KB8PMY
/
CubeSatSim
mirror of https://github.com/alanbjohnston/CubeSatSim.git
1
0
Fork 0
Code Issues Packages Projects Releases Wiki Activity

back to 11a original

Browse Source
pull/85/head
alanbjohnston 5 years ago committed by GitHub
parent 269a1d7fba
commit 84517246d2
No known key found for this signature in database
GPG Key ID: 4AEE18F83AFDEB23
2 changed files with 51 additions and 98 deletions
Show Stats Download Patch File Download Diff File

94
spacecraft/FoxTelem_11a/CubeSatSim_mintelemetry.csv
Unescape View File

@ -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,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,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_temperature,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,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
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,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,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,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

1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHOMIN_NAME DESCRIPTION DESCRIPTION
2 0 MIN BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Battery A voltage (0-2.5V scale) Battery A voltage (0-2.5V scale)
3 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) Battery A+B voltage (0-3.3V scale)
4 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) Battery A+B+C voltage (0-5.0V scale)
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis Acceleration around Z Axis
8 6 MIN TOTAL_BATT_I 12 mA cubesatsim_current NONE 4 2 3 Current Total Battery DC current Total Battery DC current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temperature STEM Payload Sensor Temperature STEM Payload Sensor Temperature
10 8 MIN PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X Panel +X Panel
11 9 MIN PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X Panel -X Panel
12 10 MIN PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y Panel +Y Panel
13 11 MIN PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y Panel -Y Panel
14 12 MIN PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z Panel +Z Panel
15 13 MIN PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z Panel -Z Panel
16 14 MIN PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current +X Panel +X Panel
17 15 MIN PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current -X Panel -X Panel
18 16 MIN PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current +Y Panel +Y Panel
19 17 MIN PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current -Y Panel -Y Panel
20 18 MIN PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current +Z Panel +Z Panel
21 19 MIN PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current -Z Panel -Z Panel
22 20 MIN PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Voltage Power Supply Voltage Power Supply Voltage
23 21 MIN SPIN 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells Calculated spin rate using solar cells
24 22 MIN Pressure 12 bar cubesatsim_pressure NONE 6 3 3 Pressure STEM Payload Sensor Pressure STEM Payload Sensor Pressure
25 23 MIN Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude STEM Payload Sensor Altitude STEM Payload Sensor Altitude
26 24 MIN Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count Software Reset Count
27 25 MIN RSSI 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication Received Signal Strength Indication
28 26 MIN IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 Temperature Internal Temperature of IHU Internal Temperature of IHU
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation Angular Veolcity around X Axis Angular Veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation Angular Veolcity around Y Axis Angular Veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation Angular Veolcity around Z Axis Angular Veolcity around Z Axis
32 30 MIN Sensor1 12 raw cubesatsim_temperature cubesatsim_sensor1|INT NONE 6 5 3 Sensor 1 STEM Payload Extra Sensor 1 STEM Payload Extra Sensor 1
33 31 MIN PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current Power Supply DC Current
34 32 MIN Sensor2 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 2 STEM Payload Extra Sensor 2 STEM Payload Extra Sensor 2
35 33 MIN Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 3 STEM Payload Extra Sensor 3 STEM Payload Extra Sensor 3
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status STEM Payload Board Status
37 35 MIN Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode) Nominal Mode (Not Safe Mode)
38 36 MIN PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator STEM Payload status 1 failure indicator
39 37 MIN PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator STEM Payload status 2 failure indicator
40 38 MIN I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator I2C bus 0 failure indicator
41 39 MIN I2CBus1Failure 1 - 17 NONE 2 3 0 I2C Bus 1 I2C bus 1 failure indicator I2C bus 1 failure indicator
42 40 MIN I2CBus3Failure 1 - 17 NONE 2 4 0 I2C Bus 3 I2C bus 3 failure indicator I2C bus 3 failure indicator
43 41 MIN CameraFailure 1 - 17 NONE 2 5 0 Camera Camera failure indicator Camera failure indicator
44 42 MIN GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received Number of ground commands received
45 43 MIN RXAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status Receive antenna status
46 44 MIN TXAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status Transmit antenna status
47 45 MIN Pad 58 - 0 NONE 0 0 0 NONE NONE NONE

55
spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
Unescape View File

@ -1,94 +1,47 @@
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)
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_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,hPa,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure
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,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
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis
30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,Humidity
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_current,PSU,5,2,3,Current,Power Supply DC Current
32,RT,Sensor1,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,RT,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,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,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
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,Transmit antenna status
45,RT,Pad,58,-,0,NONE,0,0,0,NONE,NONE

1 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)
2 1 0 RT BATT_B_V BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A+B Cell A Battery A+B voltage (0-3.3V scale) Battery A voltage (0-2.5V 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 3 1 RT SatelliteXAxisAcceleration BATT_B_V 12 g V cubesatsim_acceleration|FLOAT2 cubesatsim_voltage|FLOAT2 +X Panel NONE 7 0 4 0 3 Acceleration Cell A+B Acceleration around X Axis Battery A+B voltage (0-3.3V scale)
4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
4 5 2 RT SatelliteZAxisAcceleration BATT_V 12 g V cubesatsim_acceleration|FLOAT2 cubesatsim_voltage|FLOAT2 +Z Panel Battery 9 4 4 1 3 Acceleration Cell A+B+C Voltage Acceleration around Z Axis Battery A+B+C voltage (0-5.0V scale)
6 RT TOTAL_BATT_I 12 mA cubesatsim_current Battery 4 2 3 Current Total Battery DC current
5 7 3 RT Temperature SatelliteXAxisAcceleration 12 C g cubesatsim_temperature cubesatsim_acceleration|FLOAT2 Experiments +X Panel 6 7 2 4 3 Temperature Acceleration STEM Payload Sensor Temperature Acceleration around X Axis
8 RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X Panel
6 9 4 RT PANEL_MINUS_X_V SatelliteYAxisAcceleration 12 V g cubesatsim_voltage|FLOAT2 cubesatsim_acceleration|FLOAT2 -X Panel +Y Panel 10 8 1 4 3 Voltage Acceleration -X Panel Acceleration around Y Axis
10 RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y Panel
7 11 5 RT PANEL_MINUS_Y_V SatelliteZAxisAcceleration 12 V g cubesatsim_voltage|FLOAT2 cubesatsim_acceleration|FLOAT2 -Y Panel +Z Panel 11 9 1 4 3 Voltage Acceleration -Y Panel Acceleration around Z Axis
12 RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z Panel
8 13 6 RT PANEL_MINUS_Z_V TOTAL_BATT_I 12 V mA cubesatsim_voltage|FLOAT2 cubesatsim_current -Z Panel Battery 12 4 1 2 3 Voltage Current -Z Panel Total Battery DC current
14 RT PANEL_PLUS_X_I 12 mA cubesatsim_current +X Panel 7 2 3 Current +X Panel
9 15 7 RT PANEL_MINUS_X_I Temperature 12 mA C cubesatsim_current cubesatsim_temperature -X Panel Experiments 10 6 2 3 Current Temperature -X Panel STEM Payload Sensor Temperature
16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_current +Y Panel 8 2 3 Current +Y Panel
10 17 8 RT PANEL_MINUS_Y_I PANEL_PLUS_X_V 12 mA V cubesatsim_current cubesatsim_voltage|FLOAT2 -Y Panel +X Panel 11 7 2 1 3 Current Voltage -Y Panel +X Panel
18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_current +Z Panel 9 2 3 Current +Z Panel
11 19 9 RT PANEL_MINUS_Z_I PANEL_MINUS_X_V 12 mA V cubesatsim_current cubesatsim_voltage|FLOAT2 -Z Panel -X Panel 12 10 2 1 3 Current Voltage -Z Panel -X Panel
20 RT PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply Voltage
12 21 10 RT SPIN PANEL_PLUS_Y_V 12 rpm V cubesatsim_rpm cubesatsim_voltage|FLOAT2 Computer Software +Y Panel 3 8 1 3 Spacecraft Spin Voltage Calculated spin rate using solar cells +Y Panel
22 RT Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 Pressure STEM Payload Sensor Pressure
13 23 11 RT Altitude PANEL_MINUS_Y_V 12 m V cubesatsim_altitude cubesatsim_voltage|FLOAT2 Experiments -Y Panel 6 11 4 1 3 Altitude Voltage STEM Payload Sensor Altitude -Y Panel
24 RT Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
14 25 12 RT RSSI PANEL_PLUS_Z_V 12 dBm V cubesatsim_rssi|INT cubesatsim_voltage|FLOAT2 Radio +Z Panel 1 9 1 3 RSSI Voltage Received Signal Strength Indication +Z Panel
26 RT IHUTemperature 12 C cubesatsim_temperature Computer Hardware 2 1 3 Temperature Internal Temperature of IHU
15 27 13 RT SatelliteXAxisAngularVelocity PANEL_MINUS_Z_V 12 dps V cubesatsim_rotation|INT cubesatsim_voltage|FLOAT2 +X Panel -Z Panel 7 12 3 1 3 Rotation Voltage Angular Veolcity around X Axis -Z Panel
28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation Angular Veolcity around Y Axis
16 29 14 RT SatelliteZAxisAngularVelocity PANEL_PLUS_X_I 12 dps mA cubesatsim_rotation|INT cubesatsim_current +Z Panel +X Panel 9 7 3 2 3 Rotation Current Angular Veolcity around Z Axis +X Panel
30 RT Humidity 12 % cubesatsim_temperature Experiments 6 5 3 Humidity Humidity
17 31 15 RT PSUCurrent PANEL_MINUS_X_I 12 mA cubesatsim_current PSU -X Panel 5 10 2 3 Current Power Supply DC Current -X Panel
32 RT Sensor1 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 1 STEM Payload Extra Sensor 1
18 33 16 RT Sensor2 PANEL_PLUS_Y_I 12 signed scaled mA cubesatsim_sensor3|FLOAT2 cubesatsim_current Experiments +Y Panel 6 8 7 2 3 Sensor 2 Current STEM Payload Extra Sensor 2 +Y Panel
34 RT STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload STEM Payload Board Status
19 35 17 RT Nominal Mode PANEL_MINUS_Y_I 1 12 - mA 17 cubesatsim_current Computer Software -Y Panel 3 11 2 0 3 Nominal Mode Current Nominal Mode (Not Safe Mode) -Y Panel
36 RT PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
20 37 18 RT PayloadStatus2 PANEL_PLUS_Z_I 1 12 - mA 17 cubesatsim_current NONE +Z Panel 6 9 8 2 0 3 Exp 3 Current STEM Payload status 2 failure indicator +Z Panel
38 RT I2CBus0Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
21 39 19 RT I2CBus1Failure PANEL_MINUS_Z_I 1 12 - mA 17 cubesatsim_current Computer Hardware -Z Panel 2 12 3 2 0 3 I2C Bus 1 Current I2C bus 1 failure indicator -Z Panel
40 RT I2CBus3Failure 1 - 17 Computer Hardware 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
22 41 20 RT CameraFailure PSUVoltage 1 12 - V 17 cubesatsim_voltage|FLOAT2 Computer Hardware PSU 2 5 5 1 0 3 Camera Voltage Camera failure indicator Power Supply Voltage
42 RT GroundCommands 4 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
23 43 21 RT RXAntenna SPIN 1 12 - rpm 16 cubesatsim_rpm Radio Computer Software 1 3 3 1 0 3 RX Antenna Spacecraft Spin Receive antenna status Calculated spin rate using solar cells
24 44 22 RT TXAntenna Pressure 1 12 - bar 16 cubesatsim_pressure Radio Experiments 1 6 2 3 0 3 TX Antenna Pressure Transmit antenna status STEM Payload Sensor Pressure
45 RT Pad 58 - 0 NONE 0 0 0 NONE NONE
25 23 RT Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude STEM Payload Sensor Altitude
26 24 RT Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 RT RSSI 12 dBm cubesatsim_rssi|INT Radio 1 1 3 RSSI Received Signal Strength Indication
28 26 RT IHUTemperature 12 C cubesatsim_temperature Computer Hardware 2 1 3 Temperature Internal Temperature of IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 RT Sensor1 12 raw cubesatsim_sensor1|INT Experiments 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 RT PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 RT Sensor2 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 RT Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
36 34 RT STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload STEM Payload Board Status
37 35 RT Nominal Mode 1 - 17 Computer Software 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 RT PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 RT PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator
40 38 RT I2CBus0Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 RT I2CBus1Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 RT I2CBus3Failure 1 - 17 Computer Hardware 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 RT CameraFailure 1 - 17 Computer Hardware 2 5 0 Camera Camera failure indicator
44 42 RT GroundCommands 4 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
45 43 RT RXAntenna 1 - 16 Radio 1 3 0 RX Antenna Receive antenna status
46 44 RT TXAntenna 1 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 RT Pad 58 - 0 NONE 0 0 0 NONE NONE
Write Preview
Loading…
Cancel
Save

Powered by TurnKey Linux.