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fixed conversions for sensors

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pull/67/head
alanbjohnston 5 years ago committed by GitHub
parent dd83aa0531
commit 522d07b5e8
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GPG Key ID: 4AEE18F83AFDEB23
1 changed files with 5 additions and 5 deletions
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spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
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@ -6,7 +6,7 @@
4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis
5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis 5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis
6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,3,2,3,Current,Total Battery DC current 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,3,2,3,Current,Total Battery DC current
7,RT,Temperature,12,C,8,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature 7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature
8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,6,2,3,Voltage,+X Panel 8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,6,2,3,Voltage,+X Panel
9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,9,2,3,Voltage,-X Panel 9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,9,2,3,Voltage,-X Panel
10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,7,2,3,Voltage,+YPanel 10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,7,2,3,Voltage,+YPanel
@ -21,17 +21,17 @@
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel
20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage
21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells 21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells
22,RT,Pressure,12,bar,10,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure 22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure
23,RT,Altitude,12,m,7,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude
24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature 24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature
25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication 25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication
26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU
27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis
30,RT,Sensor1,12,raw,7,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1 30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current
32,RT,Sensor2,12,raw,7,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,RT,Unused,20,na,7,NONE,0,0,0,Unused,Unused 33,RT,Unused,20,na,7,NONE,0,0,0,Unused,Unused
34,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status 34,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status
35,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used 35,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used

1 45 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_rotation +Y Panel 7 4 3 Acceleration Acceleration around Y Axis
7 5 RT SatelliteZAxisAcceleration 12 g cubesatsim_rotation +Z Panel 8 4 3 Acceleration Acceleration around Z Axis
8 6 RT TOTAL_BATT_I 12 mA cubesatsim_ina219_current Battery 3 2 3 Current Total Battery DC current
9 7 RT Temperature 12 C 8 cubesatsim_temperature Experiments 5 2 3 Temp STEM Payload Sensor Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_ina219_voltage +X Panel 6 2 3 Voltage +X Panel
11 9 RT PANEL_MINUS_X_V 12 V cubesatsim_ina219_voltage -X Panel 9 2 3 Voltage -X Panel
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_ina219_voltage +Y Panel 7 2 3 Voltage +YPanel
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_ina219_current -Z Panel 11 1 3 Current -Z Panel
22 20 RT PSUVoltage 12 V cubesatsim_ina219_voltage PSU 4 2 3 Board Voltage Power Supply Voltage
23 21 RT SPIN 12 rpm 12 Computer 2 2 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 RT Pressure 12 bar 10 cubesatsim_pressure Experiments 5 3 3 Pressure STEM Payload Sensor Pressure
25 23 RT Altitude 12 m 7 cubesatsim_altitude Experiments 5 4 3 Altitude STEM Payload Sensor Altitude
26 24 RT RXTemperature 12 C 7 Radio 1 1 3 RX Temperature Receiver card temperature
27 25 RT RSSI 12 dBm 14 Radio 1 2 3 RSSI Received Signal Strength Indication
28 26 RT IHUTemperature 12 C cubesatsim_temperature Computer 2 1 3 Temperature Internal Temperature of IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation +X Panel 6 3 3 Rotation Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation +Y Panel 7 3 3 Rotation Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation +Z Panel 8 3 3 Rotation Angular Veolcity around Z Axis
32 30 RT Sensor1 12 raw 7 cubesatsim_sensor1 Experiments 5 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 RT PSUCurrent 12 mA cubesatsim_ina219_current PSU 4 1 3 Current Power Supply DC Current
34 32 RT Sensor2 12 raw signed raw 7 cubesatsim_sensor2 Experiments 5 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 RT Unused 20 na 7 NONE 0 0 0 Unused Unused
36 34 RT Experiment1FailureIndication 1 - 17 Experiments 5 1 0 STEM Payload Status STEM Payload Board Status
37 35 RT Experiment2FailureIndication 1 - 17 NONE 5 0 0 Not installed Not used
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