diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv b/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv index f9301dbe..cca6a65f 100644 --- a/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv @@ -1,34 +1,34 @@ 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|FLOAT2,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage -3,realTime,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis -4,realTime,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis -5,realTime,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis +2,realTime,BATT_V,12,V,cubesatsim_voltage,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|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage -9,realTime,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage -10,realTime,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,INA219 +Z solar panel Voltage -11,realTime,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,INA219 -X solar panel Voltage -12,realTime,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,INA219 -Y solar panel Voltage -13,realTime,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,INA219 -Z solar panel Voltage +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 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|FLOAT2,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage +20,realTime,BATT2_V,12,V,cubesatsim_voltage,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 24,realTime,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count -25,realTime,rssi,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication +25,realTime,rssi,12,dBm,cubesatsim_rssi,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,realTime,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi -27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis -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 +27,realTime,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis +28,realTime,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis +29,realTime,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+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,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 @@ -60,3 +60,4 @@ 58,realTime,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset 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 +