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Update PacSatSim_rttelemetry.csv from pacsat-v2.2-tlm2

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pacsat-v2.2-tlm3
Alan Johnston 4 weeks ago committed by GitHub
parent 50c51e8993
commit 54f2e5eb37
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1 changed files with 5 additions and 6 deletions
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spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv
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@ -1,12 +1,12 @@
62,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,long,timestamp,32,Sec,0,NONE,0,0,0,timestamp,This is the unix time in seconds
1,int,Sensor 2,12,1,1,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
2,int,Sensor 3,12,1,1,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
1,int,Sensor 2,12,integer,2,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
2,int,Sensor 3,12,integer,2,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
3,float,BATT_V,12,V,29,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
4,float,SatelliteXAxisAcceleration,12,g,30,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
5,float,SatelliteYAxisAcceleration,12,g,30,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
6,float,SatelliteZAxisAcceleration,12,g,30,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
7,float,BATT_I,12,mA,31,Battery,4,2,3,Battery Current,INA219 Battery Current
7,int,BATT_I,12,mA,31,Battery,4,2,3,Battery Current,INA219 Battery Current
8,float,Temperature,12,C,5,Experiments,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
9,float,posXv,12,V,29,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage
10,float,posYv,12,V,29,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage
@ -31,9 +31,9 @@
29,float,SatelliteYAxisAngularVelocity,12,dps,31,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
30,float,SatelliteZAxisAngularVelocity,12,dps,31,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
31,float,Humidity,12,%,5,Experiments,6,5,3,BME280 Humidity,BME280 Humidity
32,float,BAT2_I,12,mA,31,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
32,int,BAT2_I,12,mA,31,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
33,float,DiodeTemp,12,C,32,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature
34,int,Sensor 1,12,integer,1,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,int,Sensor 1,12,integer,2,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
35,float,STEMPayloadStatus,1,-,35,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator
36,float,SafeMode,1,-,33,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
37,float,SimulatedTelemetry,1,-,33,Computer Software,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator
@ -61,4 +61,3 @@
59,float,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
60,float,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
61,float,pad2,27,-,0,NONE,0,0,0,NONE,Filler

1 62 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 long timestamp 32 Sec 0 NONE 0 0 0 timestamp This is the unix time in seconds
3 1 int Sensor 2 12 1 integer 1 2 Experiments 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
4 2 int Sensor 3 12 1 integer 1 2 Experiments 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
5 3 float BATT_V 12 V 29 Battery 4 1 3 Battery Voltage INA219 Battery Voltage
6 4 float SatelliteXAxisAcceleration 12 g 30 +X Panel 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
7 5 float SatelliteYAxisAcceleration 12 g 30 +Y Panel 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
8 6 float SatelliteZAxisAcceleration 12 g 30 +Z Panel 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
9 7 float int BATT_I 12 mA 31 Battery 4 2 3 Battery Current INA219 Battery Current
10 8 float Temperature 12 C 5 Experiments 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
11 9 float posXv 12 V 29 +X Panel 7 1 3 Voltage INA219 +X solar panel Voltage
12 10 float posYv 12 V 29 +Y Panel 8 1 3 Voltage INA219 +Y solar panel Voltage
31 29 float SatelliteYAxisAngularVelocity 12 dps 31 +Y Panel 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
32 30 float SatelliteZAxisAngularVelocity 12 dps 31 +Z Panel 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
33 31 float Humidity 12 % 5 Experiments 6 5 3 BME280 Humidity BME280 Humidity
34 32 float int BAT2_I 12 mA 31 Battery2 5 2 3 Battery2 Current INA219 Battery2 Current
35 33 float DiodeTemp 12 C 32 Experiments 6 6 3 Diode Temp STEM Payload Diode Temperature
36 34 int Sensor 1 12 integer 1 2 Experiments 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
37 35 float STEMPayloadStatus 1 - 35 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
38 36 float SafeMode 1 - 33 Computer Software 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
39 37 float SimulatedTelemetry 1 - 33 Computer Software 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
61 59 float hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
62 60 float swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
63 61 float pad2 27 - 0 NONE 0 0 0 NONE Filler
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