From 3763facea2d7e51b74527cc2af1e91467920bd81 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Tue, 28 Oct 2025 22:45:52 -0400 Subject: [PATCH 01/28] Create README.md --- spacecraft/FoxTelem_1.13i/README.md | 1 + 1 file changed, 1 insertion(+) create mode 100644 spacecraft/FoxTelem_1.13i/README.md diff --git a/spacecraft/FoxTelem_1.13i/README.md b/spacecraft/FoxTelem_1.13i/README.md new file mode 100644 index 00000000..8220b309 --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/README.md @@ -0,0 +1 @@ +These files update FoxTelem version 1.13i and fix a bug in the payload altitude sensor display. From 23c3979948854cedd775163918acae75a5077e3a Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Tue, 28 Oct 2025 20:49:07 -0600 Subject: [PATCH 02/28] Add files via upload --- .../CubeSatSim_PSK_maxtelemetry.csv | 62 +++++++++++++++++++ .../CubeSatSim_PSK_mintelemetry.csv | 62 +++++++++++++++++++ .../CubeSatSim_PSK_rttelemetry.csv | 62 +++++++++++++++++++ .../CubeSatSim_maxtelemetry.csv | 48 ++++++++++++++ .../CubeSatSim_mintelemetry.csv | 48 ++++++++++++++ .../FoxTelem_1.13i/CubeSatSim_rttelemetry.csv | 48 ++++++++++++++ 6 files changed, 330 insertions(+) create mode 100644 spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv create mode 100644 spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv create mode 100644 spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv create mode 100644 spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv create mode 100644 spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv create mode 100644 spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv new file mode 100644 index 00000000..9bf2f291 --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_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/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv new file mode 100644 index 00000000..adf24a04 --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_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/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv new file mode 100644 index 00000000..f9301dbe --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_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/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv new file mode 100644 index 00000000..06d42d9e --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv @@ -0,0 +1,48 @@ +47,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,STEM Payload Sensor BME280 Temperature +8,MAX,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X Panel Voltage +9,MAX,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X Panel Voltage +10,MAX,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y Panel Voltage +11,MAX,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y Panel Voltage +12,MAX,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z Panel Voltage +13,MAX,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z Panel Voltage +14,MAX,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X Panel Current +15,MAX,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X Panel Current +16,MAX,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y Panel Current +17,MAX,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y Panel Current +18,MAX,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z Panel Current +19,MAX,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z 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,STEM Payload Sensor BME280 Pressure +23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 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,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU +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,STEM Payload Sensor BME280 Humidity +31,MAX,BATT2_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 Board Status +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,0,0,0,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,Pad,56,-,0,NONE,0,0,0,NONE,NONE diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv new file mode 100644 index 00000000..f3514e7b --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv @@ -0,0 +1,48 @@ +47,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,STEM Payload Sensor BME280 Temperature +8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,INA219 +X Panel Voltage +9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,INA219 -X Panel Voltage +10,MIN,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,INA219 +Y Panel Voltage +11,MIN,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,INA219 -Y Panel Voltage +12,MIN,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,INA219 +Z Panel Voltage +13,MIN,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,INA219 -Z Panel Voltage +14,MIN,PANEL_PLUS_X_I,12,mA,cubesatsim_current,NONE,7,2,3,Current,INA219 +X Panel Current +15,MIN,PANEL_MINUS_X_I,12,mA,cubesatsim_current,NONE,10,2,3,Current,INA219 -X Panel Current +16,MIN,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,NONE,8,2,3,Current,INA219 +Y Panel Current +17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,INA219 -Y Panel Current +18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,INA219 +Z Panel Current +19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,INA219 -Z 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,STEM Payload Sensor BME280 Pressure +23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 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,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU +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,STEM Payload Sensor BME280 Humidity +31,MIN,BATT2_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 Board Status +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,0,0,0,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,Pad,56,-,0,NONE,0,0,0,NONE,NONE diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv new file mode 100644 index 00000000..9dc17ff6 --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv @@ -0,0 +1,48 @@ +47,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION +0,RT,Sensor 2,12,integer,1,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2 +1,RT,Sensor 3,12,integer,1,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3 +2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage +3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis +4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis +5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis +6,RT,BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Battery Current,INA219 Battery Current +7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,STEM Payload Sensor BME280 Temperature +8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X Panel Voltage +9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,INA219 -X Panel Voltage +10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,INA219 +Y Panel Voltage +11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,INA219 -Y Panel Voltage +12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,INA219 +Z Panel Voltage +13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,INA219 -Z Panel Voltage +14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,INA219 +X Panel Current +15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,INA219 -X Panel Current +16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,INA219 +Y Panel Current +17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y Panel Current +18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,INA219 +Z Panel Current +19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z Panel Current +20,RT,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage +21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells +22,RT,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,STEM Payload Sensor BME280 Pressure +23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude +24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count +25,RT,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication +26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU +27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around X Axis +28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Y Axis +29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Z Axis +30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,STEM Payload Sensor BME280 Humidity +31,RT,BATT2_I,12,mA,cubesatsim_current,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current +32,RT,DiodeTemp,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature +33,RT,Sensor 1,12,integer,1,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1 +34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status +35,RT,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage) +36,RT,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry, Simulated Telemetry Indicator +37,RT,PayloadStatus1,1,-,17,NONE,0,0,0,Exp 3,STEM Payload status 1 failure indicator +38,RT,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator +39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator +40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 3,I2C bus 3 failure indicator +41,RT,CameraFailure,1,-,17,Computer Hardware,2,4,0,Camera,Camera failure indicator +42,RT,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received +43,RT,RXAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status +44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status +45,RT,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status +46,RT,Pad,56,-,0,NONE,0,0,0,NONE,NONE From f7c35e0ab1ddf3b866bc7493c424d522b93a33f8 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Tue, 28 Oct 2025 20:53:02 -0600 Subject: [PATCH 03/28] Add files via upload --- .../FoxTelem_1.13i/CubeSatSim_conversion_curves.csv | 13 +++++++++++++ 1 file changed, 13 insertions(+) create mode 100644 spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv new file mode 100644 index 00000000..30f05985 --- /dev/null +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_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 From d5aae747d8b7fde6399497bf0417a65261cd492d Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Tue, 28 Oct 2025 22:54:15 -0400 Subject: [PATCH 04/28] Update CubeSatSim_conversion_curves.csv --- spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv index 30f05985..c06f06ef 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv @@ -4,10 +4,11 @@ cubesatsim_current,-2048,1,0,0,0,0,Converts positive and negative currents read 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_altitude,0,100,0,0,0,0,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 + From d1f39bf14703e1fb1c7ea81f2be1537c95e3d560 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Tue, 28 Oct 2025 23:14:17 -0400 Subject: [PATCH 05/28] Update CubeSatSim_PSK_rttelemetry.csv --- spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv index f9301dbe..cf0a4536 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv @@ -22,7 +22,7 @@ 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 +23,realTime,Altitude,12,m,cubesatsim_altitude|INT,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 @@ -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 + From 207b9259629e0cb095b9ba4fa62bbd98249fe40a Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Tue, 28 Oct 2025 23:22:18 -0400 Subject: [PATCH 06/28] Update main.c alt/10 --- main.c | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/main.c b/main.c index ff1d3654..fdfa7384 100644 --- a/main.c +++ b/main.c @@ -1473,7 +1473,7 @@ void get_tlm_fox() { encodeB(b_max, 7 + head_offset, (int)(sensor_max[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel encodeA(b_max, 33 + head_offset, (int)(sensor_max[PRES] + 0.5)); // Pressure - encodeB(b_max, 34 + head_offset, (int)(sensor_max[ALT] * 10.0 + 0.5)); // Altitude + encodeB(b_max, 34 + head_offset, (int)(sensor_max[ALT] / 10.0 + 0.5)); // Altitude encodeB(b_max, 40 + head_offset, (int)(sensor_max[GYRO_X] + 0.5) + 2048); encodeA(b_max, 42 + head_offset, (int)(sensor_max[GYRO_Y] + 0.5) + 2048); encodeB(b_max, 43 + head_offset, (int)(sensor_max[GYRO_Z] + 0.5) + 2048); @@ -1530,7 +1530,7 @@ void get_tlm_fox() { encodeB(b_min, 7 + head_offset, (int)(sensor_min[ACCEL_Z] * 100 + 0.5) + 2048); // Zaccel encodeA(b_min, 33 + head_offset, (int)(sensor_min[PRES] + 0.5)); // Pressure - encodeB(b_min, 34 + head_offset, (int)(sensor_min[ALT] * 10.0 + 0.5)); // Altitude + encodeB(b_min, 34 + head_offset, (int)(sensor_min[ALT] / 10.0 + 0.5)); // Altitude encodeB(b_min, 40 + head_offset, (int)(sensor_min[GYRO_X] + 0.5) + 2048); encodeA(b_min, 42 + head_offset, (int)(sensor_min[GYRO_Y] + 0.5) + 2048); encodeB(b_min, 43 + head_offset, (int)(sensor_min[GYRO_Z] + 0.5) + 2048); @@ -1563,7 +1563,7 @@ void get_tlm_fox() { encodeB(b, 31 + head_offset, ((int)(other[SPIN] * 10)) + 2048); encodeA(b, 33 + head_offset, (int)(sensor[PRES] + 0.5)); // Pressure - encodeB(b, 34 + head_offset, (int)(sensor[ALT] * 10.0 + 0.5)); // Altitude + encodeB(b, 34 + head_offset, (int)(sensor[ALT] / 10.0 + 0.5)); // Altitude encodeA(b, 36 + head_offset, Resets); encodeB(b, 37 + head_offset, (int)(other[RSSI] + 0.5) + 2048); From 5706e44e86bcc6f428e7e587e2315119b25d9a22 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Tue, 28 Oct 2025 23:22:51 -0400 Subject: [PATCH 07/28] Update CubeSatSim_conversion_curves.csv alt*10 --- spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv index c06f06ef..5420b14d 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv @@ -4,7 +4,7 @@ cubesatsim_current,-2048,1,0,0,0,0,Converts positive and negative currents read 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,0,100,0,0,0,0,Converts altitude +cubesatsim_altitude,0,10,0,0,0,0,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 @@ -12,3 +12,4 @@ 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 + From 163278f42df4197ba040e1e8b6a7fb7c09741de3 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:07:47 -0400 Subject: [PATCH 08/28] Update CubeSatSim_rttelemetry.csv alt int --- spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv index 9dc17ff6..7ef69cfc 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv @@ -22,7 +22,7 @@ 20,RT,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage 21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells 22,RT,Pressure,12,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,STEM Payload Sensor BME280 Pressure -23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude +23,RT,Altitude,12,m,cubesatsim_altitude|INT,Experiments,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude 24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count 25,RT,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU @@ -46,3 +46,4 @@ 44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status 45,RT,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status 46,RT,Pad,56,-,0,NONE,0,0,0,NONE,NONE + From ab0b504ea8d35d692948bef100fc9fe554617e6f Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:08:10 -0400 Subject: [PATCH 09/28] Update CubeSatSim_mintelemetry.csv alt int --- spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv index f3514e7b..ade27f0b 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv @@ -22,7 +22,7 @@ 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,STEM Payload Sensor BME280 Pressure -23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude +23,MIN,Altitude,12,m,cubesatsim_altitude|INT,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 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,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU @@ -46,3 +46,4 @@ 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,Pad,56,-,0,NONE,0,0,0,NONE,NONE + From e17cbeb6dfbc881439bc2f9769d4d090d2ab3cf6 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:08:26 -0400 Subject: [PATCH 10/28] Update CubeSatSim_maxtelemetry.csv alt int --- spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv index 06d42d9e..164dc808 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv @@ -22,7 +22,7 @@ 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,STEM Payload Sensor BME280 Pressure -23,MAX,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude +23,MAX,Altitude,12,m,cubesatsim_altitude|INT,NONE,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 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,IHUTemperature,12,C,cubesatsim_temperature,NONE,2,1,3,IHU Temp (Pi),Internal Temperature of Pi IHU @@ -46,3 +46,4 @@ 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,Pad,56,-,0,NONE,0,0,0,NONE,NONE + From d29b5c8240362c96b4c5863d956e6b7a20150369 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:08:44 -0400 Subject: [PATCH 11/28] Update CubeSatSim_PSK_mintelemetry.csv alt int --- spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv index adf24a04..8acc3c69 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv @@ -22,7 +22,7 @@ 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 +23,MIN,Altitude,12,m,cubesatsim_altitude|INT,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 @@ -60,3 +60,4 @@ 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 + From 712525079eab261c2d4c47a37816514304b20479 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:08:53 -0400 Subject: [PATCH 12/28] Update CubeSatSim_PSK_maxtelemetry.csv alt int --- spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv | 3 ++- 1 file changed, 2 insertions(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv index 9bf2f291..52f6b913 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv @@ -22,7 +22,7 @@ 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 +23,MAX,Altitude,12,m,cubesatsim_altitude|INT,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 @@ -60,3 +60,4 @@ 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 + From 554d5d2058648e3d52cbf3ad5ca862eb26928cdd Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:33:26 -0400 Subject: [PATCH 13/28] Update README.md --- spacecraft/FoxTelem_1.13i/README.md | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/README.md b/spacecraft/FoxTelem_1.13i/README.md index 8220b309..6f1cd1df 100644 --- a/spacecraft/FoxTelem_1.13i/README.md +++ b/spacecraft/FoxTelem_1.13i/README.md @@ -1 +1 @@ -These files update FoxTelem version 1.13i and fix a bug in the payload altitude sensor display. +These files update the spacecraft files in FoxTelem version 1.13i or later and fix a bug in the payload altitude sensor display. From 138f30646cfb905236628aaf7e31804f974ce0ce Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:38:25 -0400 Subject: [PATCH 14/28] Update CubeSatSim_PSK_rttelemetry.csv remove blank rows --- spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv | 1 - 1 file changed, 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv index cf0a4536..2d34abc9 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv @@ -60,4 +60,3 @@ 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 - From fba8d69ff8b347ca81242770bda1af208dabda1b Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:39:48 -0400 Subject: [PATCH 15/28] Update CubeSatSim_mintelemetry.csv remove blank lines --- spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv | 1 - 1 file changed, 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv index ade27f0b..5d6627a9 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_mintelemetry.csv @@ -46,4 +46,3 @@ 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,Pad,56,-,0,NONE,0,0,0,NONE,NONE - From 608acc99d18d0e512a35f40b20da4056bf693f4c Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:40:09 -0400 Subject: [PATCH 16/28] Update CubeSatSim_maxtelemetry.csv remove blank lines --- spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv | 1 - 1 file changed, 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv index 164dc808..9bcc637e 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv @@ -46,4 +46,3 @@ 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,Pad,56,-,0,NONE,0,0,0,NONE,NONE - From e2d9dc976d434a8c20429d52ca8c4ded9372056c Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:40:27 -0400 Subject: [PATCH 17/28] Update CubeSatSim_PSK_mintelemetry.csv remove blank lines --- spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv | 1 - 1 file changed, 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv index 8acc3c69..7d69fce6 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv @@ -60,4 +60,3 @@ 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 - From db3c24561c874185bc4747c3b0e2c53ab660d26e Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:41:07 -0400 Subject: [PATCH 18/28] Update CubeSatSim_PSK_maxtelemetry.csv remove blank lines --- spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv | 1 - 1 file changed, 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv index 52f6b913..124a7a65 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv @@ -60,4 +60,3 @@ 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 - From d659d616fec49711bd58b22cb5d1315a476c06e7 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:41:52 -0400 Subject: [PATCH 19/28] Update CubeSatSim_rttelemetry.csv remove blank lines --- spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv | 1 - 1 file changed, 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv index 7ef69cfc..556e73d3 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv @@ -46,4 +46,3 @@ 44,RT,TXAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status 45,RT,C2CStatus,2,-,COMMAND_STATUS,Computer Software,3,5,0,Command Control, Command & Control Status 46,RT,Pad,56,-,0,NONE,0,0,0,NONE,NONE - From 1513228581958b254046521cf5cd3551579226e6 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:43:56 -0400 Subject: [PATCH 20/28] Update CubeSatSim_conversion_curves.csv remove blank lines --- spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv | 2 -- 1 file changed, 2 deletions(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv index 5420b14d..38f4351b 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv @@ -11,5 +11,3 @@ 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 - - From 37dc3abec95dbb781837c908a1594cae34771d63 Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 10:47:09 -0400 Subject: [PATCH 21/28] Update README.md --- spacecraft/FoxTelem_1.13i/README.md | 6 ++++++ 1 file changed, 6 insertions(+) diff --git a/spacecraft/FoxTelem_1.13i/README.md b/spacecraft/FoxTelem_1.13i/README.md index 6f1cd1df..9366c13b 100644 --- a/spacecraft/FoxTelem_1.13i/README.md +++ b/spacecraft/FoxTelem_1.13i/README.md @@ -1 +1,7 @@ These files update the spacecraft files in FoxTelem version 1.13i or later and fix a bug in the payload altitude sensor display. + +You can download them as a zip file [foxtelem_spacecraft_files.zip](https://github.com/user-attachments/files/23213090/foxtelem_spacecraft_files.zip) + +Extract (unzip foxtelem_spacecraft_files) and copy into FoxTelem spacecraft folder, replacing existing files. + +Next time you run FoxTelem, the CubeSatSim-FSK and CubeSatSim-BPSK spacecraft will be automatically updated. From 06bc063b5c04c3ae2f1ad9b925b17fa33045cbfd Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 14:52:52 -0400 Subject: [PATCH 27/28] Update CubeSatSim_PSK_maxtelemetry.csv remove blank lines at end --- spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv index 124a7a65..f99efb04 100644 --- a/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv +++ b/spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv @@ -59,4 +59,4 @@ 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 +60,MAX,pad2,27,-,0,NONE,0,0,0,NONE,Filler byets From c6e835cf4c2665ba496787ef1d64b22b0fa7267b Mon Sep 17 00:00:00 2001 From: Alan Johnston Date: Wed, 29 Oct 2025 15:04:39 -0400 Subject: [PATCH 28/28] Update README.md fix zip file --- spacecraft/FoxTelem_1.13i/README.md | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/spacecraft/FoxTelem_1.13i/README.md b/spacecraft/FoxTelem_1.13i/README.md index 9366c13b..d085dedc 100644 --- a/spacecraft/FoxTelem_1.13i/README.md +++ b/spacecraft/FoxTelem_1.13i/README.md @@ -1,6 +1,6 @@ These files update the spacecraft files in FoxTelem version 1.13i or later and fix a bug in the payload altitude sensor display. -You can download them as a zip file [foxtelem_spacecraft_files.zip](https://github.com/user-attachments/files/23213090/foxtelem_spacecraft_files.zip) +You can download them as a zip file: [foxtelem_spacecraft_files.zip](https://github.com/user-attachments/files/23217474/foxtelem_spacecraft_files.zip) Extract (unzip foxtelem_spacecraft_files) and copy into FoxTelem spacecraft folder, replacing existing files.