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Update CubeSatSim_PSK_rttelemetry.csv add Sensors 2,3 Bat2

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beta-ft2
Alan Johnston 1 year ago committed by GitHub
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spacecraft/FoxTelem_1.13e/CubeSatSim_PSK_rttelemetry.csv
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@ -1,11 +1,11 @@
60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,realTime,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale)
1,realTime,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,INA219 Battery A+B+C Voltage
0,realTime,Sensor2,12,integer,1,Experiments,6,8,3,Sensor2,STEM Payload Extra Sensor2
1,realTime,Sensor3,12,integer,1,Experiments,6,8,3,Sensor3,STEM Payload Extra Sensor3
2,realTime,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,realTime,battCurr,12,mA,cubesatsim_current,Battery,4,2,3,Current,INA219 Total Battery DC Current
6,realTime,BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Battery Current,INA219 Battery Current
7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
8,realTime,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage
9,realTime,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage
@ -19,7 +19,7 @@
17,realTime,negXi,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,INA219 -X solar panel Current
18,realTime,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y solar panel Current
19,realTime,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z solar panel Current
20,realTime,BATT2Voltage,12,V,cubesatsim_voltage|FLOAT2,BAT2,5,1,3,Voltage,INA219 Power Supply Voltage
20,realTime,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
21,realTime,spin,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,realTime,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure
23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude
@ -30,9 +30,9 @@
28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
30,realTime,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,BME280 Humidity
31,realTime,BAT2Current,12,mA,cubesatsim_current,BAT2,5,2,3,Current,INA219 Power Supply DC Current
32,realTime,Sensor1,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload extra Sensor 1 (Diode Temperature)
33,realTime,Sensor2,12,signed scaled,cubesatsim_rpm,Experiments,6,7,3,Sensor 2,STEM Payload extra Sensor 2
31,realTime,BAT2_I,12,mA,cubesatsim_current,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
32,realTime,DiodeTemp,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,realTime,Sensor1,12,signed scaled,cubesatsim_rpm,Experiments,6,7,3,Sensor 1,STEM Payload extra Sensor 1
34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator
35,realTime,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,realTime,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator

1 60 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 realTime BATT_A_V Sensor2 12 V integer cubesatsim_voltage|FLOAT2 1 NONE Experiments 4 6 1 8 3 Cell A Sensor2 Battery A voltage (0-2.5V scale) STEM Payload Extra Sensor2
3 1 realTime BATT_B_V Sensor3 12 V integer cubesatsim_voltage|FLOAT2 1 NONE Experiments 4 6 2 8 3 Cell A+B Sensor3 Battery A+B voltage (0-3.3V scale) STEM Payload Extra Sensor3
4 2 realTime BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Cell A+B+C Voltage Battery Voltage INA219 Battery A+B+C Voltage INA219 Battery Voltage
5 3 realTime SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 realTime SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 realTime SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 realTime battCurr BATT_I 12 mA cubesatsim_current Battery 4 2 3 Current Battery Current INA219 Total Battery DC Current INA219 Battery Current
9 7 realTime Temperature 12 C cubesatsim_temperature Experiments 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 realTime posXv 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 realTime posYv 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage INA219 +Y solar panel Voltage
19 17 realTime negXi 12 mA cubesatsim_current -X Panel 10 2 3 Current INA219 -X solar panel Current
20 18 realTime negYi 12 mA cubesatsim_current -Y Panel 11 2 3 Current INA219 -Y solar panel Current
21 19 realTime negZi 12 mA cubesatsim_current -Z Panel 12 2 3 Current INA219 -Z solar panel Current
22 20 realTime BATT2Voltage BATT2_V 12 V cubesatsim_voltage|FLOAT2 BAT2 Battery2 5 1 3 Voltage Battery2 Voltage INA219 Power Supply Voltage INA219 Battery2 Voltage
23 21 realTime spin 12 rpm cubesatsim_rpm Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 realTime Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 realTime Altitude 12 m cubesatsim_altitude Experiments 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
30 28 realTime SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 realTime SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 realTime Humidity 12 % cubesatsim_temperature Experiments 6 5 3 BME280 Humidity BME280 Humidity
33 31 realTime BAT2Current BAT2_I 12 mA cubesatsim_current BAT2 Battery2 5 2 3 Current Battery2 Current INA219 Power Supply DC Current INA219 Battery2 Current
34 32 realTime Sensor1 DiodeTemp 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temp STEM Payload extra Sensor 1 (Diode Temperature) STEM Payload Diode Temperature
35 33 realTime Sensor2 Sensor1 12 signed scaled cubesatsim_rpm Experiments 6 7 3 Sensor 2 Sensor 1 STEM Payload extra Sensor 2 STEM Payload extra Sensor 1
36 34 realTime STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
37 35 realTime SafeMode 1 - STATUS_ON_OFF Computer Software 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 realTime SimulatedTelemetry 1 - STATUS_ON_OFF Computer Software 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
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