From cd749932f249cb5cd4dc54c1631bb96c8dfe6926 Mon Sep 17 00:00:00 2001 From: alanbjohnston Date: Thu, 26 Nov 2020 14:17:45 -0500 Subject: [PATCH] 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