From d3f8697120116ba513f27809b152d3e2e551e5ef Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Fri, 6 Feb 2026 23:20:41 -0500 Subject: [PATCH] Add renamed BPSK telem files from FoxTelem --- .../PacSatSim_Type1_HEALTH.frame | 13 ++++ .../PacSatSim_Type2_MINMAX.frame | 13 ++++ .../PacSatSim_conversion_curves.csv | 13 ++++ .../PacSatSim_maxtelemetry.csv | 62 +++++++++++++++++++ .../PacSatSim_mintelemetry.csv | 62 +++++++++++++++++++ .../PacSatSim_rttelemetry.csv | 62 +++++++++++++++++++ .../PacSatSim_wodtelemetry.csv | 62 +++++++++++++++++++ 7 files changed, 287 insertions(+) create mode 100644 spacecraft/PacSatGround_0.46o/PacSatSim_Type1_HEALTH.frame create mode 100644 spacecraft/PacSatGround_0.46o/PacSatSim_Type2_MINMAX.frame create mode 100644 spacecraft/PacSatGround_0.46o/PacSatSim_conversion_curves.csv create mode 100644 spacecraft/PacSatGround_0.46o/PacSatSim_maxtelemetry.csv create mode 100644 spacecraft/PacSatGround_0.46o/PacSatSim_mintelemetry.csv create mode 100644 spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv create mode 100644 spacecraft/PacSatGround_0.46o/PacSatSim_wodtelemetry.csv diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_Type1_HEALTH.frame b/spacecraft/PacSatGround_0.46o/PacSatSim_Type1_HEALTH.frame new file mode 100644 index 00000000..050ff88a --- /dev/null +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_Type1_HEALTH.frame @@ -0,0 +1,13 @@ +number_of_payloads=6 +payload0.name=rttelemetry +payload0.length=78 +payload1.name=rttelemetry +payload1.length=78 +payload2.name=rttelemetry +payload2.length=78 +payload3.name=rttelemetry +payload3.length=78 +payload4.name=rttelemetry +payload4.length=78 +payload5.name=wodtelemetry +payload5.length=78 diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_Type2_MINMAX.frame b/spacecraft/PacSatGround_0.46o/PacSatSim_Type2_MINMAX.frame new file mode 100644 index 00000000..a69be045 --- /dev/null +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_Type2_MINMAX.frame @@ -0,0 +1,13 @@ +number_of_payloads=6 +payload0.name=rttelemetry +payload0.length=78 +payload1.name=rttelemetry +payload1.length=78 +payload2.name=rttelemetry +payload2.length=78 +payload3.name=maxtelemetry +payload3.length=78 +payload4.name=mintelemetry +payload4.length=78 +payload5.name=wodtelemetry +payload5.length=78 diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_conversion_curves.csv b/spacecraft/PacSatGround_0.46o/PacSatSim_conversion_curves.csv new file mode 100644 index 00000000..30f05985 --- /dev/null +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_conversion_curves.csv @@ -0,0 +1,13 @@ +CurveName,a,bx,cx^2,dx^3,ex^4,fx^5,Description +cubesatsim_voltage,0,0.01,0,0,0,0,Converts voltages read from the INA219 sensors +cubesatsim_current,-2048,1,0,0,0,0,Converts positive and negative currents read from the INA219 sensors +cubesatsim_temperature,0,0.1,0,0,0,0,Converts temperature of Pi +cubesatsim_rotation,-2048,1,0,0,0,0,Converts positive and negative dps rotation +cubesatsim_acceleration,-20.48,0.01,0,0,0,0,Converts positive and negative g acceleration +cubesatsim_altitude,0,0.1,0,0,0,0,Converts altitude +cubesatsim_pressure,0,1,0,0,0,0,Converts pressure +cubesatsim_sensor1,0,1,0,0,0,0,Conversion of Sensor 1 +cubesatsim_sensor2,-2048,1,0,0,0,0,Conversion of Sensor 2 +cubesatsim_sensor3,-20.48,0.01,0,0,0,0,Conversion of Sensor 3 +cubesatsim_rpm,-204.8,0.1,0,0,0,0,Conversion of calculated RPM +cubesatsim_rssi,-2048,1,0,0,0,0,Conversion of Received Signal Strength diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_maxtelemetry.csv b/spacecraft/PacSatGround_0.46o/PacSatSim_maxtelemetry.csv new file mode 100644 index 00000000..9bf2f291 --- /dev/null +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_maxtelemetry.csv @@ -0,0 +1,62 @@ +61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,MAX,Sensor 2,12,integer,1,NONE,6,8,3,Sensor 2,STEM Payload Extra Sensor 2 +1,MAX,Sensor 3,12,integer,1,NONE,6,9,3,Sensor 3,STEM Payload Extra Sensor 3 +2,MAX,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,INA219 Battery Voltage +3,MAX,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis +4,MAX,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis +5,MAX,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis +6,MAX,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,INA219 Battery Current +7,MAX,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature +8,MAX,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X solar panel Voltage +9,MAX,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y solar panel Voltage +10,MAX,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z solar panel Voltage +11,MAX,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X solar panel Voltage +12,MAX,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y solar panel Voltage +13,MAX,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z solar panel Voltage +14,MAX,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X solar panel Current +15,MAX,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y solar panel Current +16,MAX,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z solar panel Current +17,MAX,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X solar panel Current +18,MAX,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y solar panel Current +19,MAX,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z solar panel Current +20,MAX,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery 2 Voltage,INA219 Battery 2 Voltage +21,MAX,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MAX,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure +23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude +24,MAX,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,MAX,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication +26,MAX,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi +27,MAX,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis +28,MAX,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis +29,MAX,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis +30,MAX,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,BME280 Humidity,BME280 Humidity +31,MAX,BAT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery 2 Current,INA219 Battery 2 Current +32,MAX,DiodeTemp,12,C,cubesatsim_rpm,NONE,6,6,3,Diode Temp,STEM Payload Diode Temperature +33,MAX,Sensor 1,12,integer,1,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1 +34,MAX,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator +35,MAX,SafeMode,1,-,STATUS_ON_OFF,NONE,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage) +36,MAX,SimulatedTelemetry,1,-,STATUS_ON_OFF,NONE,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator +37,MAX,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator +38,MAX,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,MAX,I2CBus1Failure,1,-,17,NONE,2,2,0,I2C Bus 1,I2C bus 1 failure indicator +40,MAX,I2CBus3Failure,1,-,17,NONE,2,3,0,I2C Bus 3,I2C bus 3 failure indicator +41,MAX,CameraFailure,1,-,17,NONE,2,4,0,Camera,Camera failure indicator +42,MAX,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received +43,MAX,RxAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status +44,MAX,TxAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status +45,MAX,C2CStatus,2,-,COMMAND_STATUS,NONE,3,5,0,Command Control, Command & Control Status +46,MAX,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +47,MAX,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +48,MAX,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +49,MAX,rf6,12,-,0,NONE,0,0,0,None,None +50,MAX,rf7,12,-,0,NONE,0,0,0,None,None +51,MAX,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +52,MAX,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +53,MAX,pad,4,-,34,NONE,0,0,0,None,Unused +54,MAX,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +55,MAX,pad1,1,-,0,NONE,0,0,0,NONE,Filler +56,MAX,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +57,MAX,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +58,MAX,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset +59,MAX,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset +60,MAX,pad2,27,-,0,NONE,0,0,0,NONE,Filler diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_mintelemetry.csv b/spacecraft/PacSatGround_0.46o/PacSatSim_mintelemetry.csv new file mode 100644 index 00000000..adf24a04 --- /dev/null +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_mintelemetry.csv @@ -0,0 +1,62 @@ +61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,MIN,Sensor 2,12,integer,1,NONE,6,8,3,Sensor 2,STEM Payload Extra Sensor 2 +1,MIN,Sensor 3,12,integer,1,NONE,6,9,3,Sensor 3,STEM Payload Extra Sensor 3 +2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,INA219 Battery Voltage +3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis +4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis +5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis +6,MIN,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,INA219 Battery Current +7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature +8,MIN,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X solar panel Voltage +9,MIN,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y solar panel Voltage +10,MIN,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z solar panel Voltage +11,MIN,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X solar panel Voltage +12,MIN,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y solar panel Voltage +13,MIN,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z solar panel Voltage +14,MIN,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X solar panel Current +15,MIN,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y solar panel Current +16,MIN,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z solar panel Current +17,MIN,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X solar panel Current +18,MIN,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y solar panel Current +19,MIN,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z solar panel Current +20,MIN,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery 2 Voltage,INA219 Battery 2 Voltage +21,MIN,spin,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,MIN,Pressure,12,hPa,cubesatsim_pressure,NONE,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure +23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude +24,MIN,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,MIN,rssi,12,dBm,cubesatsim_rssi|INT,NONE,1,1,3,RSSI,Received Signal Strength Indication +26,MIN,IHUcpuTemp,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi +27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis +28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis +29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis +30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,BME280 Humidity,BME280 Humidity +31,MIN,BAT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery 2 Current,INA219 Battery 2 Current +32,MIN,DiodeTemp,12,C,cubesatsim_rpm,NONE,6,6,3,Diode Temp,STEM Payload Diode Temperature +33,MIN,Sensor 1,12,integer,1,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1 +34,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator +35,MIN,SafeMode,1,-,STATUS_ON_OFF,NONE,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage) +36,MIN,SimulatedTelemetry,1,-,STATUS_ON_OFF,NONE,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator +37,MIN,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator +38,MIN,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,MIN,I2CBus1Failure,1,-,17,NONE,2,2,0,I2C Bus 1,I2C bus 1 failure indicator +40,MIN,I2CBus3Failure,1,-,17,NONE,2,3,0,I2C Bus 3,I2C bus 3 failure indicator +41,MIN,CameraFailure,1,-,17,NONE,2,4,0,Camera,Camera failure indicator +42,MIN,GroundCommands,4,-,1,NONE,3,3,0,Ground Commands,Number of ground commands received +43,MIN,RxAntenna,1,-,16,NONE,1,3,0,RX Antenna,Receive antenna status +44,MIN,TxAntenna,1,-,16,NONE,1,2,0,TX Antenna,Transmit antenna status +45,MIN,C2CStatus,2,-,COMMAND_STATUS,NONE,3,5,0,Command Control, Command & Control Status +46,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +47,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +48,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +49,MIN,rf6,12,-,0,NONE,0,0,0,None,None +50,MIN,rf7,12,-,0,NONE,0,0,0,None,None +51,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +52,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +53,MIN,pad,4,-,34,NONE,0,0,0,None,Unused +54,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +55,MIN,pad1,1,-,0,NONE,0,0,0,NONE,Filler +56,MIN,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +57,MIN,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +58,MIN,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset +59,MIN,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset +60,MIN,pad2,27,-,0,NONE,0,0,0,NONE,Filler diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv b/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv new file mode 100644 index 00000000..f9301dbe --- /dev/null +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv @@ -0,0 +1,62 @@ +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 +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 +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 +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 +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 +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 +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 +35,realTime,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage) +36,realTime,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator +37,realTime,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator +38,realTime,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,realTime,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator +40,realTime,I2CBus3Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 3,I2C bus 3 failure indicator +41,realTime,CameraFailure,1,-,17,Computer Hardware,2,4,0,Camera,Camera failure indicator +42,realTime,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received +43,realTime,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,realTime,TxAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +45,realTime,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status +46,realTime,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +47,realTime,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +48,realTime,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +49,realTime,rf6,12,-,0,NONE,0,0,0,None,None +50,realTime,rf7,12,-,0,NONE,0,0,0,None,None +51,realTime,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +52,realTime,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +53,realTime,pad,4,-,34,NONE,0,0,0,None,Unused +54,realTime,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance +55,realTime,pad1,1,-,0,NONE,0,0,0,NONE,Filler +56,realTime,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +57,realTime,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +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 diff --git a/spacecraft/PacSatGround_0.46o/PacSatSim_wodtelemetry.csv b/spacecraft/PacSatGround_0.46o/PacSatSim_wodtelemetry.csv new file mode 100644 index 00000000..d1b53340 --- /dev/null +++ b/spacecraft/PacSatGround_0.46o/PacSatSim_wodtelemetry.csv @@ -0,0 +1,62 @@ +61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale) +1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale) +2,WOD,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale) +3,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis +4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis +5,WOD,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis +6,WOD,battCurr,12,mA,cubesatsim_current,Battery,4,2,4,Current,Total Battery DC current +7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature +8,WOD,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage +9,WOD,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage +10,WOD,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage +11,WOD,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage +12,WOD,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage +13,WOD,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage +14,WOD,posXi,12,mA,cubesatsim_current,+X Panel,7,2,4,Current,+X solar Panel current +15,WOD,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,4,Current,+Y solar Panel current +16,WOD,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,4,Current,+Z solar Panel current +17,WOD,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar Panel current +18,WOD,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar Panel current +19,WOD,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,Current,-Z solar Panel current +20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage +21,WOD,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,WOD,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure +23,WOD,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude +24,WOD,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,WOD,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication +26,WOD,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU +27,WOD,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis +28,WOD,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis +29,WOD,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis +30,WOD,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1 +31,WOD,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current +32,WOD,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2 +33,WOD,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3 +34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator +35,WOD,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode) +36,WOD,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator +37,WOD,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator +38,WOD,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,WOD,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator +40,WOD,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator +41,WOD,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator +42,WOD,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received +43,WOD,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,WOD,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +45,WOD,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted +46,WOD,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V +47,WOD,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected +48,WOD,rf6,12,-,0,NONE,0,0,0,None,None +49,WOD,rf7,12,-,0,NONE,0,0,0,None,None +50,WOD,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR +51,WOD,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA) +52,WOD,pad,4,-,34,NONE,0,0,0,None,Unused +53,WOD,WODTimeStampReset,16,-,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected +54,WOD,pad1,17,-,0,NONE,0,0,0,NONE,Filler +55,WOD,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds +56,WOD,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information +57,WOD,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset +58,WOD,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset +59,WOD,WODTimeStampUpTime,25,s,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected +60,WOD,pad2,3,-,0,NONE,0,0,0,NONE,Filler