Update PacSatSim_rttelemetry.csv changed voltage to 29

pacsat-v2.2-tlm
Alan Johnston 2 months ago committed by GitHub
parent 1fbee01b9d
commit 21ab4e1f18
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GPG Key ID: B5690EEEBB952194

@ -1,25 +1,25 @@
61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,realTime,Sensor 2,12,integer,1,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
1,realTime,Sensor 3,12,integer,1,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
2,realTime,BATT_V,12,V,cubesatsim_voltage,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
2,realTime,BATT_V,12,V,29,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,realTime,BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Battery Current,INA219 Battery Current
7,realTime,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
8,realTime,posXv,12,V,cubesatsim_voltage,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage
9,realTime,posYv,12,V,cubesatsim_voltage,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage
10,realTime,posZv,12,V,cubesatsim_voltage,+Z Panel,9,1,3,Voltage,INA219 +Z solar panel Voltage
11,realTime,negXv,12,V,cubesatsim_voltage,-X Panel,10,1,3,Voltage,INA219 -X solar panel Voltage
12,realTime,negYv,12,V,cubesatsim_voltage,-Y Panel,11,1,3,Voltage,INA219 -Y solar panel Voltage
13,realTime,negZv,12,V,cubesatsim_voltage,-Z Panel,12,1,3,Voltage,INA219 -Z solar panel Voltage
8,realTime,posXv,12,V,29,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage
9,realTime,posYv,12,V,29,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage
10,realTime,posZv,12,V,29,+Z Panel,9,1,3,Voltage,INA219 +Z solar panel Voltage
11,realTime,negXv,12,V,29,-X Panel,10,1,3,Voltage,INA219 -X solar panel Voltage
12,realTime,negYv,12,V,29,-Y Panel,11,1,3,Voltage,INA219 -Y solar panel Voltage
13,realTime,negZv,12,V,29,-Z Panel,12,1,3,Voltage,INA219 -Z solar panel Voltage
14,realTime,posXi,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,INA219 +X solar panel Current
15,realTime,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,INA219 +Y solar panel Current
16,realTime,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,INA219 +Z solar panel Current
17,realTime,negXi,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,INA219 -X solar panel Current
18,realTime,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y solar panel Current
19,realTime,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z solar panel Current
20,realTime,BATT2_V,12,V,cubesatsim_voltage,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
20,realTime,BATT2_V,12,V,29,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
21,realTime,spin,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,realTime,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure
23,realTime,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude
@ -61,3 +61,4 @@
59,realTime,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
60,realTime,pad2,27,-,0,NONE,0,0,0,NONE,Filler

1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 realTime Sensor 2 12 integer 1 Experiments 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 realTime Sensor 3 12 integer 1 Experiments 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 realTime BATT_V 12 V cubesatsim_voltage 29 Battery 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 realTime SatelliteXAxisAcceleration 12 g cubesatsim_acceleration +X Panel 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 realTime SatelliteYAxisAcceleration 12 g cubesatsim_acceleration +Y Panel 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 realTime SatelliteZAxisAcceleration 12 g cubesatsim_acceleration +Z Panel 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 realTime BATT_I 12 mA cubesatsim_current Battery 4 2 3 Battery Current INA219 Battery Current
9 7 realTime Temperature 12 C cubesatsim_temperature Experiments 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 realTime posXv 12 V cubesatsim_voltage 29 +X Panel 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 realTime posYv 12 V cubesatsim_voltage 29 +Y Panel 8 1 3 Voltage INA219 +Y solar panel Voltage
12 10 realTime posZv 12 V cubesatsim_voltage 29 +Z Panel 9 1 3 Voltage INA219 +Z solar panel Voltage
13 11 realTime negXv 12 V cubesatsim_voltage 29 -X Panel 10 1 3 Voltage INA219 -X solar panel Voltage
14 12 realTime negYv 12 V cubesatsim_voltage 29 -Y Panel 11 1 3 Voltage INA219 -Y solar panel Voltage
15 13 realTime negZv 12 V cubesatsim_voltage 29 -Z Panel 12 1 3 Voltage INA219 -Z solar panel Voltage
16 14 realTime posXi 12 mA cubesatsim_current +X Panel 7 2 3 Current INA219 +X solar panel Current
17 15 realTime posYi 12 mA cubesatsim_current +Y Panel 8 2 3 Current INA219 +Y solar panel Current
18 16 realTime posZi 12 mA cubesatsim_current +Z Panel 9 2 3 Current INA219 +Z solar panel Current
19 17 realTime negXi 12 mA cubesatsim_current -X Panel 10 2 3 Current INA219 -X solar panel Current
20 18 realTime negYi 12 mA cubesatsim_current -Y Panel 11 2 3 Current INA219 -Y solar panel Current
21 19 realTime negZi 12 mA cubesatsim_current -Z Panel 12 2 3 Current INA219 -Z solar panel Current
22 20 realTime BATT2_V 12 V cubesatsim_voltage 29 Battery2 5 1 3 Battery2 Voltage INA219 Battery2 Voltage
23 21 realTime spin 12 rpm cubesatsim_rpm Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 realTime Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 realTime Altitude 12 m cubesatsim_altitude Experiments 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
61 59 realTime swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
62 60 realTime pad2 27 - 0 NONE 0 0 0 NONE Filler
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