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Update CubeSatSim_PSK_rttelemetry.csv changed to Battery2

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beta-ft2
Alan Johnston 1 year ago committed by GitHub
parent 0c87fdb69d
commit 16c4b19bf3
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1 changed files with 2 additions and 2 deletions
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spacecraft/FoxTelem_1.13e/CubeSatSim_PSK_rttelemetry.csv
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@ -19,7 +19,7 @@
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|FLOAT2,Battery 2,5,1,3,Battery 2 Voltage,INA219 Battery 2 Voltage
20,realTime,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,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
@ -30,7 +30,7 @@
28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
30,realTime,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,BME280 Humidity
31,realTime,BAT2_I,12,mA,cubesatsim_current,Battery 2,5,2,3,Battery 2 Current,INA219 Battery 2 Current
31,realTime,BAT2_I,12,mA,cubesatsim_current,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
32,realTime,DiodeTemp,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature
33,realTime,Sensor 1,12,integer,1,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
34,realTime,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator

1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
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|FLOAT2 Battery 2 Battery2 5 1 3 Battery 2 Voltage Battery2 Voltage INA219 Battery 2 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
30 28 realTime SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 realTime SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 realTime Humidity 12 % cubesatsim_temperature Experiments 6 5 3 BME280 Humidity BME280 Humidity
33 31 realTime BAT2_I 12 mA cubesatsim_current Battery 2 Battery2 5 2 3 Battery 2 Current Battery2 Current INA219 Battery 2 Current INA219 Battery2 Current
34 32 realTime DiodeTemp 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 realTime Sensor 1 12 integer 1 Experiments 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 realTime STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
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