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updates to get ready for v1 code release

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alanbjohnston 5 years ago committed by GitHub
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47
spacecraft/FoxTelem_11a/CubeSatSim_maxtelemetry.csv
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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,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,hPa,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,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_temperature,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,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
1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHOMAX_NAME DESCRIPTION
2 0 MAX BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Battery A voltage (0-2.5V scale)
3 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)
4 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)
5 3 MAX SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis
6 4 MAX SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis
7 5 MAX SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis
8 6 MAX TOTAL_BATT_I 12 mA cubesatsim_current NONE 4 2 3 Current Total Battery DC current
9 7 MAX Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 MAX PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X Panel
11 9 MAX PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X Panel
12 10 MAX PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y Panel
13 11 MAX PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y Panel
14 12 MAX PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z Panel
15 13 MAX PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z Panel
16 14 MAX PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current +X Panel
17 15 MAX PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current -X Panel
18 16 MAX PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current +Y Panel
19 17 MAX PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current -Y Panel
20 18 MAX PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current +Z Panel
21 19 MAX PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current -Z Panel
22 20 MAX PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Voltage Power Supply Voltage
23 21 MAX SPIN 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MAX Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 MAX Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude STEM Payload Sensor Altitude
26 24 MAX Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MAX RSSI 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MAX IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 Temperature Internal Temperature of IHU
29 27 MAX SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation Angular Veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 MAX Sensor1 12 raw cubesatsim_temperature NONE 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 MAX PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 Current Power Supply DC Current
34 32 MAX Sensor2 12 signed raw cubesatsim_sensor2|INT NONE 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 MAX Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
36 34 MAX STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MAX Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 MAX PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 MAX PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator
40 38 MAX I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MAX I2CBus1Failure 1 - 17 NONE 2 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MAX I2CBus3Failure 1 - 17 NONE 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MAX CameraFailure 1 - 17 NONE 2 5 0 Camera Camera failure indicator
44 42 MAX GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MAX RXAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MAX TXAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MAX Pad 58 - 0 NONE 0 0 0 NONE NONE

47
spacecraft/FoxTelem_11a/CubeSatSim_mintelemetry.csv
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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
1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHOMIN_NAME 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)
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)
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)
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis
8 6 MIN TOTAL_BATT_I 12 mA cubesatsim_current NONE 4 2 3 Current Total Battery DC current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 MIN PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X Panel
11 9 MIN PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X Panel
12 10 MIN PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y Panel
13 11 MIN PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y Panel
14 12 MIN PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z Panel
15 13 MIN PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z Panel
16 14 MIN PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current +X Panel
17 15 MIN PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current -X Panel
18 16 MIN PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current +Y Panel
19 17 MIN PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current -Y Panel
20 18 MIN PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current +Z Panel
21 19 MIN PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current -Z Panel
22 20 MIN PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Voltage Power Supply Voltage
23 21 MIN SPIN 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MIN Pressure 12 bar cubesatsim_pressure NONE 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 MIN Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude STEM Payload Sensor Altitude
26 24 MIN Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MIN RSSI 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MIN IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 Temperature Internal Temperature of IHU
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation Angular Veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 MIN Sensor1 12 raw cubesatsim_temperature NONE 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 MIN PSUCurrent 12 mA cubesatsim_current NONE 5 2 3 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
35 33 MIN Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 NONE 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MIN Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 MIN PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 MIN PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator
40 38 MIN I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MIN I2CBus1Failure 1 - 17 NONE 2 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MIN I2CBus3Failure 1 - 17 NONE 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MIN CameraFailure 1 - 17 NONE 2 5 0 Camera Camera failure indicator
44 42 MIN GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MIN RXAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MIN TXAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MIN Pad 58 - 0 NONE 0 0 0 NONE NONE

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spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
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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
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,Sensor1,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,Humidity
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 1,STEM Payload Extra Sensor 1
33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
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
2 0 RT BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Battery A voltage (0-2.5V scale)
3 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)
4 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)
5 3 RT SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration Acceleration around X Axis
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
7 5 RT SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration Acceleration around Z Axis
8 6 RT TOTAL_BATT_I 12 mA cubesatsim_current Battery 4 2 3 Current Total Battery DC current
9 7 RT Temperature 12 C cubesatsim_temperature Experiments 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X Panel
11 9 RT PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage -X Panel
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y Panel
13 11 RT PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage -Y Panel
14 12 RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z Panel
15 13 RT PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage -Z Panel
16 14 RT PANEL_PLUS_X_I 12 mA cubesatsim_current +X Panel 7 2 3 Current +X Panel
17 15 RT PANEL_MINUS_X_I 12 mA cubesatsim_current -X Panel 10 2 3 Current -X Panel
18 16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_current +Y Panel 8 2 3 Current +Y Panel
19 17 RT PANEL_MINUS_Y_I 12 mA cubesatsim_current -Y Panel 11 2 3 Current -Y Panel
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_current +Z Panel 9 2 3 Current +Z Panel
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_current -Z Panel 12 2 3 Current -Z Panel
22 20 RT PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply Voltage
23 21 RT SPIN 12 rpm cubesatsim_rpm Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 RT Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 Pressure STEM Payload Sensor Pressure
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 % cubesatsim_temperature Experiments 6 5 3 Humidity Humidity
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 1 STEM Payload Extra Sensor 1
35 33 RT Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 2 STEM Payload Extra Sensor 2
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
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