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added INA, MPU, and BME labels, and Safe Mode

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alanbjohnston 5 years ago committed by GitHub
parent 75601fd028
commit 9831c7a498
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1 changed files with 27 additions and 27 deletions
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spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
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@ -1,41 +1,41 @@
46,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,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V 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) 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) 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,MPU6050 Acceleration,MPU6050 Acceleration around X Axis 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,MPU6050 Acceleration,MPU6050 Acceleration around Y 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,MPU6050 Acceleration,MPU6050 Acceleration around Z 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 Battery DC current 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 Temperature,STEM Payload Sensor BME280 Temperature 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,+X Panel 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,-X Panel 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,+Y Panel 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,-Y Panel 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,+Z Panel 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,-Z Panel 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,+X Panel 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,-X Panel 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,+Y Panel 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,-Y Panel 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,+Z Panel 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,-Z Panel 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,Power Supply Voltage 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 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,BME280 Pressure,STEM Payload Sensor BME280 Pressure 22,RT,Pressure,12,bar,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 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 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 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 Temperature (Pi),Internal Temperature of Pi IHU 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,MPU6050 Rotation,MPU6050 Angular Veolcity around X Axis 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,MPU6050 Rotation,MPU6050 Angular Veolcity around Y 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,MPU6050 Rotation,MPU6050 Angular Veolcity around Z 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 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,Power Supply DC Current 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 Temperature,STEM Payload Extra Sensor 1 (Diode Temperature) 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 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,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) 35,RT,SafeMode,1,-,17,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,RT,SimulatedTelemetry,1,-,17,Computer Software,3,4,0,Simulated Telemetry, Simulated Telemetry indicator 36,RT,SimulatedTelemetry,1,-,17,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 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 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 39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator

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) INA219 Battery A+B+C Voltage
5 3 RT SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 MPU6050 Acceleration Acceleration MPU6050 Acceleration around X Axis STEM Payload Board MPU6050 Acceleration around X Axis
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 MPU6050 Acceleration Acceleration MPU6050 Acceleration around Y Axis STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 RT SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 MPU6050 Acceleration Acceleration MPU6050 Acceleration around Z Axis STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 RT TOTAL_BATT_I 12 mA cubesatsim_current Battery 4 2 3 Current Total Battery DC current Total INA219 Battery DC Current
9 7 RT Temperature 12 C cubesatsim_temperature Experiments 6 2 3 BME280 Temperature BME280 Temp STEM Payload Sensor BME280 Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X Panel INA219 +X Panel Voltage
11 9 RT PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage -X Panel INA219 -X Panel Voltage
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y Panel INA219 +Y Panel Voltage
13 11 RT PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage -Y Panel INA219 -Y Panel Voltage
14 12 RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z Panel INA219 +Z Panel Voltage
15 13 RT PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage -Z Panel INA219 -Z Panel Voltage
16 14 RT PANEL_PLUS_X_I 12 mA cubesatsim_current +X Panel 7 2 3 Current +X Panel INA219 +X Panel Current
17 15 RT PANEL_MINUS_X_I 12 mA cubesatsim_current -X Panel 10 2 3 Current -X Panel INA219 -X Panel Current
18 16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_current +Y Panel 8 2 3 Current +Y Panel INA219 +Y Panel Current
19 17 RT PANEL_MINUS_Y_I 12 mA cubesatsim_current -Y Panel 11 2 3 Current -Y Panel INA219 -Y Panel Current
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_current +Z Panel 9 2 3 Current +Z Panel INA219 +Z Panel Current
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_current -Z Panel 12 2 3 Current -Z Panel INA219 -Z Panel Current
22 20 RT PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply Voltage INA219 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 bar cubesatsim_pressure Experiments 6 3 3 BME280 Pressure STEM Payload Sensor BME280 Pressure
25 23 RT Altitude 12 m cubesatsim_altitude Experiments 6 4 3 BME280 Altitude STEM Payload Sensor BME280 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 IHU Temperature (Pi) IHU Temp (Pi) Internal Temperature of Pi IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 MPU6050 Rotation Rotation MPU6050 Angular Veolcity around X Axis STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 MPU6050 Rotation Rotation MPU6050 Angular Veolcity around Y Axis STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 MPU6050 Rotation Rotation MPU6050 Angular Veolcity around Z Axis STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 RT Humidity 12 % cubesatsim_temperature Experiments 6 5 3 BME280 Humidity STEM Payload Sensor BME280 Humidity
33 31 RT PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current INA219 Power Supply DC Current
34 32 RT Sensor1 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temperature Diode Temp STEM Payload Extra Sensor 1 (Diode Temperature)
35 33 RT Sensor2 12 signed scaled cubesatsim_rpm 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 SafeMode 1 - 17 Computer Software 3 2 0 Nominal Mode Safe Mode Nominal Mode (Not Safe Mode) Safe Mode (Low Battery Voltage)
38 36 RT SimulatedTelemetry 1 - 17 Computer Software 3 4 0 Simulated Telemetry Simulated Telemetry indicator Simulated Telemetry Indicator
39 37 RT PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 1 failure indicator
40 38 RT I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 RT I2CBus1Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
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