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cleanup to align with rtt

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alanbjohnston 5 years ago committed by GitHub
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spacecraft/FoxTelem_1.09m/CubeSatSim_PSK_wodtelemetry.csv
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@ -1,12 +1,12 @@
60,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery pair A voltage (0-2.5V scale)
1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale)
1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A + B,Battery A+B voltage (0-3.3V scale)
2,WOD,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,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
5,WOD,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
6,WOD,battCurr,12,mA,cubesatsim_current,Battery,4,2,4,Current,Total Battery DC current
7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temp,STEM Payload Sensor Temperature
7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature
8,WOD,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage
9,WOD,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage
10,WOD,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage
@ -19,7 +19,7 @@
17,WOD,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar Panel current
18,WOD,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar Panel current
19,WOD,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,Current,-Z solar Panel current
20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Board Voltage,Power Supply Voltage
20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage
21,WOD,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,WOD,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure
23,WOD,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude
@ -32,7 +32,7 @@
30,WOD,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,WOD,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,WOD,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,WOD,Sensor3,12,signed raw,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
33,WOD,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
35,WOD,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,WOD,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator

1 60 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 WOD BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A Battery pair A voltage (0-2.5V scale) Battery A voltage (0-2.5V scale)
3 1 WOD BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 2 3 Cell A + B Battery pairs A+B voltage (0-3.3V scale) Battery A+B voltage (0-3.3V scale)
4 2 WOD 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 WOD SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration Acceleration around X Axis
6 4 WOD SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
7 5 WOD SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration Acceleration around Z Axis
8 6 WOD battCurr 12 mA cubesatsim_current Battery 4 2 4 Current Total Battery DC current
9 7 WOD Temperature 12 C cubesatsim_temperature Experiments 6 2 3 Temp Temperature STEM Payload Sensor Temperature
10 8 WOD posXv 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X solar Panel voltage
11 9 WOD posYv 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y solar Panel voltage
12 10 WOD posZv 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z solar Panel voltage
19 17 WOD negXi 12 mA cubesatsim_current -X Panel 10 2 4 Current -X solar Panel current
20 18 WOD negYi 12 mA cubesatsim_current -Y Panel 11 2 4 Current -Y solar Panel current
21 19 WOD negZi 12 mA cubesatsim_current -Z Panel 12 2 4 Current -Z solar Panel current
22 20 WOD PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Board Voltage Voltage Power Supply Voltage
23 21 WOD spin 12 rpm 12 Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 WOD Pressure 12 bar cubesatsim_pressure Experiments 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 WOD Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude STEM Payload Sensor Altitude
32 30 WOD Sensor1 12 raw cubesatsim_sensor1|INT Experiments 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 WOD PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 WOD Sensor2 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 WOD Sensor3 12 signed raw signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
36 34 WOD STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload Board Failure Indicator
37 35 WOD Nominal Mode 1 - 17 Computer Software 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 WOD PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
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