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added INT to Sensor 1 and FLOAT2 to Sensor 3

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alanbjohnston 5 years ago committed by GitHub
parent b64fd61631
commit f55727888d
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1 changed files with 3 additions and 3 deletions
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spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
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@ -19,7 +19,7 @@
17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,3,Current,-Y Panel 17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_ina219_current,-Y Panel,11,2,3,Current,-Y Panel
18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel 18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_ina219_current,+Z Panel,9,2,3,Current,+Z Panel
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,12,2,3,Current,-Z Panel
20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage | FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage
21,RT,SPIN,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 21,RT,SPIN,12,rpm,12,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 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 23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude
@ -29,10 +29,10 @@
27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis
30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 30,RT,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,5,2,3,Current,Power Supply DC Current
32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused 34,RT,Unused,8,na,7,NONE,0,0,0,Unused,Unused
35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status 35,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status
36,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) 36,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)

1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
19 17 RT PANEL_MINUS_Y_I 12 mA cubesatsim_ina219_current -Y Panel 11 2 3 Current -Y Panel
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_ina219_current +Z Panel 9 2 3 Current +Z Panel
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_ina219_current -Z Panel 12 2 3 Current -Z Panel
22 20 RT PSUVoltage 12 V cubesatsim_ina219_voltage | FLOAT2 cubesatsim_ina219_voltage|FLOAT2 PSU 5 1 3 Board Voltage Power Supply Voltage
23 21 RT SPIN 12 rpm 12 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 STEM Payload Sensor Pressure
25 23 RT Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude STEM Payload Sensor Altitude
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation +X Panel 7 3 3 Rotation Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation +Y Panel 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation +Z Panel 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 RT Sensor1 12 raw cubesatsim_sensor1 cubesatsim_sensor1|INT Experiments 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 RT PSUCurrent 12 mA cubesatsim_ina219_current PSU 5 2 3 Current Power Supply DC Current
34 32 RT Sensor2 12 signed raw cubesatsim_sensor2 Experiments 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 RT Sensor3 12 signed scaled cubesatsim_sensor3 cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
36 34 RT Unused 8 na 7 NONE 0 0 0 Unused Unused
37 35 RT STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload Board Status
38 36 RT Nominal Mode 1 - 17 Computer Software 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
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