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Update PacSatSim_rttelemetry.csv change battery currents to int

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pacsat-v2.2-tlm2
Alan Johnston 4 weeks ago committed by GitHub
parent 49550fa748
commit e9b1329e48
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1 changed files with 3 additions and 2 deletions
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spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv
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@ -6,7 +6,7 @@
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
@ -31,7 +31,7 @@
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,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
@ -63,3 +63,4 @@
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
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 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
63 61 float pad2 27 - 0 NONE 0 0 0 NONE Filler
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