.csv layout2.name=rttelemetry -layout3.filename=FOX1E_mintelemetry.csv +layout3.filename=CubeSatSim_PSK_mintelemetry.csv layout3.name=mintelemetry layout4.filename=FOX1E_radtelemetry.csv layout4.name=radtelemetry From e0f6bc09a778499e15e4e05643a3d7551b466190 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:23:49 -0500 Subject: [PATCH 025/151] Rename cubesatsim_psk_rttelemetry.csv to CubeSatSim_PSK_rttelemetry.csv --- ...esatsim_psk_rttelemetry.csv => CubeSatSim_PSK_rttelemetry.csv} | 0 1 file changed, 0 insertions(+), 0 deletions(-) rename spacecraft/FoxTelem_1.09m/{cubesatsim_psk_rttelemetry.csv => CubeSatSim_PSK_rttelemetry.csv} (100%) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv similarity index 100% rename from spacecraft/FoxTelem_1.09m/cubesatsim_psk_rttelemetry.csv rename to spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv From 5e5c12d89b1c75b24f20b7beda6ac1cc2cfb9480 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:32:05 -0500 Subject: [PATCH 026/151] Fixed numbering --- .../CubeSatSim_PSK_rttelemetry.csv | 22 +++++++++---------- 1 file changed, 11 insertions(+), 11 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 61203393..f9bd7905 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -2,11 +2,11 @@ 0,realTime,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,realTime,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) -3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,6,4,3,Acceleration,Acceleration around X Axis -4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis -5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis +3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,realTime,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current -7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature +7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature 8,realTime,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage 9,realTime,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage 10,realTime,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage @@ -21,15 +21,15 @@ 19,realTime,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current 20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,2,3,Board Voltage,Power Supply Voltage 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure -23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude +22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude 24,realTime,FwdPower,12,mW,40,Radio,1,2,3,Fwd Power,Receiver card temperature 25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,realTime,Exp4Temp,12,C,7,Experiments,6,1,3,EXP4 Temp,Experiment 4 card temperature +30,realTime,Exp4Temp,12,C,7,Experiments,6,5,3,EXP4 Temp,Experiment 4 card temperature 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current 32,realTime,ReflectedPwr,12,mW,41,Radio,1,3,3,Ref Power,Reflected Power from the Transmit Antenna 33,realTime,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V @@ -42,10 +42,10 @@ 40,realTime,LtVGACtl,12,V,42,Radio,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused 42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -43,realTime,expFailure0,1,-,17,Experiments,6,2,0,Vanderbilt Radiation,Vanderbilt University Vulcan Experiment Indicator -44,realTime,expFailure1,1,-,17,Experiments,6,3,0,Exp 1,Experiment 1 Failure Indicator -45,realTime,expFailure2,1,-,17,Experiments,6,4,0,Exp 2,Experiment 2 Failure Indicator -46,realTime,expFailure3,1,-,17,Experiments,6,5,0,Exp 3,Experiment 3 Failure Indicator +43,realTime,expFailure0,1,-,17,Experiments,6,1,0,Vanderbilt Radiation,Vanderbilt University Vulcan Experiment Indicator +44,realTime,expFailure1,1,-,17,Experiments,6,6,0,Exp 1,Experiment 1 Failure Indicator +45,realTime,expFailure2,1,-,17,Experiments,6,7,0,Exp 2,Experiment 2 Failure Indicator +46,realTime,expFailure3,1,-,17,Experiments,6,8,0,Exp 3,Experiment 3 Failure Indicator 47,realTime,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator 48,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 49,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator From d7c39bf442bf7208ffbeaa3c0ac08f8aaff0c0bf Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:39:38 -0500 Subject: [PATCH 027/151] turned off various --- .../CubeSatSim_PSK_rttelemetry.csv | 20 +++++++++---------- 1 file changed, 10 insertions(+), 10 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index f9bd7905..a88a8d55 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -23,7 +23,7 @@ 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude -24,realTime,FwdPower,12,mW,40,Radio,1,2,3,Fwd Power,Receiver card temperature +24,realTime,FwdPower,12,mW,40,NONE,1,2,3,Fwd Power,Receiver card temperature 25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis @@ -31,7 +31,7 @@ 29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,realTime,Exp4Temp,12,C,7,Experiments,6,5,3,EXP4 Temp,Experiment 4 card temperature 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current -32,realTime,ReflectedPwr,12,mW,41,Radio,1,3,3,Ref Power,Reflected Power from the Transmit Antenna +32,realTime,ReflectedPwr,12,mW,41,NONE,1,3,3,Ref Power,Reflected Power from the Transmit Antenna 33,realTime,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V 34,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 35,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V @@ -39,20 +39,20 @@ 37,realTime,rf6,12,-,0,NONE,0,0,0,None,None 38,realTime,rf7,12,-,0,NONE,0,0,0,None,None 39,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR -40,realTime,LtVGACtl,12,V,42,Radio,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +40,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused 42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance 43,realTime,expFailure0,1,-,17,Experiments,6,1,0,Vanderbilt Radiation,Vanderbilt University Vulcan Experiment Indicator -44,realTime,expFailure1,1,-,17,Experiments,6,6,0,Exp 1,Experiment 1 Failure Indicator -45,realTime,expFailure2,1,-,17,Experiments,6,7,0,Exp 2,Experiment 2 Failure Indicator -46,realTime,expFailure3,1,-,17,Experiments,6,8,0,Exp 3,Experiment 3 Failure Indicator +44,realTime,expFailure1,1,-,17,NONE,6,6,0,Exp 1,Experiment 1 Failure Indicator +45,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator +46,realTime,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator 47,realTime,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator 48,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 49,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -50,realTime,TLMresets,4,-,1,Computer Hardware,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -51,realTime,RxAntDeploy,1,-,16,Radio,1,6,0,RX Antenna,2m Antenna status -52,realTime,TxAntDeploy,2,-,16,Radio,1,5,0,TX Antenna,70cm Antenna status -53,realTime,I2CfailureRF,1,-,17,Computer Hardware,2,5,0,RF I2C,RF I2C Bus failure indicator +50,realTime,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +51,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status +52,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +53,realTime,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator 54,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler 55,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds 56,realTime,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information From ec0fdf45f0f0d5a12c202e88f0d73eee2cc51c50 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:46:36 -0500 Subject: [PATCH 028/151] added Sensor 1 and 2 --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index a88a8d55..d9a8987c 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -29,9 +29,9 @@ 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,realTime,Exp4Temp,12,C,7,Experiments,6,5,3,EXP4 Temp,Experiment 4 card temperature +30,realTime,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current -32,realTime,ReflectedPwr,12,mW,41,NONE,1,3,3,Ref Power,Reflected Power from the Transmit Antenna +32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,realTime,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V 34,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 35,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V @@ -42,7 +42,7 @@ 40,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused 42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -43,realTime,expFailure0,1,-,17,Experiments,6,1,0,Vanderbilt Radiation,Vanderbilt University Vulcan Experiment Indicator +43,realTime,STEMPayloadOK,1,-,17,Experiments,6,1,0,STEM Payload Board Failure Indicator 44,realTime,expFailure1,1,-,17,NONE,6,6,0,Exp 1,Experiment 1 Failure Indicator 45,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator 46,realTime,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator From 06e976d926c476e0d69e831f1dbd69521ac362e8 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:52:02 -0500 Subject: [PATCH 029/151] fixed error on STEM Payload status --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index d9a8987c..9a802af7 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -42,7 +42,7 @@ 40,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused 42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -43,realTime,STEMPayloadOK,1,-,17,Experiments,6,1,0,STEM Payload Board Failure Indicator +43,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator 44,realTime,expFailure1,1,-,17,NONE,6,6,0,Exp 1,Experiment 1 Failure Indicator 45,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator 46,realTime,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator From fe5bae5c58bc04795291923df7b7d90b58acff4f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 13:52:52 -0500 Subject: [PATCH 030/151] renamed STEM Payload Status variable --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 1602cf7d..8e0ed223 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -33,7 +33,7 @@ 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Unused,20,na,7,NONE,0,0,0,Unused,Unused -34,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status +34,RT,STEMPayloadStatus,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status 35,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 36,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 37,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used From 1d53090cd953ff1e12f044b37c0fad55666dad5d Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:06:24 -0500 Subject: [PATCH 031/151] added Sensor 3 --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 9a802af7..663c19d8 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -32,7 +32,7 @@ 30,realTime,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current 32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,realTime,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V +33,realTime,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 35,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V 36,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected From 839a48083fad4e9e651eb0f32306bafe02db2569 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:08:17 -0500 Subject: [PATCH 032/151] Added Sensor 3 --- .../CubeSatSim_rttelemetryFM.csv | 27 ++++++++++--------- 1 file changed, 14 insertions(+), 13 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 8e0ed223..3af53661 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,4 +1,4 @@ -45,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,3,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) @@ -32,15 +32,16 @@ 30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,RT,Unused,20,na,7,NONE,0,0,0,Unused,Unused -34,RT,STEMPayloadStatus,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status -35,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -36,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -37,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -38,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator -39,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator -40,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator -41,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -42,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status -43,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status -44,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE +33,RT,Sensor2,12,signed raw,cubesatsim_sensor3,Experiments,5,7,3,Sensor 2,STEM Payload Extra Sensor 3 +34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused +35,RT,STEMPayloadStatus,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status +36,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +37,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +38,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +39,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator +40,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator +41,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator +42,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +43,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status +44,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status +45,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE From cd749932f249cb5cd4dc54c1631bb96c8dfe6926 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:17:45 -0500 Subject: [PATCH 033/151] Inserted Computer Software panel --- .../CubeSatSim_rttelemetryFM.csv | 68 +++++++++---------- 1 file changed, 34 insertions(+), 34 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 3af53661..b1caf7cd 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,46 +1,46 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,3,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) -3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,6,4,3,Acceleration,Acceleration around X Axis -4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis -5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis -6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,3,2,3,Current,Total Battery DC current -7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature -8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,6,2,3,Voltage,+X Panel -9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,9,2,3,Voltage,-X Panel -10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,7,2,3,Voltage,+YPanel -11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage,-Y Panel,10,2,3,Voltage,-Y Panel -12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage,+Z Panel,8,2,3,Voltage,+Z Panel -13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage,-Z Panel,11,2,3,Voltage,-Z Panel -14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_ina219_current,+X Panel,6,1,3,Current,+X Panel -15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_ina219_current,-X Panel,9,1,3,Current,-X Panel -16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_ina219_current,+Y Panel,7,1,3,Current,+Y Panel -17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,10,1,3,Current,-Y Panel -18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,8,1,3,Current,+Z Panel -19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel -20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage -21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells -22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure -23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude +2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) +3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,4,2,3,Current,Total Battery DC current +7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature +8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,7,2,3,Voltage,+X Panel +9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,10,2,3,Voltage,-X Panel +10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,8,2,3,Voltage,+YPanel +11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage,-Y Panel,11,2,3,Voltage,-Y Panel +12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage,+Z Panel,9,2,3,Voltage,+Z Panel +13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage,-Z Panel,12,2,3,Voltage,-Z Panel +14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_ina219_current,+X Panel,7,1,3,Current,+X Panel +15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_ina219_current,-X Panel,10,1,3,Current,-X Panel +16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_ina219_current,+Y Panel,8,1,3,Current,+Y Panel +17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,1,3,Current,-Y Panel +18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,1,3,Current,+Z Panel +19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,1,3,Current,-Z Panel +20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,2,3,Board Voltage,Power Supply Voltage +21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude 24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature 25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication -26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU -27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis -28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis -29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis -30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current -32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,RT,Sensor2,12,signed raw,cubesatsim_sensor3,Experiments,5,7,3,Sensor 2,STEM Payload Extra Sensor 3 +26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU +27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current +32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused -35,RT,STEMPayloadStatus,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status +35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status 36,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 37,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 38,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -39,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator -40,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator -41,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator +39,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,3,0,Battery I2C,Battery I2C Bus failure indicator +40,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator +41,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator 42,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry 43,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status 44,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status From 8ad636309ada142e21c2c123f0ab885cf0e12541 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:19:08 -0500 Subject: [PATCH 034/151] renumbered Computer Hardware --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index b1caf7cd..4e7eb42a 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -38,9 +38,9 @@ 36,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 37,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 38,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -39,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,3,0,Battery I2C,Battery I2C Bus failure indicator -40,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator -41,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator +39,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator +40,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +41,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 42,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry 43,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status 44,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status From 66f8397cdb422702821be59d273ce87d333ec3a2 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:21:33 -0500 Subject: [PATCH 035/151] changed Battery and PSU --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 4e7eb42a..0267e50f 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,7 +1,7 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) +2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis 5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis @@ -19,7 +19,7 @@ 17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,1,3,Current,-Y Panel 18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,1,3,Current,+Z Panel 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,1,3,Current,-Z Panel -20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,2,3,Board Voltage,Power Supply Voltage +20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude @@ -30,7 +30,7 @@ 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current +31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused From 811e996156da1dd974841674fb8dc709dccbf3e7 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:22:29 -0500 Subject: [PATCH 036/151] Fixed Batter and PSUI --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 663c19d8..76cf6ab9 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -1,7 +1,7 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,realTime,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,realTime,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A + B + C,Battery A+B+C voltage (0-5.0V scale) +2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis 5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis @@ -19,7 +19,7 @@ 17,realTime,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current 18,realTime,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current 19,realTime,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current -20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,2,3,Board Voltage,Power Supply Voltage +20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude @@ -30,7 +30,7 @@ 28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,realTime,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,1,3,Current,Power Supply DC Current +31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,realTime,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted From 3a0b4599afbecb0545a64e8a21186c0c3f22240d Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:26:06 -0500 Subject: [PATCH 037/151] swapped order of Voltage and Current and removed RX Temp --- .../CubeSatSim_rttelemetryFM.csv | 32 +++++++++---------- 1 file changed, 16 insertions(+), 16 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 0267e50f..a3f0d3e7 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -7,24 +7,24 @@ 5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,4,2,3,Current,Total Battery DC current 7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,7,2,3,Voltage,+X Panel -9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,10,2,3,Voltage,-X Panel -10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,8,2,3,Voltage,+YPanel -11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage,-Y Panel,11,2,3,Voltage,-Y Panel -12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage,+Z Panel,9,2,3,Voltage,+Z Panel -13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage,-Z Panel,12,2,3,Voltage,-Z Panel -14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_ina219_current,+X Panel,7,1,3,Current,+X Panel -15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_ina219_current,-X Panel,10,1,3,Current,-X Panel -16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_ina219_current,+Y Panel,8,1,3,Current,+Y Panel -17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,1,3,Current,-Y Panel -18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,1,3,Current,+Z Panel -19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,1,3,Current,-Z Panel +8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X Panel +9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,10,1,3,Voltage,-X Panel +10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+YPanel +11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage,-Y Panel,11,1,3,Voltage,-Y Panel +12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z Panel +13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage,-Z Panel,12,1,3,Voltage,-Z Panel +14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_ina219_current,+X Panel,7,2,3,Current,+X Panel +15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_ina219_current,-X Panel,10,2,3,Current,-X Panel +16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,3,Current,+Y Panel +17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,3,Current,-Y Panel +18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel +19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude -24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature -25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication +24,RT,RXTemperature,12,C,7,NONE,1,1,3,RX Temperature,Receiver card temperature +25,RT,RSSI,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis @@ -42,6 +42,6 @@ 40,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 41,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 42,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -43,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status -44,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status +43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,70cm Antenna status +44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Antenna status 45,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE From 584a061823744c05f74e7874ac7dbcf7d3cd6d4d Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:29:56 -0500 Subject: [PATCH 038/151] Added Resets Count --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 76cf6ab9..8ad9c24d 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -23,7 +23,7 @@ 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude -24,realTime,FwdPower,12,mW,40,NONE,1,2,3,Fwd Power,Receiver card temperature +24,realTime,Resets,12,-,12,Computer Software,3,2,3,Reset Count 25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis From a79dedac463089649f812d95927f8ebf2b544428 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:30:24 -0500 Subject: [PATCH 039/151] Update CubeSatSim_PSK_rttelemetry.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 8ad9c24d..4de688d1 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -23,7 +23,7 @@ 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude -24,realTime,Resets,12,-,12,Computer Software,3,2,3,Reset Count +24,realTime,Resets,12,-,12,Computer Software,3,2,3,Reset Count, Software Reset Count 25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis From ad7d5ca09a97ece71e1890043fd71e941d7d555d Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:31:21 -0500 Subject: [PATCH 040/151] added Software Reset Count --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 1 + 1 file changed, 1 insertion(+) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index a3f0d3e7..c9aa7190 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -23,6 +23,7 @@ 21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +24,RT,Resets,12,-,12,Computer Software,3,2,3,Reset Count, Software Reset Count 24,RT,RXTemperature,12,C,7,NONE,1,1,3,RX Temperature,Receiver card temperature 25,RT,RSSI,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU From 0d068caa260708ea1016bff6638049117aaf1e75 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:32:52 -0500 Subject: [PATCH 041/151] Update CubeSatSim_rttelemetryFM.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 1 - 1 file changed, 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index c9aa7190..2e938b6c 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -24,7 +24,6 @@ 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude 24,RT,Resets,12,-,12,Computer Software,3,2,3,Reset Count, Software Reset Count -24,RT,RXTemperature,12,C,7,NONE,1,1,3,RX Temperature,Receiver card temperature 25,RT,RSSI,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis From 2a5dc07e71114c4c54fa186f38831731449c56a6 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:39:08 -0500 Subject: [PATCH 042/151] Added Safe Mode flag --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 2e938b6c..143dbb17 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -23,7 +23,7 @@ 21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude -24,RT,Resets,12,-,12,Computer Software,3,2,3,Reset Count, Software Reset Count +24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count 25,RT,RSSI,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis @@ -35,7 +35,7 @@ 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused 35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status -36,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +36,RT,Safe Mode,3,-,17,Computer Software,5,0,0,Safe Mode, Safe Mode 37,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 38,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 39,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator From cefbcfdd4ac05e7c200871b074e1d8d4baef7f42 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:41:02 -0500 Subject: [PATCH 043/151] fixed Safe Mode --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 143dbb17..fae02271 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -35,7 +35,7 @@ 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused 35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status -36,RT,Safe Mode,3,-,17,Computer Software,5,0,0,Safe Mode, Safe Mode +36,RT,Safe Mode,1,-,17,Computer Software,3,2,0,Safe Mode, Safe Mode 37,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 38,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 39,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator From d2bd792edc914457fea9a444efca9db21bcec746 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:46:30 -0500 Subject: [PATCH 044/151] changed Safe Mode to Nominal Mode --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index fae02271..a71243f4 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -35,7 +35,7 @@ 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused 35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status -36,RT,Safe Mode,1,-,17,Computer Software,3,2,0,Safe Mode, Safe Mode +36,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 37,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 38,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 39,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator From a625b2c638500dada964021dba2dfa28a9b998c5 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:49:22 -0500 Subject: [PATCH 045/151] Added Nominal Mode --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 4de688d1..8be4553d 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -43,7 +43,7 @@ 41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused 42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance 43,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator -44,realTime,expFailure1,1,-,17,NONE,6,6,0,Exp 1,Experiment 1 Failure Indicator +44,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 45,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator 46,realTime,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator 47,realTime,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator From 3e2c3e2334ee60332b0af22853618fe7b10e1e2f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 15:34:52 -0500 Subject: [PATCH 046/151] Removed Resets --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 8be4553d..e42c9665 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -23,7 +23,7 @@ 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude -24,realTime,Resets,12,-,12,Computer Software,3,2,3,Reset Count, Software Reset Count +24,realTime,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count 25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis From 638299c8a61d2b2f5be6778099b25fa7c85e7139 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:02:50 -0500 Subject: [PATCH 047/151] set all experiments to 0 --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 2bf8fa66..df32a230 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -11,10 +11,10 @@ name=CubeSatSim displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true -EXP1=6 -EXP2=1 -EXP3=8 -EXP4=7 +EXP1=0 +EXP2=0 +EXP3=0 +EXP4=0 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From 8798b1cf09c02201245c175e0cfa5d8c3850d19b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:06:46 -0500 Subject: [PATCH 048/151] changed to 3 layouts --- .../FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 14 +------------- 1 file changed, 1 insertion(+), 13 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index df32a230..c3810252 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -27,7 +27,7 @@ frameLayout3.filename=FOX1E_Type3_REALTIME_BEACON.frame frameLayout3.name=Realtime Beacon frameLayout4.filename=FOX1E_Type4_WOD_BEACON.frame frameLayout4.name=WOD Beacon -numberOfLayouts=9 +numberOfLayouts=3 layout0.filename=FOX1A_debug.csv layout0.name=DEBUG layout1.filename=CubeSatSim_PSK_maxtelemetry.csv @@ -36,18 +36,6 @@ layout2.filename=CubeSatSim_PSK_rttelemetry.csv layout2.name=rttelemetry layout3.filename=CubeSatSim_PSK_mintelemetry.csv layout3.name=mintelemetry -layout4.filename=FOX1E_radtelemetry.csv -layout4.name=radtelemetry -layout5.filename=FOX1E_radtelemetry2.csv -layout5.name=radtelemetry2 -layout5.parentLayout=radtelemetry -layout6.filename=FOX1E_wodtelemetry.csv -layout6.name=wodtelemetry -layout7.filename=FOX1E_wodradtelemetry.csv -layout7.name=wodradtelemetry -layout8.filename=FOX1E_wodradtelemetry2.csv -layout8.name=wodradtelemetry2 -layout8.parentLayout=wodradtelemetry numberOfLookupTables=3 lookupTable0.filename=FOX1A_rssiFM.tab lookupTable0=RSSI From 4629cec2112a95feaaf3eddee445cf247dfc73bf Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:25:42 -0500 Subject: [PATCH 049/151] fixed number of layouts --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index c3810252..dff61533 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -27,7 +27,7 @@ frameLayout3.filename=FOX1E_Type3_REALTIME_BEACON.frame frameLayout3.name=Realtime Beacon frameLayout4.filename=FOX1E_Type4_WOD_BEACON.frame frameLayout4.name=WOD Beacon -numberOfLayouts=3 +numberOfLayouts=4 layout0.filename=FOX1A_debug.csv layout0.name=DEBUG layout1.filename=CubeSatSim_PSK_maxtelemetry.csv From b67604d73b96ad8fc60a4b8b0a661b6e00246bd6 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:30:09 -0500 Subject: [PATCH 050/151] Added FLOAT2 to set 2 dp for Voltages --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 10 +++++----- 1 file changed, 5 insertions(+), 5 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index a71243f4..d13ff0dd 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,10 +1,10 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,RT,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis -4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +2,RT,BATT_V,12,V,cubesatsim_ina219_voltage | FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_racceleration | FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,4,2,3,Current,Total Battery DC current 7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature 8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X Panel @@ -19,7 +19,7 @@ 17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,3,Current,-Y Panel 18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel -20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage +20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage | FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude From 76f43efe045b6dbeeabb6e480633a23547dbc06b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:30:38 -0500 Subject: [PATCH 051/151] typo --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index d13ff0dd..c1e381c8 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -4,7 +4,7 @@ 2,RT,BATT_V,12,V,cubesatsim_ina219_voltage | FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_racceleration | FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,4,2,3,Current,Total Battery DC current 7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature 8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X Panel From 50576e24ef69b452aff062b6706ffe620bdecb2d Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:33:25 -0500 Subject: [PATCH 052/151] made all voltages 2 dp --- .../CubeSatSim_rttelemetryFM.csv | 20 +++++++++---------- 1 file changed, 10 insertions(+), 10 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index c1e381c8..77deef2f 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,18 +1,18 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,RT,BATT_V,12,V,cubesatsim_ina219_voltage | FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis -4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration | FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +2,RT,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,4,2,3,Current,Total Battery DC current 7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X Panel -9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,10,1,3,Voltage,-X Panel -10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+YPanel -11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage,-Y Panel,11,1,3,Voltage,-Y Panel -12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z Panel -13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage,-Z Panel,12,1,3,Voltage,-Z Panel +8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel +9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel +10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+YPanel +11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel +12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel +13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel 14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_ina219_current,+X Panel,7,2,3,Current,+X Panel 15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_ina219_current,-X Panel,10,2,3,Current,-X Panel 16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,3,Current,+Y Panel From a59826ff6f44376420c94d8d9b7899c91a13b569 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:34:41 -0500 Subject: [PATCH 053/151] All voltages 2 dp with |FLOAT2 --- .../CubeSatSim_PSK_rttelemetry.csv | 16 ++++++++-------- 1 file changed, 8 insertions(+), 8 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index e42c9665..b304377d 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -1,25 +1,25 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,realTime,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,realTime,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis 5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,realTime,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current 7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,realTime,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage -9,realTime,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage -10,realTime,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage -11,realTime,negXv,12,V,cubesatsim_ina219_voltage,-X Panel,10,1,3,Voltage,-X solar Panel voltage -12,realTime,negYv,12,V,cubesatsim_ina219_voltage,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage -13,realTime,negZv,12,V,cubesatsim_ina219_voltage,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage +8,realTime,posXv,12,V,cubesatsim_ina219_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage +9,realTime,posYv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage +10,realTime,posZv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage +11,realTime,negXv,12,V,cubesatsim_ina219_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage +12,realTime,negYv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage +13,realTime,negZv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage 14,realTime,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current 15,realTime,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current 16,realTime,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current 17,realTime,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current 18,realTime,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current 19,realTime,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current -20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage +20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage 21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude From f7ea1e9a102146aae859c808141be3e8e23df659 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:39:59 -0500 Subject: [PATCH 054/151] changed accel curve --- spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv index 087a4af3..cc7cb072 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv @@ -3,7 +3,7 @@ cubesatsim_ina219_voltage,0,0.01,0,0,0,0,Converts voltages read from the INA219 cubesatsim_ina219_current,-2048,1,0,0,0,0,Converts positive and negative currents read from the INA219 sensors cubesatsim_temperature,0,0.1,0,0,0,0,Converts temperature of Pi cubesatsim_rotation,-2048,1,0,0,0,0,Converts positive and negative dps rotation -cubesatsim_acceleration,-2048,0.01,0,0,0,0,Converts positive and negative g acceleration +cubesatsim_acceleration,-20.48,0.01,0,0,0,0,Converts positive and negative g acceleration cubesatsim_altitude,0,0.1,0,0,0,0,Converts altitude cubesatsim_pressure,0,1,0,0,0,0,Converts pressure cubesatsim_sensor1,0,1,0,0,0,0,Integer conversion of Sensor 1 From beb0194e5c56d4b1ae356f04f5a460a4175d0545 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:42:44 -0500 Subject: [PATCH 055/151] test accel values --- afsk/main.c | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 0db1befd..2604835c 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -22,6 +22,7 @@ #include #include #include + #include #include #include "status.h" @@ -885,7 +886,7 @@ int get_tlm_fox() { // int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0 int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; - int xAccel = 2048, yAccel = 2048, zAccel = 2048, temp = 224, pressure = 1000, altitude = 1000; + int xAccel = 2048+100, yAccel = 2048-100, zAccel = 2048+500, temp = 224, pressure = 1000, altitude = 1000; int sensor1 = 0, sensor2 = 2048; short int buffer_test[bufLen]; From 6692047dd19371be85122f974c8c1de447ab825f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:49:56 -0500 Subject: [PATCH 056/151] added Sensor 3 conversion --- spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv | 5 +++-- 1 file changed, 3 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv index cc7cb072..109b4f4e 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv @@ -6,5 +6,6 @@ cubesatsim_rotation,-2048,1,0,0,0,0,Converts positive and negative dps rotation cubesatsim_acceleration,-20.48,0.01,0,0,0,0,Converts positive and negative g acceleration cubesatsim_altitude,0,0.1,0,0,0,0,Converts altitude cubesatsim_pressure,0,1,0,0,0,0,Converts pressure -cubesatsim_sensor1,0,1,0,0,0,0,Integer conversion of Sensor 1 -cubesatsim_sensor2,-2048,1,0,0,0,0,Integer conversion of Sensor 2 +cubesatsim_sensor1,0,1,0,0,0,0,Conversion of Sensor 1 +cubesatsim_sensor2,-2048,1,0,0,0,0,Conversion of Sensor 2 +cubesatsim_sensor3,-20.48,0.01,0,0,0,0,Conversion of Sensor 3 From c13bf2769862b722e204f2942173575748bac62e Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 16:57:57 -0500 Subject: [PATCH 057/151] try Normal Mode FAIL --- afsk/main.c | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 2604835c..a2693ef4 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -887,7 +887,7 @@ int get_tlm_fox() { int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; int xAccel = 2048+100, yAccel = 2048-100, zAccel = 2048+500, temp = 224, pressure = 1000, altitude = 1000; - int sensor1 = 0, sensor2 = 2048; + int sensor1 = 0, sensor2 = 2048-3, sensor3 = 2048+200; short int buffer_test[bufLen]; int buffSize; @@ -1178,9 +1178,9 @@ if (payload == ON) encodeA(b, 45 + head_offset, sensor1); encodeB(b, 46 + head_offset,PSUCurrent); encodeA(b, 48 + head_offset, sensor2); - + encodeB(b, 49 + head_offset, sensor3); - encodeB(b, 51 + head_offset, STEMBoardFailure); + encodeB(b, 51 + head_offset, STEMBoardFailure + 32); // Normal Mode FAIL? short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From 5eb8dbc10971cd8fc7053a75b9fe0f5158534baa Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 17:04:36 -0500 Subject: [PATCH 058/151] Added NormalModeFailure and test RXAntenna and TXAntenna --- afsk/main.c | 5 +++-- 1 file changed, 3 insertions(+), 2 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index a2693ef4..76bf84d7 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -876,7 +876,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 16; + int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 16, NormalModeFailure = 0; // set to 32 to fail into Safe Mode int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; @@ -1180,7 +1180,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeB(b, 51 + head_offset, STEMBoardFailure + 32); // Normal Mode FAIL? + encodeB(b, 51 + head_offset, STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode + encodeA(b, 52 + head_offset, 16+32+64); // Try TXAntenna RXAntenna short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From 84562e9d191e77c7083251a035fee427ccfe59ef Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 17:09:04 -0500 Subject: [PATCH 059/151] testing NormalModeFail --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 76bf84d7..b5cabf57 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -876,7 +876,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 16, NormalModeFailure = 0; // set to 32 to fail into Safe Mode + int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 16, NormalModeFailure = 32; // set to 32 to fail into Safe Mode int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From fe43a4b430f87a938fcfe73bd9e16c60e2129de9 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 09:29:01 -0500 Subject: [PATCH 060/151] Replaced from version n default, edited max and min filenames only to get rid of FoxTelem log errors --- .../CubeSat_Simulator_PSK_fm.MASTER | 24 ++++++++++++++----- 1 file changed, 18 insertions(+), 6 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index dff61533..c63f9913 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -11,10 +11,10 @@ name=CubeSatSim displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true -EXP1=0 -EXP2=0 -EXP3=0 -EXP4=0 +EXP1=6 +EXP2=1 +EXP3=8 +EXP4=7 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame @@ -27,15 +27,27 @@ frameLayout3.filename=FOX1E_Type3_REALTIME_BEACON.frame frameLayout3.name=Realtime Beacon frameLayout4.filename=FOX1E_Type4_WOD_BEACON.frame frameLayout4.name=WOD Beacon -numberOfLayouts=4 +numberOfLayouts=9 layout0.filename=FOX1A_debug.csv layout0.name=DEBUG layout1.filename=CubeSatSim_PSK_maxtelemetry.csv layout1.name=maxtelemetry -layout2.filename=CubeSatSim_PSK_rttelemetry.csv +layout2.filename=cubesatsim_psk_rttelemetry.csv layout2.name=rttelemetry layout3.filename=CubeSatSim_PSK_mintelemetry.csv layout3.name=mintelemetry +layout4.filename=FOX1E_radtelemetry.csv +layout4.name=radtelemetry +layout5.filename=FOX1E_radtelemetry2.csv +layout5.name=radtelemetry2 +layout5.parentLayout=radtelemetry +layout6.filename=FOX1E_wodtelemetry.csv +layout6.name=wodtelemetry +layout7.filename=FOX1E_wodradtelemetry.csv +layout7.name=wodradtelemetry +layout8.filename=FOX1E_wodradtelemetry2.csv +layout8.name=wodradtelemetry2 +layout8.parentLayout=wodradtelemetry numberOfLookupTables=3 lookupTable0.filename=FOX1A_rssiFM.tab lookupTable0=RSSI From 5abba2ac9eedeedae30fd7a79b55f872f8e57838 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 09:39:54 -0500 Subject: [PATCH 061/151] changed filename for rtt to CubeSatSim not cubesatsim --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index c63f9913..2bf8fa66 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -32,7 +32,7 @@ layout0.filename=FOX1A_debug.csv layout0.name=DEBUG layout1.filename=CubeSatSim_PSK_maxtelemetry.csv layout1.name=maxtelemetry -layout2.filename=cubesatsim_psk_rttelemetry.csv +layout2.filename=CubeSatSim_PSK_rttelemetry.csv layout2.name=rttelemetry layout3.filename=CubeSatSim_PSK_mintelemetry.csv layout3.name=mintelemetry From fec6f5db202f1262ea9609b3d6f12060a3c06896 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 10:27:58 -0500 Subject: [PATCH 062/151] changed mode to 0 for Engineering Model (EM) --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 2bf8fa66..455b1aa9 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -4,7 +4,7 @@ user_mode=4 foxId=99 IHU_SN=7 catalogNumber=0 -model=1 +model=0 mpptResistanceError=6.58 mpptSensorOffThreshold=1600 name=CubeSatSim From 5557f065770e1f09b6d41b28d42b039676f1e4d7 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 10:50:51 -0500 Subject: [PATCH 063/151] trying STEM Board Failure --- afsk/main.c | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index b5cabf57..794f71ce 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1180,8 +1180,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeB(b, 51 + head_offset, STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode - encodeA(b, 52 + head_offset, 16+32+64); // Try TXAntenna RXAntenna + encodeB(b, 52 + head_offset, 4095); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode + encodeA(b, 53 + head_offset, 0); // 16+32+64); // Try TXAntenna RXAntenna short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From db951ef4a7cd4ab3d53719d624a3795f22c5a508 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 10:54:47 -0500 Subject: [PATCH 064/151] More testing --- afsk/main.c | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 794f71ce..37ce82fb 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -7,7 +7,7 @@ * * This program is free software: you can redistribute it and/or modify * it under the terms of the GNU General Public License as published by - * the Free Software Foundation, either version 3 of the License, or/ + * the Free Software Foundation, either version 3 of the License, or * (at your option) any later version. * * This program is distributed in the hope that it will be useful, @@ -1180,8 +1180,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeB(b, 52 + head_offset, 4095); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode - encodeA(b, 53 + head_offset, 0); // 16+32+64); // Try TXAntenna RXAntenna + encodeA(b, 51 + head_offset, 4095); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode + encodeB(b, 52 + head_offset, 0); // 16+32+64); // Try TXAntenna RXAntenna short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; @@ -1539,7 +1539,7 @@ static unsigned char CCSDS_index_of[NN+1] = { 192,115,153,119,150, 92,250, 82,228,236, 95, 74,182,162, 22,134, 105,197, 98,254, 41,125,187,204,224,211, 77,140,242, 31, 48,220, 130,171,231, 86,179,147, 64,216, 52,176,239, 38, 55, 12, 17, 68, -111,120, 25,154, 71,116,167,193, 35, 83,137,251, 20, 93,248,151, +111,120, 25,154, 71,116,167,193, 35, 83,137,251, 20, 93,248,1/, 46, 75,185, 96, 15,237, 62,229,246,135,165, 23, 58,163, 60,183, }; From 2bdc2a00eaa4bff61676975f96b84274c2013975 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:09:37 -0500 Subject: [PATCH 065/151] testing sensor3 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 37ce82fb..9357df8c 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -887,7 +887,7 @@ int get_tlm_fox() { int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; int xAccel = 2048+100, yAccel = 2048-100, zAccel = 2048+500, temp = 224, pressure = 1000, altitude = 1000; - int sensor1 = 0, sensor2 = 2048-3, sensor3 = 2048+200; + int sensor1 = 0, sensor2 = 2048-3, sensor3 = 2048-1501; short int buffer_test[bufLen]; int buffSize; From b64fd616311e45a9d990130be35c32b63ba65fae Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:11:30 -0500 Subject: [PATCH 066/151] fixed lookup value --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 9357df8c..917c7a58 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1539,7 +1539,7 @@ static unsigned char CCSDS_index_of[NN+1] = { 192,115,153,119,150, 92,250, 82,228,236, 95, 74,182,162, 22,134, 105,197, 98,254, 41,125,187,204,224,211, 77,140,242, 31, 48,220, 130,171,231, 86,179,147, 64,216, 52,176,239, 38, 55, 12, 17, 68, -111,120, 25,154, 71,116,167,193, 35, 83,137,251, 20, 93,248,1/, +111,120, 25,154, 71,116,167,193, 35, 83,137,251, 20, 93,248,151, 46, 75,185, 96, 15,237, 62,229,246,135,165, 23, 58,163, 60,183, }; From f55727888d821a465d302eabc66be943e470ec56 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:15:59 -0500 Subject: [PATCH 067/151] added INT to Sensor 1 and FLOAT2 to Sensor 3 --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 77deef2f..3cc63105 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -19,7 +19,7 @@ 17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,3,Current,-Y Panel 18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel -20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage | FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage +20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude @@ -29,10 +29,10 @@ 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +30,RT,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused 35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status 36,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) From 338a95640285a8b6955b391c8936f0ebb1d4796c Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:21:10 -0500 Subject: [PATCH 068/151] Try removing experiments --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 4 ---- 1 file changed, 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 455b1aa9..a3e774ae 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -11,10 +11,6 @@ name=CubeSatSim displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true -EXP1=6 -EXP2=1 -EXP3=8 -EXP4=7 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From af8c39ef4a6b9ac5e0efceda18a659e312e5d75d Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:23:01 -0500 Subject: [PATCH 069/151] Just EXP1=0 --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 4 ++++ 1 file changed, 4 insertions(+) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index a3e774ae..665a316d 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -11,6 +11,10 @@ name=CubeSatSim displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true +EXP1=0 +EXP2=1 +EXP3=8 +EXP4=7 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From 6e5838573b0171508969393041900d58cbb7b6da Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:24:05 -0500 Subject: [PATCH 070/151] set all EXP to 0 --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 665a316d..30fe9ece 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -12,9 +12,9 @@ displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true EXP1=0 -EXP2=1 -EXP3=8 -EXP4=7 +EXP2=0 +EXP3=0 +EXP4=0 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From 219234dbebd15099f29a5fde87bf099ae8f9c8a0 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:26:08 -0500 Subject: [PATCH 071/151] resetting EXP back --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 30fe9ece..455b1aa9 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -11,10 +11,10 @@ name=CubeSatSim displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true -EXP1=0 -EXP2=0 -EXP3=0 -EXP4=0 +EXP1=6 +EXP2=1 +EXP3=8 +EXP4=7 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From 86e4bb7260f71d18e64cb59ecb68bc862221edef Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:44:24 -0500 Subject: [PATCH 072/151] reordered --- .../CubeSatSim_PSK_rttelemetry.csv | 38 +++++++++---------- 1 file changed, 19 insertions(+), 19 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index b304377d..67fcf98e 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -33,25 +33,25 @@ 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,realTime,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 -34,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted -35,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V -36,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected -37,realTime,rf6,12,-,0,NONE,0,0,0,None,None -38,realTime,rf7,12,-,0,NONE,0,0,0,None,None -39,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR -40,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) -41,realTime,pad,4,-,34,NONE,0,0,0,None,Unused -42,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -43,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator -44,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) -45,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator -46,realTime,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator -47,realTime,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator -48,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator -49,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -50,realTime,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -51,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status -52,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +35,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +36,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator +37,realTime,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator +38,realTime,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator +39,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +40,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator +41,realTime,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +42,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status +43,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +44,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +45,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +46,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +47,realTime,rf6,12,-,0,NONE,0,0,0,None,None +48,realTime,rf7,12,-,0,NONE,0,0,0,None,None +49,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +50,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +51,realTime,pad,4,-,34,NONE,0,0,0,None,Unused +52,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance 53,realTime,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator 54,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler 55,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds From 4e772c8a8ec28fa3474f89b9b767f7b9c9f8708b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:44:35 -0500 Subject: [PATCH 073/151] reordered --- .../CubeSatSim_rttelemetryFM.csv | 22 +++++++++---------- 1 file changed, 11 insertions(+), 11 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 3cc63105..308c8e1e 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -33,15 +33,15 @@ 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 -34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused -35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status -36,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) -37,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -38,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -39,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator -40,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator -41,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -42,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,70cm Antenna status -44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Antenna status +34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status +35,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +36,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +37,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used +38,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator +39,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +40,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator +41,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +42,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,70cm Antenna status +43,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Antenna status +44,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused 45,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE From 9464d69471e45867c7e8e9c3ef31cbc238362b1c Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:51:59 -0500 Subject: [PATCH 074/151] testing again --- afsk/main.c | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 917c7a58..0133aa2e 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1180,8 +1180,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeA(b, 51 + head_offset, 4095); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode - encodeB(b, 52 + head_offset, 0); // 16+32+64); // Try TXAntenna RXAntenna + encodeA(b, 51 + head_offset, 1 + 2048); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode + encodeB(b, 52 + head_offset, 1 + 2048); // 16+32+64); // Try TXAntenna RXAntenna short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From 26e0019d23df9fc089a047f02098cb790ecd246c Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 11:58:23 -0500 Subject: [PATCH 075/151] still testing --- afsk/main.c | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 0133aa2e..a972dc01 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1180,8 +1180,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeA(b, 51 + head_offset, 1 + 2048); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode - encodeB(b, 52 + head_offset, 1 + 2048); // 16+32+64); // Try TXAntenna RXAntenna + encodeA(b, 51 + head_offset, 1); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode + encodeB(b, 52 + head_offset, 2048); // 16+32+64); // Try TXAntenna RXAntenna short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From b51018b998bacfd52c97a2badaef5adc9801ae44 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:01:26 -0500 Subject: [PATCH 076/151] turning on all four status bits --- afsk/main.c | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index a972dc01..a1c46d54 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1180,8 +1180,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeA(b, 51 + head_offset, 1); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode - encodeB(b, 52 + head_offset, 2048); // 16+32+64); // Try TXAntenna RXAntenna + encodeA(b, 51 + head_offset, 1 + 2 + 2048); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode + encodeB(b, 52 + head_offset, 1); // 16+32+64); // Try TXAntenna RXAntenna short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From 7163cfe619c908439fed8959fa3b167e1b03c680 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:06:44 -0500 Subject: [PATCH 077/151] setting all EXP to 0 with new FoxTelem.jar --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 455b1aa9..30fe9ece 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -11,10 +11,10 @@ name=CubeSatSim displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true -EXP1=6 -EXP2=1 -EXP3=8 -EXP4=7 +EXP1=0 +EXP2=0 +EXP3=0 +EXP4=0 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From 97d18a77675317f1856605ebbb3e7a6b52739646 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:27:03 -0500 Subject: [PATCH 078/151] added one more flag to align --- .../FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 12 ++++++------ 1 file changed, 6 insertions(+), 6 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 308c8e1e..efb37365 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,4 +1,4 @@ -46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +45,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,RT,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) @@ -40,8 +40,8 @@ 38,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator 39,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 40,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -41,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -42,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,70cm Antenna status -43,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Antenna status -44,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused -45,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE +41,RT,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +42,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,70cm Antenna status +44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Antenna status +45,RT,Pad,58,-,0,NONE,0,0,0,NONE,NONE From 66b1808803a5fa8aed34f73fce5f6c05c47607b8 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:27:16 -0500 Subject: [PATCH 079/151] moved a flag to align --- .../CubeSatSim_PSK_rttelemetry.csv | 26 +++++++++---------- 1 file changed, 13 insertions(+), 13 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 67fcf98e..d7b77ba8 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -40,19 +40,19 @@ 38,realTime,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator 39,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 40,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -41,realTime,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -42,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status -43,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status -44,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted -45,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V -46,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected -47,realTime,rf6,12,-,0,NONE,0,0,0,None,None -48,realTime,rf7,12,-,0,NONE,0,0,0,None,None -49,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR -50,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) -51,realTime,pad,4,-,34,NONE,0,0,0,None,Unused -52,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -53,realTime,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +41,realTime,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +42,realTime,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +43,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status +44,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +45,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +46,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +47,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +48,realTime,rf6,12,-,0,NONE,0,0,0,None,None +49,realTime,rf7,12,-,0,NONE,0,0,0,None,None +50,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +51,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +52,realTime,pad,4,-,34,NONE,0,0,0,None,Unused +53,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance 54,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler 55,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds 56,realTime,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information From f1b1e200e2b2bbaba2b04e0dd38fcbbeb082b6ce Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:33:14 -0500 Subject: [PATCH 080/151] fixed number of fields --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index efb37365..873799ae 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,4 +1,4 @@ -45,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,RT,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) From 01b090441d2ac1b8ef26ca214a9e0008bd252e73 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:36:25 -0500 Subject: [PATCH 081/151] testing all flags --- afsk/main.c | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index a1c46d54..03632181 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1180,8 +1180,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeA(b, 51 + head_offset, 1 + 2 + 2048); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode - encodeB(b, 52 + head_offset, 1); // 16+32+64); // Try TXAntenna RXAntenna + encodeA(b, 51 + head_offset, 1 + 2); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode + encodeB(b, 52 + head_offset, 1 + 2); // 16+32+64); // Try TXAntenna RXAntenna short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From f40612f71c5f751f8c3d9d4568ee3a9ba951bbe8 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:37:58 -0500 Subject: [PATCH 082/151] only set EXP1 to 0 --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 30fe9ece..665a316d 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -12,9 +12,9 @@ displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true EXP1=0 -EXP2=0 -EXP3=0 -EXP4=0 +EXP2=1 +EXP3=8 +EXP4=7 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From d41a14c826fb57f2f55bf54a4c93a0a9495b1c10 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:48:47 -0500 Subject: [PATCH 083/151] added Ground Commands to Software --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 873799ae..0d0a7f6c 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -41,7 +41,7 @@ 39,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 40,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 41,RT,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator -42,RT,NumberofGroundCommandedTLMResets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +42,RT,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received 43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,70cm Antenna status 44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Antenna status 45,RT,Pad,58,-,0,NONE,0,0,0,NONE,NONE From 102ebd6d432dabcb3a3adc7ad48769357bef076b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:51:09 -0500 Subject: [PATCH 084/151] encoding for failures and antenna deployment and ground command count --- afsk/main.c | 7 +++---- 1 file changed, 3 insertions(+), 4 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 03632181..fdf0bbaa 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -7,7 +7,6 @@ * * This program is free software: you can redistribute it and/or modify * it under the terms of the GNU General Public License as published by - * the Free Software Foundation, either version 3 of the License, or * (at your option) any later version. * * This program is distributed in the hope that it will be useful, @@ -876,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 16, NormalModeFailure = 32; // set to 32 to fail into Safe Mode + int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 1, rxAntennaFailure = 1, txAntennaFailure = 0, groundCommandCount = 1; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; @@ -1180,8 +1179,8 @@ if (payload == ON) encodeA(b, 48 + head_offset, sensor2); encodeB(b, 49 + head_offset, sensor3); - encodeA(b, 51 + head_offset, 1 + 2); // STEMBoardFailure + NormalModeFailure); // NormalModeFailure set to 32 if in Safe Mode - encodeB(b, 52 + head_offset, 1 + 2); // 16+32+64); // Try TXAntenna RXAntenna + encodeA(b, 51 + head_offset, STEMBoardFailure + NormalModeFailure * 2 + groundCommandCount * 256); + encodeB(b, 52 + head_offset, rxAntenna + txAntenna * 2); short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From 01f8be893d495a9db063f19fa8055cb710ad193c Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:52:48 -0500 Subject: [PATCH 085/151] typo in antenna failure --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index fdf0bbaa..5ceb1792 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1180,7 +1180,7 @@ if (payload == ON) encodeB(b, 49 + head_offset, sensor3); encodeA(b, 51 + head_offset, STEMBoardFailure + NormalModeFailure * 2 + groundCommandCount * 256); - encodeB(b, 52 + head_offset, rxAntenna + txAntenna * 2); + encodeB(b, 52 + head_offset, rxAntennaFailure + txAntennaFailure* 2); short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From be0ad9844b53389c126140911577d6652dd1009e Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 12:58:13 -0500 Subject: [PATCH 086/151] changed antenna failure to antenna deploy --- afsk/main.c | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index 5ceb1792..fa852714 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 1, rxAntennaFailure = 1, txAntennaFailure = 0, groundCommandCount = 1; // + int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; @@ -1180,7 +1180,7 @@ if (payload == ON) encodeB(b, 49 + head_offset, sensor3); encodeA(b, 51 + head_offset, STEMBoardFailure + NormalModeFailure * 2 + groundCommandCount * 256); - encodeB(b, 52 + head_offset, rxAntennaFailure + txAntennaFailure* 2); + encodeB(b, 52 + head_offset, rxAntennaDeployed + txAntennaDeployed* 2); short int data10[headerLen + rsFrames * (rsFrameLen + parityLen)]; short int data8[headerLen + rsFrames * (rsFrameLen + parityLen)]; From bdbd35ff70272e885409c8c4c550eb7dab2a5e92 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 13:31:19 -0500 Subject: [PATCH 087/151] added ground commands count --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index d7b77ba8..73d3fcd5 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -41,7 +41,7 @@ 39,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator 40,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 41,realTime,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator -42,realTime,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received 43,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status 44,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status 45,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted From 60c9ee390c626afce1d8eaac66b938ecd8428f20 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 13:36:57 -0500 Subject: [PATCH 088/151] added INT and FLOAT2 --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 73d3fcd5..9b471c19 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -29,10 +29,10 @@ 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,realTime,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +30,realTime,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current -32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,realTime,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,realTime,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator 35,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 36,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator From 1bf3f86246d42028524e8ec43a72e56917344bf4 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 13:44:29 -0500 Subject: [PATCH 089/151] added voltage placeholders --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 9b471c19..8ac392a6 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -1,6 +1,6 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,realTime,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,realTime,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +0,realTime,BATT_A_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,realTime,BATT_B_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis @@ -42,8 +42,8 @@ 40,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 41,realTime,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator 42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received -43,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status -44,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +43,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status 45,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 46,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V 47,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected From 2641e3a01d9b398a4a82cb471a41933059e86eda Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 13:48:28 -0500 Subject: [PATCH 090/151] testing Angular Velocity --- afsk/main.c | 10 +++------- 1 file changed, 3 insertions(+), 7 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index fa852714..da882833 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1107,14 +1107,10 @@ if (payload == ON) gyroZ = atof(token); printf("gyroZ %f \n", gyroZ); } - -// xAngularVelocity = (-0.69)*(gyroX)*(gyroX) + 45.3 * (gyroX) + 2078; -// yAngularVelocity = (-0.69)*(gyroY)*(gyroY) + 45.3 * (gyroY) + 2078; -// zAngularVelocity = (-0.69)*(gyroZ)*(gyroZ) + 45.3 * (gyroZ) + 2078; - xAngularVelocity = 1 * (gyroX) + 2048; - yAngularVelocity = 1 * (gyroY) + 2048; - zAngularVelocity = 1 * (gyroZ) + 2048; +// xAngularVelocity = 1 * (gyroX) + 2048; +// yAngularVelocity = 1 * (gyroY) + 2048; +// zAngularVelocity = 1 * (gyroZ) + 2048; } encodeA(b, 0 + head_offset, batt_a_v); From 6aa8800f6e2bfa37908bb811c595e078b156198a Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 13:52:33 -0500 Subject: [PATCH 091/151] more testing --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index da882833..dc03c642 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -883,7 +883,7 @@ int get_tlm_fox() { int head_offset = 0; // int xAngularVelocity = (-0.69)*(-10)*(-10) + 45.3 * (-10) + 2078, yAngularVelocity = (-0.69)*(-6)*(-6) + 45.3 * (-6) + 2078, zAngularVelocity = (-0.69)*(6)*(6) + 45.3 * (6) + 2078; // XAxisAngularVelocity // int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0 - int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0 + int xAngularVelocity = 2048-100, yAngularVelocity = 2048-400, zAngularVelocity = 2048+150; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; int xAccel = 2048+100, yAccel = 2048-100, zAccel = 2048+500, temp = 224, pressure = 1000, altitude = 1000; int sensor1 = 0, sensor2 = 2048-3, sensor3 = 2048-1501; From 6430a5a4645fa904460a47a4e0ab10a2be4e870f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 13:55:39 -0500 Subject: [PATCH 092/151] fixed acceleration conversion --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 8ac392a6..4befc77a 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -2,9 +2,9 @@ 0,realTime,BATT_A_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,realTime,BATT_B_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis -4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,realTime,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current 7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature 8,realTime,posXv,12,V,cubesatsim_ina219_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage From e9ed60b3d44939e90c0b6abc0a6e890a3359bcb6 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:05:07 -0500 Subject: [PATCH 093/151] fixed angular velocity --- afsk/main.c | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index dc03c642..6c024b30 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -883,7 +883,7 @@ int get_tlm_fox() { int head_offset = 0; // int xAngularVelocity = (-0.69)*(-10)*(-10) + 45.3 * (-10) + 2078, yAngularVelocity = (-0.69)*(-6)*(-6) + 45.3 * (-6) + 2078, zAngularVelocity = (-0.69)*(6)*(6) + 45.3 * (6) + 2078; // XAxisAngularVelocity // int xAngularVelocity = 2078, yAngularVelocity = 2078, zAngularVelocity = 2078; // XAxisAngularVelocity Y and Z set to 0 - int xAngularVelocity = 2048-100, yAngularVelocity = 2048-400, zAngularVelocity = 2048+150; // XAxisAngularVelocity Y and Z set to 0 + int xAngularVelocity = 2048, yAngularVelocity = 2048, zAngularVelocity = 2048; // XAxisAngularVelocity Y and Z set to 0 int RXTemperature = 0; int xAccel = 2048+100, yAccel = 2048-100, zAccel = 2048+500, temp = 224, pressure = 1000, altitude = 1000; int sensor1 = 0, sensor2 = 2048-3, sensor3 = 2048-1501; @@ -1108,9 +1108,9 @@ if (payload == ON) printf("gyroZ %f \n", gyroZ); } -// xAngularVelocity = 1 * (gyroX) + 2048; -// yAngularVelocity = 1 * (gyroY) + 2048; -// zAngularVelocity = 1 * (gyroZ) + 2048; + xAngularVelocity = (int)(gyroX + 0.5) + 2048; + yAngularVelocity = (int)(gyroY + 0.5) + 2048; + zAngularVelocity = (int)(gyroZ + 0.5) + 2048; } encodeA(b, 0 + head_offset, batt_a_v); From 11ae669ac8663c5a687755948e57a62fbb174716 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:15:02 -0500 Subject: [PATCH 094/151] made rotation INT --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 4befc77a..32fe7edb 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -26,9 +26,9 @@ 24,realTime,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count 25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU -27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis -28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis -29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,realTime,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 From 4322b7c465701465664190dafb14dc8979ce933b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:15:29 -0500 Subject: [PATCH 095/151] made rotation INT --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 0d0a7f6c..f55bb6c3 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -26,9 +26,9 @@ 24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count 25,RT,RSSI,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU -27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis -28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis -29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,RT,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 From 6c2a65959b7ebcc16e21a77563edf71cf2f66e55 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:16:12 -0500 Subject: [PATCH 096/151] made unused voltages same conversion --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index f55bb6c3..d5a70060 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,6 +1,6 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +0,RT,BATT_A_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,RT,BATT_B_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) 2,RT,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis From 5bc57232499c58160f0aa95180982f96f366277f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:27:07 -0500 Subject: [PATCH 097/151] created from rttelemetry.csv --- .../CubeSatSim_PSK_wodtelemetry.csv | 61 +++++++++++++++++++ 1 file changed, 61 insertions(+) create mode 100644 spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv new file mode 100644 index 00000000..96d73dc8 --- /dev/null +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv @@ -0,0 +1,61 @@ +60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,WOD,BATT_A_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,WOD,BATT_B_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,WOD,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,WOD,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +6,WOD,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current +7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature +8,WOD,posXv,12,V,cubesatsim_ina219_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage +9,WOD,posYv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage +10,WOD,posZv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage +11,WOD,negXv,12,V,cubesatsim_ina219_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage +12,WOD,negYv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage +13,WOD,negZv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage +14,WOD,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current +15,WOD,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current +16,WOD,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current +17,WOD,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current +18,WOD,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current +19,WOD,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current +20,WOD,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage +21,WOD,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,WOD,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,WOD,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +24,WOD,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,WOD,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication +26,WOD,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU +27,WOD,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,WOD,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,WOD,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +30,WOD,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,WOD,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current +32,WOD,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,WOD,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +35,WOD,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +36,WOD,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator +37,WOD,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator +38,WOD,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator +39,WOD,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +40,WOD,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator +41,WOD,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +42,WOD,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received +43,WOD,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,WOD,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +45,WOD,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +46,WOD,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +47,WOD,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +48,WOD,rf6,12,-,0,NONE,0,0,0,None,None +49,WOD,rf7,12,-,0,NONE,0,0,0,None,None +50,WOD,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +51,WOD,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +52,WOD,pad,4,-,34,NONE,0,0,0,None,Unused +53,WOD,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +54,WOD,pad1,1,-,0,NONE,0,0,0,NONE,Filler +55,WOD,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +56,WOD,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +57,WOD,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset +58,WOD,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset +59,WOD,pad2,28,-,0,NONE,0,0,0,NONE,Filler From 018543fbb82042f02ead1efccff28debbd0c3981 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:29:20 -0500 Subject: [PATCH 098/151] changed to CubeSatSim_PSK_wodtelemetry.csv --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 665a316d..90b681c1 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -41,7 +41,7 @@ layout4.name=radtelemetry layout5.filename=FOX1E_radtelemetry2.csv layout5.name=radtelemetry2 layout5.parentLayout=radtelemetry -layout6.filename=FOX1E_wodtelemetry.csv +layout6.filename=CubeSatSim_PSK_wodtelemetry.csv layout6.name=wodtelemetry layout7.filename=FOX1E_wodradtelemetry.csv layout7.name=wodradtelemetry From 961f0de1acb67917d430d17fc3429c1f5a08935e Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:33:21 -0500 Subject: [PATCH 099/151] made sensor 2 INT --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index d5a70060..5dfd23d7 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -31,7 +31,7 @@ 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,RT,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current -32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +32,RT,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status 35,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) From e278c5e55411f0c854f71c78662695e5c4a09bed Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:41:06 -0500 Subject: [PATCH 100/151] added rpm and rssi conversions --- spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv | 2 ++ 1 file changed, 2 insertions(+) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv index 109b4f4e..ce790d69 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv @@ -9,3 +9,5 @@ cubesatsim_pressure,0,1,0,0,0,0,Converts pressure cubesatsim_sensor1,0,1,0,0,0,0,Conversion of Sensor 1 cubesatsim_sensor2,-2048,1,0,0,0,0,Conversion of Sensor 2 cubesatsim_sensor3,-20.48,0.01,0,0,0,0,Conversion of Sensor 3 +cubesatsim_rpm,-204.8,0.1,0,0,0,0,Conversion of calculated RPM +cubesatsim_rssi,-2048,1,0,0,0,0,Conversion of Received Signal Strength From 2b8436e8420a87be00f99954b6b512dacbf14559 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:42:22 -0500 Subject: [PATCH 101/151] changed rssi and rpm conversion --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 32fe7edb..5640c36a 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -20,11 +20,11 @@ 18,realTime,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current 19,realTime,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current 20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage -21,realTime,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +21,realTime,spin,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude 24,realTime,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,realTime,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication +25,realTime,rssi,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis From 080abbcef91c8467f1b3429b485f680de482b910 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 14:43:13 -0500 Subject: [PATCH 102/151] changed conversion of rssi and rpm --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 5dfd23d7..dbed4e59 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -20,11 +20,11 @@ 18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage -21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude 24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,RT,RSSI,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication +25,RT,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis From 13747df1a94529f3bdb0fddafa228eb47c9e0da7 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:06:30 -0500 Subject: [PATCH 103/151] changed antenna notes --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index dbed4e59..249b9442 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -42,6 +42,6 @@ 40,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 41,RT,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator 42,RT,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received -43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,70cm Antenna status -44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Antenna status +43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Transmit antenna status 45,RT,Pad,58,-,0,NONE,0,0,0,NONE,NONE From 8ce314cf76572f79d89896cc0a0bf1965c45182b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:30:22 -0500 Subject: [PATCH 104/151] removed ina219 in names and renamed --- ...conversion_curves.csv => CubeSatSim_conversion_curves.csv} | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) rename spacecraft/FoxTelem_1.09m/{cubesatsim_conversion_curves.csv => CubeSatSim_conversion_curves.csv} (76%) diff --git a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_conversion_curves.csv similarity index 76% rename from spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv rename to spacecraft/FoxTelem_1.09m/CubeSatSim_conversion_curves.csv index ce790d69..30f05985 100755 --- a/spacecraft/FoxTelem_1.09m/cubesatsim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_conversion_curves.csv @@ -1,6 +1,6 @@ CurveName,a,bx,cx^2,dx^3,ex^4,fx^5,Description -cubesatsim_ina219_voltage,0,0.01,0,0,0,0,Converts voltages read from the INA219 sensors -cubesatsim_ina219_current,-2048,1,0,0,0,0,Converts positive and negative currents read from the INA219 sensors +cubesatsim_voltage,0,0.01,0,0,0,0,Converts voltages read from the INA219 sensors +cubesatsim_current,-2048,1,0,0,0,0,Converts positive and negative currents read from the INA219 sensors cubesatsim_temperature,0,0.1,0,0,0,0,Converts temperature of Pi cubesatsim_rotation,-2048,1,0,0,0,0,Converts positive and negative dps rotation cubesatsim_acceleration,-20.48,0.01,0,0,0,0,Converts positive and negative g acceleration From b2311362fe0b7df061196e80b8eab7502434dcf7 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:38:48 -0500 Subject: [PATCH 105/151] minor edits and renames for I2C bus and Camera failures --- .../CubeSatSim_PSK_rttelemetry.csv | 74 +++++++++---------- 1 file changed, 37 insertions(+), 37 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 5640c36a..ad240148 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -1,49 +1,49 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,realTime,BATT_A_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,realTime,BATT_B_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,realTime,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +0,realTime,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis 5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis -6,realTime,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current -7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,realTime,posXv,12,V,cubesatsim_ina219_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage -9,realTime,posYv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage -10,realTime,posZv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage -11,realTime,negXv,12,V,cubesatsim_ina219_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage -12,realTime,negYv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage -13,realTime,negZv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage -14,realTime,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current -15,realTime,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current -16,realTime,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current -17,realTime,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current -18,realTime,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current -19,realTime,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current -20,realTime,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage +6,realTime,battCurr,12,mA,cubesatsim_current,Battery,4,2,4,Current,Total Battery DC current +7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload sensor temperature +8,realTime,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar panel voltage +9,realTime,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar panel voltage +10,realTime,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar panel voltage +11,realTime,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar panel voltage +12,realTime,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar panel voltage +13,realTime,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar panel voltage +14,realTime,posXi,12,mA,cubesatsim_current,+X Panel,7,2,4,Current,+X solar panel current +15,realTime,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,4,Current,+Y solar panel current +16,realTime,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,4,Current,+Z solar panel current +17,realTime,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar panel current +18,realTime,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar panel current +19,realTime,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,Current,-Z solar panel current +20,realTime,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply voltage 21,realTime,spin,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure -23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +22,realTime,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload sensor pressure +23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload sensor altitude 24,realTime,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count 25,realTime,rssi,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication -26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU -27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis -28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis -29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,realTime,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,realTime,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current -32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,realTime,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 -34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal temperature of IHU from Pi +27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular veolcity around X Axis +28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular veolcity around Y Axis +29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular veolcity around Z Axis +30,realTime,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload extra Sensor 1 +31,realTime,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current +32,realTime,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload extra Sensor 2 +33,realTime,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload extra Sensor 3 +34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload, STEM Payload STEM Payload board failure indicator 35,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) -36,realTime,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator -37,realTime,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator -38,realTime,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator -39,realTime,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator -40,realTime,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -41,realTime,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +36,realTime,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator +37,realTime,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator +38,realTime,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,Battery I2C,I2C bus 0 failure indicator +39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,I2C bus 1 failure indicator +40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,I2C bus 3 failure indicator +41,realTime,CameraFailure,1,-,17,NONE,2,5,0,RF I2C,Camera failure indicator 42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received -43,realTime,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status -44,realTime,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +43,realTime,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,realTime,TxAntenna,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status 45,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 46,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V 47,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected From 3c6398bf951635d53146ec56b92ee25098a44ad6 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:41:39 -0500 Subject: [PATCH 106/151] fixed I2C and Camera status --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 8 ++++---- 1 file changed, 4 insertions(+), 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index ad240148..28e9710e 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -37,10 +37,10 @@ 35,realTime,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 36,realTime,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator 37,realTime,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator -38,realTime,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,Battery I2C,I2C bus 0 failure indicator -39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,I2C bus 1 failure indicator -40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,I2C bus 3 failure indicator -41,realTime,CameraFailure,1,-,17,NONE,2,5,0,RF I2C,Camera failure indicator +38,realTime,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,realTime,CameraFailure,1,-,17,NONE,2,5,0,Camera,Camera failure indicator 42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received 43,realTime,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status 44,realTime,TxAntenna,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status From ab5d233fca96405efc93654239dfd980a9ddd5e8 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:44:33 -0500 Subject: [PATCH 107/151] display Camera status --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index 28e9710e..d57c6120 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -40,7 +40,7 @@ 38,realTime,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator 39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator 40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator -41,realTime,CameraFailure,1,-,17,NONE,2,5,0,Camera,Camera failure indicator +41,realTime,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator 42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received 43,realTime,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status 44,realTime,TxAntenna,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status From dab147c8c546368243b297a02d7bb14f89dcf19f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:45:42 -0500 Subject: [PATCH 108/151] updated I2C and Camera Failures --- .../FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv | 12 ++++++------ 1 file changed, 6 insertions(+), 6 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv index 96d73dc8..c989364e 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv @@ -35,12 +35,12 @@ 33,WOD,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator 35,WOD,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) -36,WOD,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator -37,WOD,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator -38,WOD,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator -39,WOD,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator -40,WOD,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -41,WOD,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +36,WOD,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator +37,WOD,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator +38,WOD,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,WOD,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,WOD,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,WOD,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator 42,WOD,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received 43,WOD,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status 44,WOD,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status From 5aed371e178a3514e63be53117b48ee31763ea5e Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:48:45 -0500 Subject: [PATCH 109/151] aligned with rtt --- .../CubeSatSim_PSK_wodtelemetry.csv | 36 +++++++++---------- 1 file changed, 18 insertions(+), 18 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv index c989364e..98f14859 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv @@ -1,25 +1,25 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,WOD,BATT_A_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,WOD,BATT_B_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,WOD,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,WOD,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis 5,WOD,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis -6,WOD,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current +6,WOD,battCurr,12,mA,cubesatsim_current,Battery,4,2,4,Current,Total Battery DC current 7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,WOD,posXv,12,V,cubesatsim_ina219_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage -9,WOD,posYv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage -10,WOD,posZv,12,V,cubesatsim_ina219_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage -11,WOD,negXv,12,V,cubesatsim_ina219_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage -12,WOD,negYv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage -13,WOD,negZv,12,V,cubesatsim_ina219_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage -14,WOD,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current -15,WOD,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current -16,WOD,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current -17,WOD,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current -18,WOD,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current -19,WOD,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current -20,WOD,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage +8,WOD,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage +9,WOD,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage +10,WOD,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage +11,WOD,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage +12,WOD,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage +13,WOD,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage +14,WOD,posXi,12,mA,cubesatsim_current,+X Panel,7,2,4,Current,+X solar Panel current +15,WOD,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,4,Current,+Y solar Panel current +16,WOD,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,4,Current,+Z solar Panel current +17,WOD,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar Panel current +18,WOD,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar Panel current +19,WOD,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,Current,-Z solar Panel current +20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage 21,WOD,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,WOD,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,WOD,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude @@ -30,7 +30,7 @@ 28,WOD,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,WOD,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,WOD,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,WOD,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current +31,WOD,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current 32,WOD,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,WOD,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator From 39f95b5a160eee26a79ed1a5a2c6032f8bd6d1b6 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:53:13 -0500 Subject: [PATCH 110/151] changed name of conversion curve --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 90b681c1..7edb7563 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -69,4 +69,4 @@ numberOfSources=1 source0.name=amsat.cubesat_simulator.ihu.bpsk user_format=0 useConversionCoeffs=true -conversionCurvesFileName=cubesatsim_conversion_curves.csv +conversionCurvesFileName=CubeSatsim_conversion_curves.csv From 054f79f3c10b864c0b1519d2cdf7378f0f8773a7 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 15:54:42 -0500 Subject: [PATCH 111/151] fixed filename --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER index 7edb7563..6b3132cd 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER @@ -69,4 +69,4 @@ numberOfSources=1 source0.name=amsat.cubesat_simulator.ihu.bpsk user_format=0 useConversionCoeffs=true -conversionCurvesFileName=CubeSatsim_conversion_curves.csv +conversionCurvesFileName=CubeSatSim_conversion_curves.csv From fd4a02eaca0be409dc292baeb081757bd97c7262 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:02:13 -0500 Subject: [PATCH 112/151] cleanup to align with rtt --- .../FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv | 10 +++++----- 1 file changed, 5 insertions(+), 5 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv index 98f14859..72288982 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv @@ -1,12 +1,12 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale) +1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery A+B voltage (0-3.3V scale) 2,WOD,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis 5,WOD,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis 6,WOD,battCurr,12,mA,cubesatsim_current,Battery,4,2,4,Current,Total Battery DC current -7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature +7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature 8,WOD,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage 9,WOD,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage 10,WOD,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage @@ -19,7 +19,7 @@ 17,WOD,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar Panel current 18,WOD,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar Panel current 19,WOD,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,Current,-Z solar Panel current -20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage +20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage 21,WOD,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,WOD,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,WOD,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude @@ -32,7 +32,7 @@ 30,WOD,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 31,WOD,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current 32,WOD,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,WOD,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +33,WOD,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator 35,WOD,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 36,WOD,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator From b6808b483cbb196747462adbefad95c104f9ea5d Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:02:50 -0500 Subject: [PATCH 113/151] cleanup --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index d57c6120..baeb7d15 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -1,6 +1,6 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,realTime,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +0,realTime,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale) +1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery A+B voltage (0-3.3V scale) 2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis From f178b4f0e1006520a11f57023647ddefd3c88b49 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:04:00 -0500 Subject: [PATCH 114/151] cleanup --- .../CubeSatSim_rttelemetryFM.csv | 52 +++++++++---------- 1 file changed, 26 insertions(+), 26 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index 249b9442..c2320aa9 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,25 +1,25 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,RT,BATT_A_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,RT,BATT_B_V,12,V,cubesatsim_ina219_voltage|FLOAT2,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,RT,BATT_V,12,V,cubesatsim_ina219_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +0,RT,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale) +1,RT,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A + B,Battery A+B voltage (0-3.3V scale) +2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis 5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis -6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,4,2,3,Current,Total Battery DC current -7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel -9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel -10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+YPanel -11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_ina219_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel -12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_ina219_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel -13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_ina219_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel -14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_ina219_current,+X Panel,7,2,3,Current,+X Panel -15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_ina219_current,-X Panel,10,2,3,Current,-X Panel -16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,3,Current,+Y Panel -17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,3,Current,-Y Panel -18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel -19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel -20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage +6,RT,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current +7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature +8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel +9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel +10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel +11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel +12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel +13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel +14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel +15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel +16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel +17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel +18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel +19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel +20,RT,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage 21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude @@ -30,18 +30,18 @@ 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 30,RT,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current +31,RT,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status 35,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) -36,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -37,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used -38,RT,BATTI2CFailureIndications,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator -39,RT,PSU1I2CFailureIndications,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator -40,RT,PSU2I2CFailureIndications,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -41,RT,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +36,RT,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator +37,RT,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator +38,RT,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,RT,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator 42,RT,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received 43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status -44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,2m Transmit antenna status +44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status 45,RT,Pad,58,-,0,NONE,0,0,0,NONE,NONE From 86f584cb4e2e7f8bfadabbbfe15f18df5ed4bc95 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:04:20 -0500 Subject: [PATCH 115/151] Update CubeSatSim_rttelemetryFM.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv index c2320aa9..d950ec24 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv @@ -1,6 +1,6 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,RT,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale) -1,RT,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A + B,Battery A+B voltage (0-3.3V scale) +1,RT,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale) 2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis From 3e45c2d54c197acde6a2d8fc1f70731c3c195132 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:04:35 -0500 Subject: [PATCH 116/151] Update CubeSatSim_PSK_rttelemetry.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv index baeb7d15..518a39ac 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_rttelemetry.csv @@ -1,6 +1,6 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,realTime,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale) -1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery A+B voltage (0-3.3V scale) +1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale) 2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis From 2298225e0dde3e7f2dcc9f3586d13846a3564e11 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:04:49 -0500 Subject: [PATCH 117/151] Update CubeSatSim_PSK_wodtelemetry.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv index 72288982..62084a60 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv @@ -1,6 +1,6 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale) -1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery A+B voltage (0-3.3V scale) +1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale) 2,WOD,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) 3,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis 4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis From 327a575b38273d755821f3c6c15962a2964178f5 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:08:08 -0500 Subject: [PATCH 118/151] Update and rename CubeSat_Simulator_DUV_fm.MASTER to CubeSat_Simulator_DUV.MASTER --- ...t_Simulator_DUV_fm.MASTER => CubeSat_Simulator_DUV.MASTER} | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) rename spacecraft/FoxTelem_1.09m/{CubeSat_Simulator_DUV_fm.MASTER => CubeSat_Simulator_DUV.MASTER} (91%) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER similarity index 91% rename from spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.MASTER rename to spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER index c1a90d35..d9284763 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER @@ -19,7 +19,7 @@ layout0.filename=FOX1A_debug.csv layout0.name=DEBUG layout1.filename=CubeSatSim_maxtelemetry.csv layout1.name=maxtelemetry -layout2.filename=CubeSatSim_rttelemetryFM.csv +layout2.filename=CubeSatSim_rttelemetry.csv layout2.name=rttelemetry layout3.filename=CubeSatSim_mintelemetry.csv layout3.name=mintelemetry @@ -51,4 +51,4 @@ useIHUVBatt=true user_mode=0 user_format=0 useConversionCoeffs=true -conversionCurvesFileName=cubesatsim_conversion_curves.csv +conversionCurvesFileName=CubeSatSim_conversion_curves.csv From 7e935531f9ca7eb1d82447d89e67f77a08f4ed98 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:08:24 -0500 Subject: [PATCH 119/151] Rename CubeSatSim_rttelemetryFM.csv to CubeSatSim_rttelemetry.csv --- .../{CubeSatSim_rttelemetryFM.csv => CubeSatSim_rttelemetry.csv} | 0 1 file changed, 0 insertions(+), 0 deletions(-) rename spacecraft/FoxTelem_1.09m/{CubeSatSim_rttelemetryFM.csv => CubeSatSim_rttelemetry.csv} (100%) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetry.csv similarity index 100% rename from spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv rename to spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetry.csv From 6b83d4e89d8818e3a453a4a899761983e9972887 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:14:18 -0500 Subject: [PATCH 120/151] Rename CubeSat_Simulator_PSK_fm.MASTER to CubeSat_Simulator_PSK.MASTER --- ...beSat_Simulator_PSK_fm.MASTER => CubeSat_Simulator_PSK.MASTER} | 0 1 file changed, 0 insertions(+), 0 deletions(-) rename spacecraft/FoxTelem_1.09m/{CubeSat_Simulator_PSK_fm.MASTER => CubeSat_Simulator_PSK.MASTER} (100%) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER similarity index 100% rename from spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.MASTER rename to spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER From 275be777482a8b910b121c9910c442e252cd48e6 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Fri, 27 Nov 2020 16:46:45 -0500 Subject: [PATCH 121/151] generated max and min from rtt --- .../CubeSatSim_PSK_maxtelemetry.csv | 113 ++++++++++-------- .../CubeSatSim_PSK_mintelemetry.csv | 113 ++++++++++-------- .../CubeSatSim_maxtelemetry.csv | 87 +++++++------- .../CubeSatSim_mintelemetry.csv | 87 +++++++------- 4 files changed, 216 insertions(+), 184 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv index 74f9a66e..8b8efd37 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv @@ -1,52 +1,61 @@ -51,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,MAX,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,MAX,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,MAX,BATT_C_V,12,V,4,NONE,4,3,3,Cell A + B + C,Battery pairs A+B+C voltage (0-5.0V scale) -3,MAX,battAtemp,12,C,8,NONE,4,4,3,Temperature A,Battery pair A temperature -4,MAX,battBtemp,12,C,8,NONE,4,5,3,Temperature B,Battery pair B temperature -5,MAX,battCtemp,12,C,8,NONE,4,6,3,Temperature C,Battery pair C temperature -6,MAX,battCurr,12,mA,9,NONE,4,7,3,Current,Total Battery DC current -7,MAX,battCardTemp,12,C,8,NONE,4,8,3,Board Temp,Battery Card Temperature -8,MAX,posXv,12,V,23,NONE,8,1,3,Voltage,+X solar Panel voltage -9,MAX,posYv,12,V,23,NONE,9,1,3,Voltage,+Y solar Panel voltage -10,MAX,posZv,12,V,23,NONE,10,1,3,Voltage,+Z solar Panel voltage -11,MAX,negXv,12,V,23,NONE,11,1,3,Voltage,-X solar Panel voltage -12,MAX,negYv,12,V,23,NONE,12,1,3,Voltage,-Y solar Panel voltage -13,MAX,negZv,12,V,23,NONE,13,1,3,Voltage,-Z solar Panel voltage -14,MAX,posXt,12,C,24,NONE,8,2,3,Temp,+X solar Panel temperature -15,MAX,posYt,12,C,24,NONE,9,2,3,Temp,+Y solar Panel temperature -16,MAX,posZt,12,C,24,NONE,10,2,3,Temp,+Z solar Panel temperature -17,MAX,negXt,12,C,24,NONE,11,2,3,Temp,-X solar Panel temperature -18,MAX,negYt,12,C,24,NONE,12,2,3,Temp,-Y solar Panel temperature -19,MAX,negZt,12,C,24,NONE,13,2,3,Temp,-Z solar Panel temperature -20,MAX,PSUTemp,12,C,8,NONE,5,2,3,Board Temp,Power Supply Card Temperature -21,MAX,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,MAX,TxPAi,12,mA,38,NONE,1,2,3,PA Current,Transmit power amplifier current -23,MAX,TxTemp,12,C,37,NONE,1,1,3,TX Temperature,Transmitter card temperature -24,MAX,FwdPower,12,mW,40,NONE,1,4,3,Fwd Power,Receiver card temperature -25,MAX,rssi,12,dBm,14,NONE,1,3,3,RSSI,Received Signal Strength Indication -26,MAX,IHUcpuTemp,12,C,15,NONE,2,1,3,Temperature,Internal Temperature of IHU -27,MAX,SatelliteXAxisAngularVelocity,12,dps,13,NONE,8,3,3,Rotation,Angular Veolcity around X Axis -28,MAX,SatelliteYAxisAngularVelocity,12,dps,13,NONE,9,3,3,Rotation,Angular Veolcity around Y Axis -29,MAX,SatelliteZAxisAngularVelocity,12,dps,13,NONE,10,3,3,Rotation,Angular Veolcity around Z Axis -30,MAX,Exp4Temp,12,C,7,NONE,6,1,3,EXP4 Temp,Experiment 4 card temperature -31,MAX,PSUCurrent,12,mA,22,NONE,5,1,3,Current,Power Supply DC Current -32,MAX,ReflectedPwr,12,mW,41,NONE,1,5,3,Ref Power,Reflected Power from the Transmit Antenna -33,MAX,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V -34,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted -35,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V -36,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected -37,MAX,rf6,12,-,0,NONE,0,0,0,None,None -38,MAX,rf7,12,-,0,NONE,0,0,0,None,None -39,MAX,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR -40,MAX,LtVGACtl,12,V,42,NONE,1,6,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) -41,MAX,pad,4,-,34,NONE,0,0,0,None,Unused -42,MAX,IHUhardError,32,-,19,NONE,2,7,0,IHU Hard Error Data,Reason for last reset -43,MAX,maxTimestampReset,16,s,1,NONE,0,0,0,MAX Timestamp Reset Count,Timestamp of last max change -44,MAX,maxTimestampUptime,25,s,1,NONE,0,0,0,MAX Timestamp Uptime,Timestamp of last max change -45,MAX,SafeModeIndication,1,-,21,NONE,3,4,0,Safe Mode,In safe mode? -46,MAX,AutoSafeModeActive,1,-,21,NONE,3,5,0,Auto Safe Mode,In Autosafe mode? -47,MAX,AutoSafeModeAllowed,1,-,21,NONE,3,6,0,Auto Safe Allowed,Autosafe enabled? -48,MAX,ScienceModeActive,1,-,21,NONE,3,7,0,Science Mode,In Science Mode? -49,MAX,pad1,19,-,0,NONE,0,0,0,NONE,Make it even -50,MAX,pad2,32,-,0,NONE,0,0,0,NONE,- +60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,MIN,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +6,MIN,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current +7,MIN,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature +8,MIN,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage +9,MIN,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage +10,MIN,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage +11,MIN,negXv,12,V,cubesatsim_ina219_voltage,-X Panel,10,1,3,Voltage,-X solar Panel voltage +12,MIN,negYv,12,V,cubesatsim_ina219_voltage,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage +13,MIN,negZv,12,V,cubesatsim_ina219_voltage,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage +14,MIN,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current +15,MIN,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current +16,MIN,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current +17,MIN,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current +18,MIN,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current +19,MIN,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current +20,MIN,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage +21,MIN,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MIN,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MIN,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,MIN,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication +26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU +27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MIN,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MIN,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current +32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +37,MIN,rf6,12,-,0,NONE,0,0,0,None,None +38,MIN,rf7,12,-,0,NONE,0,0,0,None,None +39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +40,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused +42,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +43,MIN,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +44,MIN,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +45,MIN,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator +46,MIN,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator +47,MIN,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator +48,MIN,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +49,MIN,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator +50,MIN,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +51,MIN,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status +52,MIN,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +53,MIN,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +54,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler +55,MIN,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +56,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +57,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset +58,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset +59,MIN,pad2,28,-,0,NONE,0,0,0,NONE,Filler diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv index 89fe9a7a..8b8efd37 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv @@ -1,52 +1,61 @@ -51,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,MIN,BATT_C_V,12,V,4,NONE,4,3,3,Cell A + B + C,Battery pairs A+B+C voltage (0-5.0V scale) -3,MIN,battAtemp,12,C,8,NONE,4,4,3,Temperature A,Battery pair A temperature -4,MIN,battBtemp,12,C,8,NONE,4,5,3,Temperature B,Battery pair B temperature -5,MIN,battCtemp,12,C,8,NONE,4,6,3,Temperature C,Battery pair C temperature -6,MIN,battCurr,12,mA,9,NONE,4,7,3,Current,Total Battery DC current -7,MIN,battCardTemp,12,C,8,NONE,4,8,3,Board Temp,Battery Card Temperature -8,MIN,posXv,12,V,23,NONE,8,1,3,Voltage,+X solar Panel voltage -9,MIN,posYv,12,V,23,NONE,9,1,3,Voltage,+Y solar Panel voltage -10,MIN,posZv,12,V,23,NONE,10,1,3,Voltage,+Z solar Panel voltage -11,MIN,negXv,12,V,23,NONE,11,1,3,Voltage,-X solar Panel voltage -12,MIN,negYv,12,V,23,NONE,12,1,3,Voltage,-Y solar Panel voltage -13,MIN,negZv,12,V,23,NONE,13,1,3,Voltage,-Z solar Panel voltage -14,MIN,posXt,12,C,24,NONE,8,2,3,Temp,+X solar Panel temperature -15,MIN,posYt,12,C,24,NONE,9,2,3,Temp,+Y solar Panel temperature -16,MIN,posZt,12,C,24,NONE,10,2,3,Temp,+Z solar Panel temperature -17,MIN,negXt,12,C,24,NONE,11,2,3,Temp,-X solar Panel temperature -18,MIN,negYt,12,C,24,NONE,12,2,3,Temp,-Y solar Panel temperature -19,MIN,negZt,12,C,24,NONE,13,2,3,Temp,-Z solar Panel temperature -20,MIN,PSUTemp,12,C,8,NONE,5,2,3,Board Temp,Power Supply Card Temperature -21,MIN,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,MIN,TxPAi,12,mA,38,NONE,1,2,3,PA Current,Transmit power amplifier current -23,MIN,TxTemp,12,C,37,NONE,1,1,3,TX Temperature,Transmitter card temperature -24,MIN,FwdPower,12,mW,40,NONE,1,4,3,Fwd Power,Receiver card temperature -25,MIN,rssi,12,dBm,14,NONE,1,3,3,RSSI,Received Signal Strength Indication -26,MIN,IHUcpuTemp,12,C,15,NONE,2,1,3,Temperature,Internal Temperature of IHU -27,MIN,SatelliteXAxisAngularVelocity,12,dps,13,NONE,8,3,3,Rotation,Angular Veolcity around X Axis -28,MIN,SatelliteYAxisAngularVelocity,12,dps,13,NONE,9,3,3,Rotation,Angular Veolcity around Y Axis -29,MIN,SatelliteZAxisAngularVelocity,12,dps,13,NONE,10,3,3,Rotation,Angular Veolcity around Z Axis -30,MIN,Exp4Temp,12,C,7,NONE,6,1,3,EXP4 Temp,Experiment 4 card temperature -31,MIN,PSUCurrent,12,mA,22,NONE,5,1,3,Current,Power Supply DC Current -32,MIN,ReflectedPwr,12,mW,41,NONE,1,5,3,Ref Power,Reflected Power from the Transmit Antenna -33,MIN,ICR3V,12,V,43,NONE,7,1,3,3V,ICR 3V -34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted -35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V -36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected -37,MIN,rf6,12,-,0,NONE,0,0,0,None,None -38,MIN,rf7,12,-,0,NONE,0,0,0,None,None -39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR -40,MIN,LtVGACtl,12,V,42,NONE,1,6,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) -41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused -42,MIN,IHUsoftError,32,-,39,NONE,3,8,0,Soft Error,Diagnostic Data on IHU Software Errors -43,MIN,minTimestampReset,16,s,1,NONE,0,0,0,NONE,Timestamp Resets -44,MIN,minTimestampUptime,25,s,1,NONE,0,0,0,NONE,Timestamp uptime -45,MIN,SafeModeIndication,1,-,21,NONE,0,0,0,NONE,In safe mode? -46,MIN,AutoSafeModeActive,1,-,21,NONE,0,0,0,NONE,In Autosafe mode? -47,MIN,AutoSafeModeAllowed,1,-,21,NONE,0,0,0,NONE,Autosafe enabled? -48,MIN,ScienceModeActive,1,-,21,NONE,0,0,0,Science Mode,In Science Mode? -49,MIN,pad1,19,-,0,NONE,0,0,0,NONE,Make it even -50,MIN,pad2,32,-,0,NONE,0,0,0,NONE,Make it even +60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,MIN,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +6,MIN,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current +7,MIN,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature +8,MIN,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage +9,MIN,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage +10,MIN,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage +11,MIN,negXv,12,V,cubesatsim_ina219_voltage,-X Panel,10,1,3,Voltage,-X solar Panel voltage +12,MIN,negYv,12,V,cubesatsim_ina219_voltage,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage +13,MIN,negZv,12,V,cubesatsim_ina219_voltage,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage +14,MIN,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current +15,MIN,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current +16,MIN,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current +17,MIN,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current +18,MIN,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current +19,MIN,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current +20,MIN,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage +21,MIN,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MIN,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MIN,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,MIN,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication +26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU +27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MIN,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MIN,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current +32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +37,MIN,rf6,12,-,0,NONE,0,0,0,None,None +38,MIN,rf7,12,-,0,NONE,0,0,0,None,None +39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +40,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused +42,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +43,MIN,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +44,MIN,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +45,MIN,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator +46,MIN,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator +47,MIN,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator +48,MIN,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +49,MIN,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator +50,MIN,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +51,MIN,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status +52,MIN,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +53,MIN,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +54,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler +55,MIN,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +56,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +57,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset +58,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset +59,MIN,pad2,28,-,0,NONE,0,0,0,NONE,Filler diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv index adbb8b06..68bb086a 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv @@ -1,40 +1,47 @@ -39,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,MAX,BATT_A_V,12,V,4,NONE,0,0,0,NONE,Battery pair A high voltage raw value (0-2.5V scale) -1,MAX,BATT_B_V,12,V,4,NONE,0,0,0,NONE,Battery pair B high voltage raw value (0-3.3V scale) -2,MAX,BATT_C_V,12,V,4,NONE,0,0,0,NONE,Battery pair C high voltage raw value (0-5.0V scale) -3,MAX,BATT_A_T,12,C,8,NONE,0,0,0,NONE,Battery pair A high temperature raw value -4,MAX,BATT_B_T,12,C,8,NONE,0,0,0,NONE,Battery pair B high temperature raw value -5,MAX,BATT_C_T,12,C,8,NONE,0,0,0,NONE,Battery pair C high temperature raw value -6,MAX,TOTAL_BATT_I,12,mA,9,NONE,0,0,0,NONE,Battery DC high current raw value -7,MAX,BATTBoardTemperature,12,C,8,NONE,0,0,0,NONE,High PC Board Temperature of BATT raw value -8,MAX,PANEL_PLUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME? -9,MAX,PANEL_MINUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME? -10,MAX,PANEL_PLUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME? -11,MAX,PANEL_MINUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME? -12,MAX,PANEL_PLUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME? -13,MAX,PANEL_MINUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME? -14,MAX,PANEL_PLUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME? -15,MAX,PANEL_MINUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME? -16,MAX,PANEL_PLUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME? -17,MAX,PANEL_MINUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME? -18,MAX,PANEL_PLUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME? -19,MAX,PANEL_MINUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME? -20,MAX,PSUTemperature,12,C,7,NONE,0,0,0,NONE,PSU card high temperature raw value -21,MAX,SPIN,12,rpm,12,NONE,0,0,0,NONE,Highest calculated spin rate RPM using solar cells -22,MAX,TXPACurrent,12,mA,10,NONE,0,0,0,NONE,Transmit power amplifier high current raw value -23,MAX,TXTemperature,12,C,7,NONE,0,0,0,NONE,Transmitter card high temperature raw value -24,MAX,RXTemperature,12,C,7,NONE,0,0,0,NONE,Receiver card high temperature raw value -25,MAX,RSSI,12,dBm,14,NONE,0,0,0,NONE,High Received Signal Strength Indication raw value -26,MAX,IHUTemperature,12,C,15,NONE,0,0,0,NONE,High CPU Temperature of IHU raw value -27,MAX,SatelliteXAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Highest Raw Angle -28,MAX,SatelliteYAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Highest Raw Angle -29,MAX,SatelliteZAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Highest Raw Angle -30,MAX,EXP4Temperature,12,C,7,NONE,0,0,0,NONE,LBand Uplink card temperature raw value -31,MAX,PSUCurrent,12,mA,22,NONE,0,0,0,NONE,PSU DC high current -32,MAX,IHUHardErrorData,32,-,19,NONE,2,8,0,Hard Error,Diagnostic Data on IHU Hard Errors -33,MAX,MaxTimestampResetCount,16,-,1,NONE,0,0,0,NONE,Total number of times IHU has reset since initial on-orbit startup -34,MAX,MaxTimestampUptime,25,-,1,NONE,0,0,0,NONE,This is the IHU uptime in seconds since the last reset -35,MAX,SafeModeIndication,1,-,21,NONE,2,10,0,Safe Mode,State: 1 = Safe Mode Active -36,MAX,AutoSafeModeActive,1,-,21,NONE,2,11,0,Auto Safe Mode,State: 1 = Auto Safe Mode Active -37,MAX,AutoSafeModeAllowed,1,-,21,NONE,2,12,0,Auto Safe Allowed,State: 1 = Auto Safe Mode Allowed -38,MAX,Pad,20,-,0,NONE,0,0,0,NONE,NONE +46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMAX_NAME,DESCRIPTION +0,MAX,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale) +1,MAX,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale) +2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +6,MAX,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current +7,MAX,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature +8,MAX,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel +9,MAX,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel +10,MAX,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel +11,MAX,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel +12,MAX,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel +13,MAX,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel +14,MAX,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel +15,MAX,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel +16,MAX,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel +17,MAX,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel +18,MAX,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel +19,MAX,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel +20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage +21,MAX,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MAX,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MAX,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,MAX,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication +26,MAX,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU +27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MAX,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MAX,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current +32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MAX,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,MAX,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status +35,MAX,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +36,MAX,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator +37,MAX,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator +38,MAX,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,MAX,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,MAX,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,MAX,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator +42,MAX,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received +43,MAX,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,MAX,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +45,MAX,Pad,58,-,0,NONE,0,0,0,NONE,NONE diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv index 573cad76..49ed51e1 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv @@ -1,40 +1,47 @@ -39,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,MIN,BATT_A_V,12,V,4,NONE,0,0,0,NONE,Battery pair A low voltage raw value (0-2.5V scale) -1,MIN,BATT_B_V,12,V,4,NONE,0,0,0,NONE,Battery pair B low voltage raw value (0-3.3V scale) -2,MIN,BATT_C_V,12,V,4,NONE,0,0,0,NONE,Battery pair C low voltage raw value (0-5.0V scale) -3,MIN,BATT_A_T,12,T,8,NONE,0,0,0,NONE,Battery pair A low temperature raw value -4,MIN,BATT_B_T,12,T,8,NONE,0,0,0,NONE,Battery pair B low temperature raw value -5,MIN,BATT_C_T,12,T,8,NONE,0,0,0,NONE,Battery pair C low temperature raw value -6,MIN,TOTAL_BATT_I,12,mA,9,NONE,0,0,0,NONE,Battery DC low current raw value -7,MIN,BATTBoardTemperature,12,C,8,NONE,0,0,0,NONE,Low PC Board Temperature of BATT raw value -8,MIN,PANEL_PLUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME? -9,MIN,PANEL_MINUS_X_V,12,V,5,NONE,0,0,0,NONE,#NAME? -10,MIN,PANEL_PLUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME? -11,MIN,PANEL_MINUS_Y_V,12,V,5,NONE,0,0,0,NONE,#NAME? -12,MIN,PANEL_PLUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME? -13,MIN,PANEL_MINUS_Z_V,12,V,5,NONE,0,0,0,NONE,#NAME? -14,MIN,PANEL_PLUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME? -15,MIN,PANEL_MINUS_X_T,12,C,6,NONE,0,0,0,NONE,#NAME? -16,MIN,PANEL_PLUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME? -17,MIN,PANEL_MINUS_Y_T,12,C,6,NONE,0,0,0,NONE,#NAME? -18,MIN,PANEL_PLUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME? -19,MIN,PANEL_MINUS_Z_T,12,C,6,NONE,0,0,0,NONE,#NAME? -20,MIN,PSUTemperature,12,C,7,NONE,0,0,0,NONE,PSU card low temperature raw value -21,MIN,SPIN,12,rpm,12,NONE,0,0,0,NONE,Lowest calculated spin rate RPM using solar cells -22,MIN,TXPACurrent,12,mA,10,NONE,0,0,0,NONE,Transmit power amplifier low current raw value -23,MIN,TXTemperature,12,C,7,NONE,0,0,0,NONE,Transmitter card low temperature raw value -24,MIN,RXTemperature,12,C,7,NONE,0,0,0,NONE,Receiver card low temperature raw value -25,MIN,RSSI,12,dBm,14,NONE,0,0,0,NONE,Low Received Signal Strength Indication raw value -26,MIN,IHUTemperature,12,C,15,NONE,0,0,0,NONE,Low CPU Temperature of IHU raw value -27,MIN,SatelliteXAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Lowest Raw Angle -28,MIN,SatelliteYAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Lowest Raw Angle -29,MIN,SatelliteZAxisAngularVelocity,12,dps,13,NONE,0,0,0,NONE,Lowest Raw Angle -30,MIN,EXP4Temperature,12,C,7,NONE,0,0,0,NONE,Experiment 4 card low temperature raw value -31,MIN,PSUCurrent,12,mA,11,NONE,0,0,0,NONE,PSU DC low current -32,MIN,IHUSoftErrorData,32,-,20,NONE,2,9,0,Soft Error,Diagnostic Data on IHU Soft Errors -33,MIN,MinTimestampResetCount,16,-,1,NONE,0,0,0,NONE,Total number of times IHU has reset since initial on-orbit startup -34,MIN,MinTimestampUptime,25,-,1,NONE,0,0,0,NONE,This is the IHU uptime in seconds since the last reset -35,MIN,SafeModeIndication,1,-,21,NONE,0,0,0,NONE,State: 1 = Safe Mode Active -36,MIN,AutoSafeModeActive,1,-,21,NONE,0,0,0,NONE,State: 1 = Auto Safe Mode Active -37,MIN,AutoSafeModeAllowed,1,-,21,NONE,0,0,0,NONE,State: 1 = Auto Safe Mode Allowed -38,MIN,Pad,20,-,0,NONE,0,0,0,NONE,NONE +46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMIN_NAME,DESCRIPTION +0,MIN,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale) +1,MIN,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale) +2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +6,MIN,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current +7,MIN,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature +8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel +9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel +10,MIN,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel +11,MIN,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel +12,MIN,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel +13,MIN,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel +14,MIN,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel +15,MIN,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel +16,MIN,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel +17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel +18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel +19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel +20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage +21,MIN,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MIN,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MIN,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,MIN,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication +26,MIN,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU +27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MIN,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MIN,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current +32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MIN,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,MIN,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status +35,MIN,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +36,MIN,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator +37,MIN,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator +38,MIN,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,MIN,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,MIN,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,MIN,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator +42,MIN,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received +43,MIN,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,MIN,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +45,MIN,Pad,58,-,0,NONE,0,0,0,NONE,NONE From e68af88d5fb795d0283ee202c32c4ccdeeefbdf2 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:54:34 -0500 Subject: [PATCH 122/151] Delete CubeSat_Simulator_DUV_fm.dat --- .../FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.dat | 15 --------------- 1 file changed, 15 deletions(-) delete mode 100644 spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.dat diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.dat b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.dat deleted file mode 100644 index 32d452e8..00000000 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV_fm.dat +++ /dev/null @@ -1,15 +0,0 @@ -#Fox 1 Telemetry Decoder User Spacecraft Properties -#Wed Nov 25 09:31:53 EST 2020 -hasModeInHeader=false -maxFreqBoundkHz=434950.0 -displayName=CubeSatSim-FSK -minFreqBoundkHz=434850.0 -priority=1 -memsRestValueY=2101 -memsRestValueZ=2045 -user_format=0 -memsRestValueX=2087 -name=CubeSatSim -track=true -telemetryDownlinkFreqkHz=434900.0 -BATTERY_CURRENT_ZERO=-1.839 From 5583b3433d822adf33e95fa84ffa82bcb558856f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 16:54:43 -0500 Subject: [PATCH 123/151] Delete CubeSat_Simulator_PSK_fm.dat --- .../FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.dat | 17 ----------------- 1 file changed, 17 deletions(-) delete mode 100644 spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.dat diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.dat b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.dat deleted file mode 100644 index dca5d27b..00000000 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK_fm.dat +++ /dev/null @@ -1,17 +0,0 @@ -#Fox 1 Telemetry Decoder User Spacecraft Properties -#Wed Nov 25 09:32:32 EST 2020 -hasModeInHeader=false -maxFreqBoundkHz=434950.0 -mpptSensorOffThreshold=1600 -displayName=CubeSatSim-BPSK -minFreqBoundkHz=434850.0 -mpptResistanceError=6.58 -priority=1 -memsRestValueY=2131 -memsRestValueZ=2103 -user_format=0 -memsRestValueX=2129 -name=CubeSatSim -track=false -telemetryDownlinkFreqkHz=434900.0 -BATTERY_CURRENT_ZERO=-1.834 From f42bcc4b95d13350b9f6360dbd35d3961966d81c Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 17:12:59 -0500 Subject: [PATCH 124/151] recreated from 1.09m --- .../FoxTelem_1.09m/CubeSat_Simulator_DUV.dat | 15 +++++++++++++++ 1 file changed, 15 insertions(+) create mode 100644 spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat new file mode 100644 index 00000000..32d452e8 --- /dev/null +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat @@ -0,0 +1,15 @@ +#Fox 1 Telemetry Decoder User Spacecraft Properties +#Wed Nov 25 09:31:53 EST 2020 +hasModeInHeader=false +maxFreqBoundkHz=434950.0 +displayName=CubeSatSim-FSK +minFreqBoundkHz=434850.0 +priority=1 +memsRestValueY=2101 +memsRestValueZ=2045 +user_format=0 +memsRestValueX=2087 +name=CubeSatSim +track=true +telemetryDownlinkFreqkHz=434900.0 +BATTERY_CURRENT_ZERO=-1.839 From 42fe3cf78c5ef9d646e97552e09a125858b48d4e Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 17:13:58 -0500 Subject: [PATCH 125/151] recreated from 1.09m --- .../FoxTelem_1.09m/CubeSat_Simulator_PSK.dat | 17 +++++++++++++++++ 1 file changed, 17 insertions(+) create mode 100644 spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.dat diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.dat b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.dat new file mode 100644 index 00000000..dca5d27b --- /dev/null +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.dat @@ -0,0 +1,17 @@ +#Fox 1 Telemetry Decoder User Spacecraft Properties +#Wed Nov 25 09:32:32 EST 2020 +hasModeInHeader=false +maxFreqBoundkHz=434950.0 +mpptSensorOffThreshold=1600 +displayName=CubeSatSim-BPSK +minFreqBoundkHz=434850.0 +mpptResistanceError=6.58 +priority=1 +memsRestValueY=2131 +memsRestValueZ=2103 +user_format=0 +memsRestValueX=2129 +name=CubeSatSim +track=false +telemetryDownlinkFreqkHz=434900.0 +BATTERY_CURRENT_ZERO=-1.834 From 338ea6de2b8205858d271e49dca21a0322c695a3 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 17:41:08 -0500 Subject: [PATCH 126/151] changed everything to NONE --- .../CubeSatSim_mintelemetry.csv | 80 +++++++++---------- 1 file changed, 40 insertions(+), 40 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv index 49ed51e1..f09e5349 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_mintelemetry.csv @@ -1,47 +1,47 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMIN_NAME,DESCRIPTION 0,MIN,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale) 1,MIN,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale) -2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis -4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis -6,MIN,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current -7,MIN,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature -8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel -9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel -10,MIN,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel -11,MIN,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel -12,MIN,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel -13,MIN,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel -14,MIN,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel -15,MIN,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel -16,MIN,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel -17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel -18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel -19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel -20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage -21,MIN,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,MIN,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure -23,MIN,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis +4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis +5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis +6,MIN,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current +7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature +8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel +9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel +10,MIN,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y Panel +11,MIN,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y Panel +12,MIN,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z Panel +13,MIN,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z Panel +14,MIN,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X Panel +15,MIN,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X Panel +16,MIN,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y Panel +17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel +18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel +19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel +20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Voltage,Power Supply Voltage +21,MIN,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MIN,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude 24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,MIN,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication -26,MIN,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU -27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis -28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis -29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,MIN,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,MIN,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current -32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,MIN,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 -34,MIN,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status -35,MIN,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +25,MIN,RSSI,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication +26,MIN,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU +27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,Angular Veolcity around X Axis +28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MIN,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current +32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MIN,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status +35,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 36,MIN,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator 37,MIN,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator -38,MIN,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator -39,MIN,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator -40,MIN,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator -41,MIN,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator -42,MIN,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received -43,MIN,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status -44,MIN,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +38,MIN,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,MIN,I2CBus1Failure,1,-,17,NONE,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,MIN,I2CBus3Failure,1,-,17,NONE,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,MIN,CameraFailure,1,-,17,NONE,2,5,0,Camera,Camera failure indicator +42,MIN,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received +43,MIN,RXAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status +44,MIN,TXAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status 45,MIN,Pad,58,-,0,NONE,0,0,0,NONE,NONE From 081a2bc9336cadbc2a5f22000844f31e3cd1ed3b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 17:43:45 -0500 Subject: [PATCH 127/151] changed all to NONE --- .../CubeSatSim_maxtelemetry.csv | 80 +++++++++---------- 1 file changed, 40 insertions(+), 40 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv index 68bb086a..b8440ecd 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_maxtelemetry.csv @@ -1,47 +1,47 @@ 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMAX_NAME,DESCRIPTION 0,MAX,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale) 1,MAX,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale) -2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis -4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis -6,MAX,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current -7,MAX,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature -8,MAX,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel -9,MAX,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel -10,MAX,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel -11,MAX,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel -12,MAX,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel -13,MAX,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel -14,MAX,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel -15,MAX,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel -16,MAX,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel -17,MAX,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel -18,MAX,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel -19,MAX,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel -20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage -21,MAX,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,MAX,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure -23,MAX,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis +4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis +5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis +6,MAX,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current +7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature +8,MAX,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel +9,MAX,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel +10,MAX,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y Panel +11,MAX,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y Panel +12,MAX,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z Panel +13,MAX,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z Panel +14,MAX,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X Panel +15,MAX,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X Panel +16,MAX,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y Panel +17,MAX,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel +18,MAX,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel +19,MAX,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel +20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Voltage,Power Supply Voltage +21,MAX,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MAX,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude 24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,MAX,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication -26,MAX,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU -27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis -28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis -29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,MAX,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,MAX,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current -32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,MAX,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 -34,MAX,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status -35,MAX,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +25,MAX,RSSI,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication +26,MAX,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU +27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,Angular Veolcity around X Axis +28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MAX,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current +32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MAX,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status +35,MAX,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 36,MAX,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator 37,MAX,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator -38,MAX,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator -39,MAX,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator -40,MAX,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator -41,MAX,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator -42,MAX,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received -43,MAX,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status -44,MAX,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +38,MAX,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,MAX,I2CBus1Failure,1,-,17,NONE,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,MAX,I2CBus3Failure,1,-,17,NONE,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,MAX,CameraFailure,1,-,17,NONE,2,5,0,Camera,Camera failure indicator +42,MAX,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received +43,MAX,RXAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status +44,MAX,TXAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status 45,MAX,Pad,58,-,0,NONE,0,0,0,NONE,NONE From 7d83dc66888c67b8fc85c8ea374ce36c7b024c5f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 17:50:00 -0500 Subject: [PATCH 128/151] changed all to NONE --- .../CubeSatSim_PSK_mintelemetry.csv | 76 +++++++++---------- 1 file changed, 38 insertions(+), 38 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv index 8b8efd37..d1bcb2aa 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv @@ -1,38 +1,38 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,MIN,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis -4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis -6,MIN,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current -7,MIN,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,MIN,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage -9,MIN,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage -10,MIN,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage -11,MIN,negXv,12,V,cubesatsim_ina219_voltage,-X Panel,10,1,3,Voltage,-X solar Panel voltage -12,MIN,negYv,12,V,cubesatsim_ina219_voltage,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage -13,MIN,negZv,12,V,cubesatsim_ina219_voltage,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage -14,MIN,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current -15,MIN,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current -16,MIN,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current -17,MIN,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current -18,MIN,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current -19,MIN,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current -20,MIN,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage -21,MIN,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,MIN,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure -23,MIN,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +2,MIN,BATT_V,12,V,cubesatsim_ina219_voltage,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,NONE,7,4,3,Acceleration,Acceleration around X Axis +4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,NONE,8,4,3,Acceleration,Acceleration around Y Axis +5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,NONE,9,4,3,Acceleration,Acceleration around Z Axis +6,MIN,battCurr,12,mA,cubesatsim_ina219_current,NONE,4,2,4,Current,Total Battery DC current +7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature +8,MIN,posXv,12,V,cubesatsim_ina219_voltage,NONE,7,1,3,Voltage,+X solar Panel voltage +9,MIN,posYv,12,V,cubesatsim_ina219_voltage,NONE,8,1,3,Voltage,+Y solar Panel voltage +10,MIN,posZv,12,V,cubesatsim_ina219_voltage,NONE,9,1,3,Voltage,+Z solar Panel voltage +11,MIN,negXv,12,V,cubesatsim_ina219_voltage,NONE,10,1,3,Voltage,-X solar Panel voltage +12,MIN,negYv,12,V,cubesatsim_ina219_voltage,NONE,11,1,3,Voltage,-Y solar Panel voltage +13,MIN,negZv,12,V,cubesatsim_ina219_voltage,NONE,12,1,3,Voltage,-Z solar Panel voltage +14,MIN,posXi,12,mA,cubesatsim_ina219_current,NONE,7,2,4,Current,+X solar Panel current +15,MIN,posYi,12,mA,cubesatsim_ina219_current,NONE,8,2,4,Current,+Y solar Panel current +16,MIN,posZi,12,mA,cubesatsim_ina219_current,NONE,9,2,4,Current,+Z solar Panel current +17,MIN,negXi,12,mA,cubesatsim_ina219_current,NONE,10,2,4,Current,-X solar Panel current +18,MIN,negYi,12,mA,cubesatsim_ina219_current,NONE,11,2,4,Current,-Y solar Panel current +19,MIN,negZi,12,mA,cubesatsim_ina219_current,NONE,12,2,4,Current,-Z solar Panel current +20,MIN,PSUVoltage,12,V,cubesatsim_ina219_voltage,NONE,5,1,3,Board Voltage,Power Supply Voltage +21,MIN,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MIN,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude 24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,MIN,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication -26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU -27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis -28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis -29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,MIN,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,MIN,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current -32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +25,MIN,rssi,12,dBm,14,NONE,1,1,3,RSSI,Received Signal Strength Indication +26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU +27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis +28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MIN,Sensor1,12,raw,cubesatsim_sensor1,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MIN,PSUCurrent,12,mA,cubesatsim_ina219_current,NONE,5,2,3,Current,Power Supply DC Current +32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V 36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected @@ -42,16 +42,16 @@ 40,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused 42,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -43,MIN,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator -44,MIN,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +43,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +44,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 45,MIN,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator 46,MIN,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator -47,MIN,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator -48,MIN,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator -49,MIN,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator +47,MIN,I2CfailureBatt,1,-,17,NONE,2,2,0,Battery I2C,Battery I2C Bus failure indicator +48,MIN,I2CfailurePSU1,1,-,17,NONE,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +49,MIN,I2CfailurePSU2,1,-,17,NONE,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator 50,MIN,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -51,MIN,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status -52,MIN,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status +51,MIN,RxAntDeploy,1,-,16,NONE,1,3,0,RX Antenna,2m Antenna status +52,MIN,TxAntDeploy,2,-,16,NONE,1,2,0,TX Antenna,70cm Antenna status 53,MIN,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator 54,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler 55,MIN,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds From 96921922834d17243d4025b265f7370e35f37b86 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Fri, 27 Nov 2020 17:53:45 -0500 Subject: [PATCH 129/151] Set all to NONE --- .../CubeSatSim_PSK_maxtelemetry.csv | 120 +++++++++--------- 1 file changed, 60 insertions(+), 60 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv index 8b8efd37..9f857d29 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv @@ -1,61 +1,61 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION -0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) -1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,MIN,BATT_V,12,V,cubesatsim_ina219_voltage,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,+X Panel,7,4,3,Acceleration,Acceleration around X Axis -4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis -5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis -6,MIN,battCurr,12,mA,cubesatsim_ina219_current,Battery,4,2,4,Current,Total Battery DC current -7,MIN,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature -8,MIN,posXv,12,V,cubesatsim_ina219_voltage,+X Panel,7,1,3,Voltage,+X solar Panel voltage -9,MIN,posYv,12,V,cubesatsim_ina219_voltage,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage -10,MIN,posZv,12,V,cubesatsim_ina219_voltage,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage -11,MIN,negXv,12,V,cubesatsim_ina219_voltage,-X Panel,10,1,3,Voltage,-X solar Panel voltage -12,MIN,negYv,12,V,cubesatsim_ina219_voltage,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage -13,MIN,negZv,12,V,cubesatsim_ina219_voltage,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage -14,MIN,posXi,12,mA,cubesatsim_ina219_current,+X Panel,7,2,4,Current,+X solar Panel current -15,MIN,posYi,12,mA,cubesatsim_ina219_current,+Y Panel,8,2,4,Current,+Y solar Panel current -16,MIN,posZi,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,4,Current,+Z solar Panel current -17,MIN,negXi,12,mA,cubesatsim_ina219_current,-X Panel,10,2,4,Current,-X solar Panel current -18,MIN,negYi,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,4,Current,-Y solar Panel current -19,MIN,negZi,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,4,Current,-Z solar Panel current -20,MIN,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,5,1,3,Board Voltage,Power Supply Voltage -21,MIN,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells -22,MIN,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure -23,MIN,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude -24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,MIN,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication -26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU -27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis -28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis -29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis -30,MIN,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,MIN,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current -32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 -34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted -35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V -36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected -37,MIN,rf6,12,-,0,NONE,0,0,0,None,None -38,MIN,rf7,12,-,0,NONE,0,0,0,None,None -39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR -40,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) -41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused -42,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -43,MIN,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator -44,MIN,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) -45,MIN,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator -46,MIN,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator -47,MIN,I2CfailureBatt,1,-,17,Computer Hardware,2,2,0,Battery I2C,Battery I2C Bus failure indicator -48,MIN,I2CfailurePSU1,1,-,17,Computer Hardware,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator -49,MIN,I2CfailurePSU2,1,-,17,Computer Hardware,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator -50,MIN,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry -51,MIN,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,2m Antenna status -52,MIN,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,70cm Antenna status -53,MIN,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator -54,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler -55,MIN,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds -56,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information -57,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset -58,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset -59,MIN,pad2,28,-,0,NONE,0,0,0,NONE,Filler +0,MAX,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) +1,MAX,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) +2,MAX,BATT_V,12,V,cubesatsim_ina219_voltage,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,NONE,7,4,3,Acceleration,Acceleration around X Axis +4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,NONE,8,4,3,Acceleration,Acceleration around Y Axis +5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,NONE,9,4,3,Acceleration,Acceleration around Z Axis +6,MAX,battCurr,12,mA,cubesatsim_ina219_current,NONE,4,2,4,Current,Total Battery DC current +7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature +8,MAX,posXv,12,V,cubesatsim_ina219_voltage,NONE,7,1,3,Voltage,+X solar Panel voltage +9,MAX,posYv,12,V,cubesatsim_ina219_voltage,NONE,8,1,3,Voltage,+Y solar Panel voltage +10,MAX,posZv,12,V,cubesatsim_ina219_voltage,NONE,9,1,3,Voltage,+Z solar Panel voltage +11,MAX,negXv,12,V,cubesatsim_ina219_voltage,NONE,10,1,3,Voltage,-X solar Panel voltage +12,MAX,negYv,12,V,cubesatsim_ina219_voltage,NONE,11,1,3,Voltage,-Y solar Panel voltage +13,MAX,negZv,12,V,cubesatsim_ina219_voltage,NONE,12,1,3,Voltage,-Z solar Panel voltage +14,MAX,posXi,12,mA,cubesatsim_ina219_current,NONE,7,2,4,Current,+X solar Panel current +15,MAX,posYi,12,mA,cubesatsim_ina219_current,NONE,8,2,4,Current,+Y solar Panel current +16,MAX,posZi,12,mA,cubesatsim_ina219_current,NONE,9,2,4,Current,+Z solar Panel current +17,MAX,negXi,12,mA,cubesatsim_ina219_current,NONE,10,2,4,Current,-X solar Panel current +18,MAX,negYi,12,mA,cubesatsim_ina219_current,NONE,11,2,4,Current,-Y solar Panel current +19,MAX,negZi,12,mA,cubesatsim_ina219_current,NONE,12,2,4,Current,-Z solar Panel current +20,MAX,PSUVoltage,12,V,cubesatsim_ina219_voltage,NONE,5,1,3,Board Voltage,Power Supply Voltage +21,MAX,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MAX,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure +23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude +24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,MAX,rssi,12,dBm,14,NONE,1,1,3,RSSI,Received Signal Strength Indication +26,MAX,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU +27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis +28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis +29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis +30,MAX,Sensor1,12,raw,cubesatsim_sensor1,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MAX,PSUCurrent,12,mA,cubesatsim_ina219_current,NONE,5,2,3,Current,Power Supply DC Current +32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MAX,Sensor3,12,signed raw,cubesatsim_sensor3,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +35,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +36,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +37,MAX,rf6,12,-,0,NONE,0,0,0,None,None +38,MAX,rf7,12,-,0,NONE,0,0,0,None,None +39,MAX,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +40,MAX,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +41,MAX,pad,4,-,34,NONE,0,0,0,None,Unused +42,MAX,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +43,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +44,MAX,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +45,MAX,expFailure2,1,-,17,NONE,6,7,0,Exp 2,Experiment 2 Failure Indicator +46,MAX,expFailure3,1,-,17,NONE,6,8,0,Exp 3,Experiment 3 Failure Indicator +47,MAX,I2CfailureBatt,1,-,17,NONE,2,2,0,Battery I2C,Battery I2C Bus failure indicator +48,MAX,I2CfailurePSU1,1,-,17,NONE,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator +49,MAX,I2CfailurePSU2,1,-,17,NONE,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator +50,MAX,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry +51,MAX,RxAntDeploy,1,-,16,NONE,1,3,0,RX Antenna,2m Antenna status +52,MAX,TxAntDeploy,2,-,16,NONE,1,2,0,TX Antenna,70cm Antenna status +53,MAX,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator +54,MAX,pad1,1,-,0,NONE,0,0,0,NONE,Filler +55,MAX,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +56,MAX,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +57,MAX,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset +58,MAX,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset +59,MAX,pad2,28,-,0,NONE,0,0,0,NONE,Filler From 4d52525bf1642159c935be9b2128b91911d04b68 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 03:15:03 -0500 Subject: [PATCH 130/151] changed to CubeSatSim_PSK_Type1_HEALTH.frame --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER index 6b3132cd..d84569c0 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER @@ -19,7 +19,7 @@ description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite m numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame frameLayout0.name=All WOD -frameLayout1.filename=FOX1E_Type1_HEALTH.frame +frameLayout1.filename=CubeSatSim_PSK_Type1_HEALTH.frame frameLayout1.name=Health frameLayout2.filename=FOX1E_Type2_MINMAX.frame frameLayout2.name=MinMax From 66f68444a9b22f46e43976d72294aeb93f873c42 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 03:18:32 -0500 Subject: [PATCH 131/151] created from FOX1E file but only rt and wod payloads --- .../CubeSatSim_PSK_Type1_HEALTH.frame | 13 +++++++++++++ 1 file changed, 13 insertions(+) create mode 100644 spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type1_HEALTH.frame diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type1_HEALTH.frame b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type1_HEALTH.frame new file mode 100644 index 00000000..7a2c87de --- /dev/null +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type1_HEALTH.frame @@ -0,0 +1,13 @@ +number_of_payloads=6 +payload0.name=rttelemetry +payload0.length=78 +payload1.name=rttelemetry +payload1.length=78 +payload2.name=rttelemetry +payload2.length=78 +payload3.name=rttelemetry +payload3.length=78 +payload4.name=rttelemetry +payload4.length=78 +payload5.name=wodtelemetry +payload5.length=78 From d68943e250fd1831344ddb12dc09df74d55ac5de Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 03:24:35 -0500 Subject: [PATCH 132/151] Try turning off all EXP --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER index d84569c0..44b56791 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER @@ -12,9 +12,9 @@ displayName=CubeSatSim-BPSK BATTERY_CURRENT_ZERO=-1.834 hasImprovedCommandReceiver=true EXP1=0 -EXP2=1 -EXP3=8 -EXP4=7 +EXP2=0 +EXP3=0 +EXP4=0 description=CubeSatSim, the AMSAT CubeSat Simulator, is a functional satellite model that generates real telemetry from solar panels, batteries, and temperature sensors. Use this for BPSK telemetry. For more information see http://cubesatsim.org numberOfFrameLayouts=5 frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame From 2b5b3566f3db9bfc3d7655e7dc1bfb99e350ea8b Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 03:35:31 -0500 Subject: [PATCH 133/151] changed to CubeSatSim_PSK_Type2_MINMAX.frame --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER index 44b56791..81bd29ae 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_PSK.MASTER @@ -21,7 +21,7 @@ frameLayout0.filename=FOX1E_Type0_ALL_WOD.frame frameLayout0.name=All WOD frameLayout1.filename=CubeSatSim_PSK_Type1_HEALTH.frame frameLayout1.name=Health -frameLayout2.filename=FOX1E_Type2_MINMAX.frame +frameLayout2.filename=CubeSatSim_PSK_Type2_MINMAX.frame frameLayout2.name=MinMax frameLayout3.filename=FOX1E_Type3_REALTIME_BEACON.frame frameLayout3.name=Realtime Beacon From 7c600d55011f928a4081d7112d36a86694763a40 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 03:38:01 -0500 Subject: [PATCH 134/151] created from FOX1E but only rt, max, min, and wod payloads --- .../CubeSatSim_PSK_Type2_MINMAX.frame | 13 +++++++++++++ 1 file changed, 13 insertions(+) create mode 100644 spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame new file mode 100644 index 00000000..f46a9538 --- /dev/null +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame @@ -0,0 +1,13 @@ +number_of_payloads=6 +payload0.name=rtelemetry +payload0.length=78 +payload1.name=rtelemetry +payload1.length=78 +payload2.name=rtelemetry +payload2.length=78 +payload3.name=maxtelemetry +payload3.length=78 +payload4.name=mintelemetry +payload4.length=78 +payload5.name=wodtelemetry +payload5.length=78 From 14800af0095bbd04c38dd2b130913b8bb4724a5f Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 03:42:08 -0500 Subject: [PATCH 135/151] changed tracked to false --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER index d9284763..87be4f31 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.MASTER @@ -46,7 +46,7 @@ passMeasurementsFileName=passmeasurements.csv numberOfSources=1 source0.name=amsat.cubesat_simulator.ihu.duv #source1.name=amsat.cubesat_simulator.ihu.highspeed -track=true +track=false useIHUVBatt=true user_mode=0 user_format=0 From 32bf053a0b16036e94890f98264fd41c0aba13d2 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 03:45:21 -0500 Subject: [PATCH 136/151] changed to track false --- spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat index 32d452e8..65bebafc 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat +++ b/spacecraft/FoxTelem_1.09m/CubeSat_Simulator_DUV.dat @@ -10,6 +10,6 @@ memsRestValueZ=2045 user_format=0 memsRestValueX=2087 name=CubeSatSim -track=true +track=false telemetryDownlinkFreqkHz=434900.0 BATTERY_CURRENT_ZERO=-1.839 From f97d863948b5d39c2e7218860e38525e9e125a97 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 12:22:59 -0500 Subject: [PATCH 137/151] changed to frame_type 2 to test max, min --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 6c024b30..b3bba8fe 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x02, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From 2fb646bedbb37b70d04436f9909822be17ab14ac Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 13:24:34 -0500 Subject: [PATCH 138/151] testing frame type 3 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index b3bba8fe..0404cc47 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x02, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x03, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From dc71a9b9c5822d07ce0d5fb1c5e30096b81abb58 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 13:34:19 -0500 Subject: [PATCH 139/151] frame type 2 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 0404cc47..b3bba8fe 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x03, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x02, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From ff153c836dcbb368fe6fa73814890cb8a1435314 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Sat, 28 Nov 2020 15:18:18 -0500 Subject: [PATCH 140/151] changes after n2 --- .../CubeSatSim_PSK_Type2_MINMAX.frame | 6 +-- .../CubeSatSim_PSK_maxtelemetry.csv | 48 +++++++++--------- .../CubeSatSim_PSK_mintelemetry.csv | 50 +++++++++---------- 3 files changed, 52 insertions(+), 52 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame index f46a9538..771b59f5 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_Type2_MINMAX.frame @@ -1,9 +1,9 @@ number_of_payloads=6 -payload0.name=rtelemetry +payload0.name=rttelemetry payload0.length=78 -payload1.name=rtelemetry +payload1.name=rttelemetry payload1.length=78 -payload2.name=rtelemetry +payload2.name=rttelemetry payload2.length=78 payload3.name=maxtelemetry payload3.length=78 diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv index 9f857d29..3b7d4c90 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_maxtelemetry.csv @@ -1,38 +1,38 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,MAX,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,MAX,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,MAX,BATT_V,12,V,cubesatsim_ina219_voltage,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,NONE,7,4,3,Acceleration,Acceleration around X Axis -4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,NONE,8,4,3,Acceleration,Acceleration around Y Axis -5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,NONE,9,4,3,Acceleration,Acceleration around Z Axis -6,MAX,battCurr,12,mA,cubesatsim_ina219_current,NONE,4,2,4,Current,Total Battery DC current +2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis +4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis +5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis +6,MAX,battCurr,12,mA,cubesatsim_current,NONE,4,2,4,Current,Total Battery DC current 7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature -8,MAX,posXv,12,V,cubesatsim_ina219_voltage,NONE,7,1,3,Voltage,+X solar Panel voltage -9,MAX,posYv,12,V,cubesatsim_ina219_voltage,NONE,8,1,3,Voltage,+Y solar Panel voltage -10,MAX,posZv,12,V,cubesatsim_ina219_voltage,NONE,9,1,3,Voltage,+Z solar Panel voltage -11,MAX,negXv,12,V,cubesatsim_ina219_voltage,NONE,10,1,3,Voltage,-X solar Panel voltage -12,MAX,negYv,12,V,cubesatsim_ina219_voltage,NONE,11,1,3,Voltage,-Y solar Panel voltage -13,MAX,negZv,12,V,cubesatsim_ina219_voltage,NONE,12,1,3,Voltage,-Z solar Panel voltage -14,MAX,posXi,12,mA,cubesatsim_ina219_current,NONE,7,2,4,Current,+X solar Panel current -15,MAX,posYi,12,mA,cubesatsim_ina219_current,NONE,8,2,4,Current,+Y solar Panel current -16,MAX,posZi,12,mA,cubesatsim_ina219_current,NONE,9,2,4,Current,+Z solar Panel current -17,MAX,negXi,12,mA,cubesatsim_ina219_current,NONE,10,2,4,Current,-X solar Panel current -18,MAX,negYi,12,mA,cubesatsim_ina219_current,NONE,11,2,4,Current,-Y solar Panel current -19,MAX,negZi,12,mA,cubesatsim_ina219_current,NONE,12,2,4,Current,-Z solar Panel current -20,MAX,PSUVoltage,12,V,cubesatsim_ina219_voltage,NONE,5,1,3,Board Voltage,Power Supply Voltage -21,MAX,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +8,MAX,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X solar Panel voltage +9,MAX,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y solar Panel voltage +10,MAX,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z solar Panel voltage +11,MAX,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X solar Panel voltage +12,MAX,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y solar Panel voltage +13,MAX,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z solar Panel voltage +14,MAX,posXi,12,mA,cubesatsim_current,NONE,7,2,4,Current,+X solar Panel current +15,MAX,posYi,12,mA,cubesatsim_current,NONE,8,2,4,Current,+Y solar Panel current +16,MAX,posZi,12,mA,cubesatsim_current,NONE,9,2,4,Current,+Z solar Panel current +17,MAX,negXi,12,mA,cubesatsim_current,NONE,10,2,4,Current,-X solar Panel current +18,MAX,negYi,12,mA,cubesatsim_current,NONE,11,2,4,Current,-Y solar Panel current +19,MAX,negZi,12,mA,cubesatsim_current,NONE,12,2,4,Current,-Z solar Panel current +20,MAX,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Board Voltage,Power Supply Voltage +21,MAX,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,MAX,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure 23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude 24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,MAX,rssi,12,dBm,14,NONE,1,1,3,RSSI,Received Signal Strength Indication +25,MAX,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication 26,MAX,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU 27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis 28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis 29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis -30,MAX,Sensor1,12,raw,cubesatsim_sensor1,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,MAX,PSUCurrent,12,mA,cubesatsim_ina219_current,NONE,5,2,3,Current,Power Supply DC Current -32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,MAX,Sensor3,12,signed raw,cubesatsim_sensor3,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +30,MAX,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MAX,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current +32,MAX,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MAX,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 35,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V 36,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv index d1bcb2aa..174cb667 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_mintelemetry.csv @@ -1,38 +1,38 @@ 60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,MIN,BATT_A_V,12,V,4,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale) 1,MIN,BATT_B_V,12,V,4,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale) -2,MIN,BATT_V,12,V,cubesatsim_ina219_voltage,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) -3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_rotation,NONE,7,4,3,Acceleration,Acceleration around X Axis -4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,NONE,8,4,3,Acceleration,Acceleration around Y Axis -5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,NONE,9,4,3,Acceleration,Acceleration around Z Axis -6,MIN,battCurr,12,mA,cubesatsim_ina219_current,NONE,4,2,4,Current,Total Battery DC current +2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis +4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis +5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis +6,MIN,battCurr,12,mA,cubesatsim_current,NONE,4,2,4,Current,Total Battery DC current 7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature -8,MIN,posXv,12,V,cubesatsim_ina219_voltage,NONE,7,1,3,Voltage,+X solar Panel voltage -9,MIN,posYv,12,V,cubesatsim_ina219_voltage,NONE,8,1,3,Voltage,+Y solar Panel voltage -10,MIN,posZv,12,V,cubesatsim_ina219_voltage,NONE,9,1,3,Voltage,+Z solar Panel voltage -11,MIN,negXv,12,V,cubesatsim_ina219_voltage,NONE,10,1,3,Voltage,-X solar Panel voltage -12,MIN,negYv,12,V,cubesatsim_ina219_voltage,NONE,11,1,3,Voltage,-Y solar Panel voltage -13,MIN,negZv,12,V,cubesatsim_ina219_voltage,NONE,12,1,3,Voltage,-Z solar Panel voltage -14,MIN,posXi,12,mA,cubesatsim_ina219_current,NONE,7,2,4,Current,+X solar Panel current -15,MIN,posYi,12,mA,cubesatsim_ina219_current,NONE,8,2,4,Current,+Y solar Panel current -16,MIN,posZi,12,mA,cubesatsim_ina219_current,NONE,9,2,4,Current,+Z solar Panel current -17,MIN,negXi,12,mA,cubesatsim_ina219_current,NONE,10,2,4,Current,-X solar Panel current -18,MIN,negYi,12,mA,cubesatsim_ina219_current,NONE,11,2,4,Current,-Y solar Panel current -19,MIN,negZi,12,mA,cubesatsim_ina219_current,NONE,12,2,4,Current,-Z solar Panel current -20,MIN,PSUVoltage,12,V,cubesatsim_ina219_voltage,NONE,5,1,3,Board Voltage,Power Supply Voltage -21,MIN,spin,12,rpm,12,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +8,MIN,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X solar Panel voltage +9,MIN,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y solar Panel voltage +10,MIN,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z solar Panel voltage +11,MIN,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X solar Panel voltage +12,MIN,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y solar Panel voltage +13,MIN,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z solar Panel voltage +14,MIN,posXi,12,mA,cubesatsim_current,NONE,7,2,4,Current,+X solar Panel current +15,MIN,posYi,12,mA,cubesatsim_current,NONE,8,2,4,Current,+Y solar Panel current +16,MIN,posZi,12,mA,cubesatsim_current,NONE,9,2,4,Current,+Z solar Panel current +17,MIN,negXi,12,mA,cubesatsim_current,NONE,10,2,4,Current,-X solar Panel current +18,MIN,negYi,12,mA,cubesatsim_current,NONE,11,2,4,Current,-Y solar Panel current +19,MIN,negZi,12,mA,cubesatsim_current,NONE,12,2,4,Current,-Z solar Panel current +20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Board Voltage,Power Supply Voltage +21,MIN,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,MIN,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure 23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude 24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,MIN,rssi,12,dBm,14,NONE,1,1,3,RSSI,Received Signal Strength Indication +25,MIN,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication 26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,Temperature,Internal Temperature of IHU 27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis 28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis 29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis -30,MIN,Sensor1,12,raw,cubesatsim_sensor1,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 -31,MIN,PSUCurrent,12,mA,cubesatsim_ina219_current,NONE,5,2,3,Current,Power Supply DC Current -32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 -33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +30,MIN,Sensor1,12,raw,cubesatsim_sensor1|INT,NONE,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current +32,MIN,Sensor2,12,signed raw,cubesatsim_sensor2|INT,NONE,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,MIN,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,NONE,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted 35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V 36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected @@ -58,4 +58,4 @@ 56,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information 57,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset 58,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset -59,MIN,pad2,28,-,0,NONE,0,0,0,NONE,Filler +59,MIN,pad2,28,-,0,NONE,0,0,0,NONE,Filler \ No newline at end of file From cc52a0a2232122704a8a6719adf6979d36a32999 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 15:27:05 -0500 Subject: [PATCH 141/151] added WODTimeStampReset and WODTimeStampUpTime for Whole Orbit Data frames --- .../FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv | 9 +++++---- 1 file changed, 5 insertions(+), 4 deletions(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv index 62084a60..54944fc2 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv @@ -1,4 +1,4 @@ -60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION 0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale) 1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale) 2,WOD,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) @@ -52,10 +52,11 @@ 50,WOD,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR 51,WOD,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 52,WOD,pad,4,-,34,NONE,0,0,0,None,Unused -53,WOD,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance -54,WOD,pad1,1,-,0,NONE,0,0,0,NONE,Filler +53,WOD,WODTimeStampReset,25,-,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected +54,WOD,pad1,17,-,0,NONE,0,0,0,NONE,Filler 55,WOD,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds 56,WOD,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information 57,WOD,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset 58,WOD,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset -59,WOD,pad2,28,-,0,NONE,0,0,0,NONE,Filler +59,WOD,WODTimeStampUpTime,25,s,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected +60,WOD,pad2,3,-,0,NONE,0,0,0,NONE,Filler From 792fa371d925a8b3810c33ca55bc2ae314370813 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 15:27:42 -0500 Subject: [PATCH 142/151] Update CubeSatSim_PSK_wodtelemetry.csv --- spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv index 54944fc2..2af08ba9 100644 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv @@ -52,7 +52,7 @@ 50,WOD,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR 51,WOD,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) 52,WOD,pad,4,-,34,NONE,0,0,0,None,Unused -53,WOD,WODTimeStampReset,25,-,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected +53,WOD,WODTimeStampReset,16,-,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected 54,WOD,pad1,17,-,0,NONE,0,0,0,NONE,Filler 55,WOD,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds 56,WOD,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information From 1845d78d5a2bb4f5504813bcb85c1621e1f51a20 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 15:51:03 -0500 Subject: [PATCH 143/151] added rounding in integer conversion for currents --- afsk/main.c | 16 ++++++++-------- 1 file changed, 8 insertions(+), 8 deletions(-) diff --git a/afsk/main.c b/afsk/main.c index b3bba8fe..b4864f01 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -1003,12 +1003,12 @@ if (firstTime != ON) if (mode == BPSK) h[6] = 99; - posXi = (int)current[map[PLUS_X]] + 2048; - posYi = (int)current[map[PLUS_Y]] + 2048; - posZi = (int)current[map[PLUS_Z]] + 2048; - negXi = (int)current[map[MINUS_X]] + 2048; - negYi = (int)current[map[MINUS_Y]] + 2048; - negZi = (int)current[map[MINUS_Z]] + 2048; + posXi = (int)(current[map[PLUS_X]] + 0.5) + 2048; + posYi = (int)(current[map[PLUS_Y]] + 0.5) + 2048; + posZi = (int)(current[map[PLUS_Z]] + 0.5) + 2048; + negXi = (int)(current[map[MINUS_X]] + 0.5) + 2048; + negYi = (int)(current[map[MINUS_Y]] + 0.5) + 2048; + negZi = (int)(current[map[MINUS_Z]] + 0.5) + 2048; posXv = (int)(voltage[map[PLUS_X]] * 100); posYv = (int)(voltage[map[PLUS_Y]] * 100); @@ -1017,9 +1017,9 @@ if (firstTime != ON) negYv = (int)(voltage[map[MINUS_Y]] * 100); negZv = (int)(voltage[map[MINUS_Z]] * 100); batt_c_v = (int)(voltage[map[BAT]] * 100); - battCurr = (int)current[map[BAT]] + 2048; + battCurr = (int)(current[map[BAT]] + 0.5) + 2048; PSUVoltage = (int)(voltage[map[BUS]] * 100); - PSUCurrent = (int)current[map[BUS]] + 2048; + PSUCurrent = (int)(current[map[BUS]] + 0.5) + 2048; if (payload == ON) STEMBoardFailure = 0; From 5175f5df3a480c22e147374856b88fd90e6c7a0e Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 15:54:37 -0500 Subject: [PATCH 144/151] test payload type 3 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index b4864f01..b3b4bdda 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x02, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x03, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From 1a490d7ba5190e4fbd7b2385181b0c2e5cefd2a1 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 15:57:54 -0500 Subject: [PATCH 145/151] back to frame type 1 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index b3b4bdda..695df092 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x03, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From 73e39bcb69e7629bb4742cad97b67a66c8b0e575 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 16:19:59 -0500 Subject: [PATCH 146/151] Got rid of Status in STEM Payload field --- spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetry.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetry.csv index d950ec24..129c5153 100755 --- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetry.csv @@ -33,7 +33,7 @@ 31,RT,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 -34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status +34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload,STEM Payload Board Status 35,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 36,RT,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator 37,RT,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator From 20ef9f3f9020de0ad0a0f7b202eec6099d98b2bf Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 22:17:08 -0500 Subject: [PATCH 147/151] testing type 2 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 695df092..b4864f01 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x02, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From dd7e8a9feb84df0aa97b9e9af71cc47f29be17a5 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 22:29:36 -0500 Subject: [PATCH 148/151] test type 3 --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index b4864f01..b3b4bdda 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x02, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x03, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From c429ae441e0868f2c7c1b0219a823e0cf5a3eab1 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Sat, 28 Nov 2020 22:34:53 -0500 Subject: [PATCH 149/151] back to type 1 again --- afsk/main.c | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index b3b4bdda..695df092 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -875,7 +875,7 @@ int get_tlm_fox() { short int rs_frame[rsFrames][223]; unsigned char parities[rsFrames][parityLen], inputByte; - int id, frm_type = 0x03, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // + int id, frm_type = 0x01, TxTemp = 0, IHUcpuTemp = 0, STEMBoardFailure = 1, NormalModeFailure = 0, rxAntennaDeployed = 0, txAntennaDeployed = 1, groundCommandCount = 3; // int PSUVoltage = 0, PSUCurrent = 0; int batt_a_v = 0, batt_b_v = 0, batt_c_v = 0, battCurr = 0; int posXv = 0, negXv = 0, posYv = 0, negYv = 0, posZv = 0, negZv = 0; From 7698dbb6ebad25500eb0740a86cda578f12ca7a1 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Mon, 30 Nov 2020 09:57:52 -0500 Subject: [PATCH 150/151] swapped -X and +Z for vB5 --- afsk/telem.c | 5 +++-- 1 file changed, 3 insertions(+), 2 deletions(-) diff --git a/afsk/telem.c b/afsk/telem.c index 3e7a9227..88a7b006 100644 --- a/afsk/telem.c +++ b/afsk/telem.c @@ -105,12 +105,13 @@ int main(int argc, char *argv[]) { if (digitalRead(26) != HIGH) { printf("vB5 Present\n"); // Don't print normal board detection - + map[MINUS_X] = PLUS_Z; + map[PLUS_Z] = MINUS_X; snprintf(busStr, 10, "%d %d", test_i2c_bus(1), test_i2c_bus(3)); printf("New Bus String: %s \n", busStr); /* - if (test_i2c_bus(0) != OFF) + if (test_i2c_b0) != OFF) strcpy(busStr,"1 "); else strcpy(busStr,"-1 "); From a2309c00a7ea19f01713578e6a33a55b6194dca6 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Mon, 30 Nov 2020 09:59:56 -0500 Subject: [PATCH 151/151] swapped -X and +Z mapping --- afsk/main.c | 5 ++++- 1 file changed, 4 insertions(+), 1 deletion(-) diff --git a/afsk/main.c b/afsk/main.c index 695df092..07884672 100644 --- a/afsk/main.c +++ b/afsk/main.c @@ -317,7 +317,10 @@ if (vB4) snprintf(busStr, 10, "%d %d", test_i2c_bus(1), test_i2c_bus(0)); } else if (vB5) -{ +{ + map[MINUS_X] = PLUS_Z; + map[PLUS_Z] = MINUS_X; + if (access("/dev/i2c-11", W_OK | R_OK) >= 0) { // Test if I2C Bus 11 is present printf("/dev/i2c-11 is present\n\n"); snprintf(busStr, 10, "%d %d", test_i2c_bus(1), test_i2c_bus(11));