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added BME280 and MPU6050 to sensor names

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alanbjohnston 5 years ago committed by GitHub
parent b8590bb821
commit 1c4661fef7
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1 changed files with 11 additions and 11 deletions
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spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
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@ -2,11 +2,11 @@
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
3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,MPU6050 Acceleration,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
5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,MPU6050 Acceleration,MPU6050 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
7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temperature,STEM Payload Sensor BME280 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
@ -21,15 +21,15 @@
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,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
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
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,STEM Payload Sensor Humidity
26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,IHU Temperature (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
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,MPU6050 Rotation,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
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
32,RT,Sensor1,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temperature,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

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 MPU6050 Acceleration Acceleration around X Axis MPU6050 Acceleration around X Axis
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration MPU6050 Acceleration Acceleration around Y Axis MPU6050 Acceleration around Y Axis
7 5 RT SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration MPU6050 Acceleration Acceleration around Z Axis MPU6050 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 BME280 Temperature STEM Payload Sensor Temperature 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
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
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 bar cubesatsim_pressure Experiments 6 3 3 Pressure BME280 Pressure STEM Payload Sensor Pressure STEM Payload Sensor BME280 Pressure
25 23 RT Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude BME280 Altitude STEM Payload Sensor 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 Temperature IHU Temperature (Pi) Internal Temperature of IHU Internal Temperature of Pi IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation MPU6050 Rotation Angular Veolcity around X Axis MPU6050 Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation MPU6050 Rotation Angular Veolcity around Y Axis MPU6050 Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation MPU6050 Rotation Angular Veolcity around Z Axis MPU6050 Angular Veolcity around Z Axis
32 30 RT Humidity 12 % cubesatsim_temperature Experiments 6 5 3 Humidity BME280 Humidity STEM Payload Sensor Humidity STEM Payload Sensor BME280 Humidity
33 31 RT PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 RT Sensor1 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temperature 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
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