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Update CubeSatSim_rttelemetry.csv revert

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beta-ft2
Alan Johnston 1 year ago committed by GitHub
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spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv
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@ -1,47 +1,47 @@
46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMIN_NAME,DESCRIPTION
0,MIN,SENSOR2,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor2,STEM Payload Extra Sensor2
1,MIN,SENSOR3,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor3,STEM Payload Extra Sensor3
2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,Battery Voltage
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,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,Battery 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,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery2 Voltage,Battery2 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,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,STEM Payload Sensor Humidity
31,MIN,BATT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery2 Current,Power Supply DC Current
32,MIN,DIODE_T,12,signed raw,cubesatsim_rpm,NONE,6,6,3,Diode Temperature,Diode Temperature
33,MIN,Sensor1,12,signed scaled,cubesatsim_rpm,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
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,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,INA219 Battery A+B+C Voltage
3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,RT,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total INA219 Battery DC Current
7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,STEM Payload Sensor BME280 Temperature
8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X Panel Voltage
9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,INA219 -X Panel Voltage
10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,INA219 +Y Panel Voltage
11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,INA219 -Y Panel Voltage
12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,INA219 +Z Panel Voltage
13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,INA219 -Z Panel Voltage
14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,INA219 +X Panel Current
15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,INA219 -X Panel Current
16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,INA219 +Y Panel Current
17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y Panel Current
18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,INA219 +Z Panel Current
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z Panel Current
20,RT,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,INA219 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,BME280 Pressure,STEM Payload Sensor BME280 Pressure
23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 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,IHU Temp (Pi),Internal Temperature of Pi IHU
27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Z Axis
30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,STEM Payload Sensor BME280 Humidity
31,RT,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,INA219 Power Supply DC Current
32,RT,Sensor1,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Extra Sensor 1 (Diode Temperature)
33,RT,Sensor2,12,signed scaled,cubesatsim_rpm,Experiments,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status
35,RT,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,RT,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry, Simulated Telemetry Indicator
37,RT,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator
38,RT,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
41,RT,CameraFailure,1,-,17,Computer Hardware,2,4,0,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 SHOMIN_NAME SHORT_NAME DESCRIPTION
2 0 MIN RT SENSOR2 BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Sensor2 Cell A STEM Payload Extra Sensor2 Battery A voltage (0-2.5V scale)
3 1 MIN RT SENSOR3 BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Sensor3 Cell A+B STEM Payload Extra Sensor3 Battery A+B voltage (0-3.3V scale)
4 2 MIN RT BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE Battery 4 1 3 Battery Voltage Cell A+B+C Voltage Battery Voltage INA219 Battery A+B+C Voltage
5 3 MIN RT SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE +X Panel 7 4 3 Acceleration Acceleration Acceleration around X Axis STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MIN RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE +Y Panel 8 4 3 Acceleration Acceleration Acceleration around Y Axis STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MIN RT SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE +Z Panel 9 4 3 Acceleration Acceleration Acceleration around Z Axis STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MIN RT BATT_I TOTAL_BATT_I 12 mA cubesatsim_current NONE Battery 4 2 3 Battery Current Current Battery current Total INA219 Battery DC Current
9 7 MIN RT Temperature 12 C cubesatsim_temperature NONE Experiments 6 2 3 Temperature BME280 Temp STEM Payload Sensor Temperature STEM Payload Sensor BME280 Temperature
10 8 MIN RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE +X Panel 7 1 3 Voltage Voltage +X Panel INA219 +X Panel Voltage
11 9 MIN RT PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE -X Panel 10 1 3 Voltage Voltage -X Panel INA219 -X Panel Voltage
12 10 MIN RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE +Y Panel 8 1 3 Voltage Voltage +Y Panel INA219 +Y Panel Voltage
13 11 MIN RT PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE -Y Panel 11 1 3 Voltage Voltage -Y Panel INA219 -Y Panel Voltage
14 12 MIN RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE +Z Panel 9 1 3 Voltage Voltage +Z Panel INA219 +Z Panel Voltage
15 13 MIN RT PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE -Z Panel 12 1 3 Voltage Voltage -Z Panel INA219 -Z Panel Voltage
16 14 MIN RT PANEL_PLUS_X_I 12 mA cubesatsim_current NONE +X Panel 7 2 3 Current Current +X Panel INA219 +X Panel Current
17 15 MIN RT PANEL_MINUS_X_I 12 mA cubesatsim_current NONE -X Panel 10 2 3 Current Current -X Panel INA219 -X Panel Current
18 16 MIN RT PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE +Y Panel 8 2 3 Current Current +Y Panel INA219 +Y Panel Current
19 17 MIN RT PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE -Y Panel 11 2 3 Current Current -Y Panel INA219 -Y Panel Current
20 18 MIN RT PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE +Z Panel 9 2 3 Current Current +Z Panel INA219 +Z Panel Current
21 19 MIN RT PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE -Z Panel 12 2 3 Current Current -Z Panel INA219 -Z Panel Current
22 20 MIN RT BATT2_V PSUVoltage 12 V cubesatsim_voltage|FLOAT2 NONE PSU 5 1 3 Battery2 Voltage Voltage Battery2 Voltage INA219 Power Supply Voltage
23 21 MIN RT SPIN 12 rpm cubesatsim_rpm NONE Computer Software 3 1 3 Spacecraft Spin Spacecraft Spin Calculated spin rate using solar cells
24 22 MIN RT Pressure 12 bar hPa cubesatsim_pressure NONE Experiments 6 3 3 Pressure BME280 Pressure STEM Payload Sensor Pressure STEM Payload Sensor BME280 Pressure
25 23 MIN RT Altitude 12 m cubesatsim_altitude NONE Experiments 6 4 3 Altitude BME280 Altitude STEM Payload Sensor Altitude STEM Payload Sensor BME280 Altitude
26 24 MIN RT Resets 12 - 12 NONE 3 2 3 Reset Count Reset Count Software Reset Count
27 25 MIN RT RSSI 12 dBm cubesatsim_rssi|INT NONE Radio 1 1 3 RSSI RSSI Received Signal Strength Indication
28 26 MIN RT IHUTemperature 12 C cubesatsim_temperature NONE Computer Hardware 2 1 3 Temperature IHU Temp (Pi) Internal Temperature of IHU Internal Temperature of Pi IHU
29 27 MIN RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE +X Panel 7 3 3 Rotation Rotation Angular Veolcity around X Axis STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 MIN RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE +Y Panel 8 3 3 Rotation Rotation Angular Veolcity around Y Axis STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 MIN RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE +Z Panel 9 3 3 Rotation Rotation Angular Veolcity around Z Axis STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 MIN RT Humidity 12 % cubesatsim_temperature NONE Experiments 6 5 3 Humidity BME280 Humidity STEM Payload Sensor Humidity STEM Payload Sensor BME280 Humidity
33 31 MIN RT BATT2_I PSUCurrent 12 mA cubesatsim_current NONE PSU 5 2 3 Battery2 Current Current Power Supply DC Current INA219 Power Supply DC Current
34 32 MIN RT DIODE_T Sensor1 12 signed raw C cubesatsim_rpm NONE Experiments 6 6 3 Diode Temperature Diode Temp Diode Temperature STEM Payload Extra Sensor 1 (Diode Temperature)
35 33 MIN RT Sensor1 Sensor2 12 signed scaled cubesatsim_rpm NONE Experiments 6 7 3 Sensor 1 Sensor 2 STEM Payload Extra Sensor 1 STEM Payload Extra Sensor 2
36 34 MIN RT STEMPayloadStatus 1 - 17 NONE Experiments 6 1 0 STEM Payload Status STEM Payload Status STEM Payload Board Status
37 35 MIN RT Nominal Mode SafeMode 1 - 17 STATUS_ON_OFF NONE Computer Software 3 2 0 Nominal Mode Safe Mode Nominal Mode (Not Safe Mode) Safe Mode (Low Battery Voltage)
38 36 MIN RT PayloadStatus1 SimulatedTelemetry 1 - 17 STATUS_ON_OFF NONE Computer Software 6 3 7 4 0 Exp 2 Simulated Telemetry STEM Payload status 1 failure indicator Simulated Telemetry Indicator
39 37 MIN RT PayloadStatus2 PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 Exp 3 STEM Payload status 2 failure indicator STEM Payload status 1 failure indicator
40 38 MIN RT I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MIN RT I2CBus1Failure 1 - 17 NONE Computer Hardware 2 3 2 0 I2C Bus 1 I2C Bus 1 I2C bus 1 failure indicator
42 40 MIN RT I2CBus3Failure 1 - 17 NONE Computer Hardware 2 4 3 0 I2C Bus 3 I2C Bus 3 I2C bus 3 failure indicator
43 41 MIN RT CameraFailure 1 - 17 NONE Computer Hardware 2 5 4 0 Camera Camera Camera failure indicator
44 42 MIN RT GroundCommands 4 - 1 NONE Computer Software 3 3 0 Ground Commands Ground Commands Number of ground commands received
45 43 MIN RT RXAntenna 1 - 16 NONE Radio 1 3 0 RX Antenna RX Antenna Receive antenna status
46 44 MIN RT TXAntenna 1 - 16 NONE Radio 1 2 0 TX Antenna TX Antenna Transmit antenna status
47 45 MIN RT Pad 58 - 0 NONE 0 0 0 NONE NONE NONE
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