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Merge pull request #399 from alanbjohnston/master-alt-bug to fix altitude bug

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Master alt bug
pi4
Alan Johnston 2 months ago committed by GitHub
parent be0cf14131 c6e835cf4c
commit d3e40c4d1b
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GPG Key ID: B5690EEEBB952194
9 changed files with 353 additions and 3 deletions
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6
main.c
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@ -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);

62
spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_maxtelemetry.csv
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@ -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|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
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 byets
1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MAX Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MAX Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MAX BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MAX SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MAX SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MAX SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MAX BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MAX Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 MAX posXv 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 MAX posYv 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y solar panel Voltage
12 10 MAX posZv 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z solar panel Voltage
13 11 MAX negXv 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X solar panel Voltage
14 12 MAX negYv 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y solar panel Voltage
15 13 MAX negZv 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z solar panel Voltage
16 14 MAX posXi 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X solar panel Current
17 15 MAX posYi 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y solar panel Current
18 16 MAX posZi 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z solar panel Current
19 17 MAX negXi 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X solar panel Current
20 18 MAX negYi 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y solar panel Current
21 19 MAX negZi 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z solar panel Current
22 20 MAX BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MAX spin 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MAX Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 MAX Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
26 24 MAX Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MAX rssi 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MAX IHUcpuTemp 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal temperature of IHU from Pi
29 27 MAX SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 MAX Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity BME280 Humidity
33 31 MAX BAT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MAX DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MAX Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MAX STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
37 35 MAX SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MAX SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MAX PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MAX I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MAX I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MAX I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MAX CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MAX GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MAX RxAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MAX TxAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MAX C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MAX ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
49 47 MAX ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
50 48 MAX ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
51 49 MAX rf6 12 - 0 NONE 0 0 0 None None
52 50 MAX rf7 12 - 0 NONE 0 0 0 None None
53 51 MAX MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
54 52 MAX LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
55 53 MAX pad 4 - 34 NONE 0 0 0 None Unused
56 54 MAX IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
57 55 MAX pad1 1 - 0 NONE 0 0 0 NONE Filler
58 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
59 57 MAX swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
60 58 MAX hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
61 59 MAX swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
62 60 MAX pad2 27 - 0 NONE 0 0 0 NONE Filler byets

62
spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_mintelemetry.csv
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@ -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|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
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
1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MIN Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MIN Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MIN BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MIN BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 MIN posXv 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 MIN posYv 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y solar panel Voltage
12 10 MIN posZv 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z solar panel Voltage
13 11 MIN negXv 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X solar panel Voltage
14 12 MIN negYv 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y solar panel Voltage
15 13 MIN negZv 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z solar panel Voltage
16 14 MIN posXi 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X solar panel Current
17 15 MIN posYi 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y solar panel Current
18 16 MIN posZi 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z solar panel Current
19 17 MIN negXi 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X solar panel Current
20 18 MIN negYi 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y solar panel Current
21 19 MIN negZi 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z solar panel Current
22 20 MIN BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MIN spin 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MIN Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 MIN Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
26 24 MIN Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MIN rssi 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MIN IHUcpuTemp 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal temperature of IHU from Pi
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity BME280 Humidity
33 31 MIN BAT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MIN DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MIN Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
37 35 MIN SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MIN SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MIN PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MIN I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MIN I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MIN I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MIN CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MIN GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MIN RxAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MIN TxAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MIN C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MIN ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
49 47 MIN ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
50 48 MIN ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
51 49 MIN rf6 12 - 0 NONE 0 0 0 None None
52 50 MIN rf7 12 - 0 NONE 0 0 0 None None
53 51 MIN MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
54 52 MIN LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
55 53 MIN pad 4 - 34 NONE 0 0 0 None Unused
56 54 MIN IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
57 55 MIN pad1 1 - 0 NONE 0 0 0 NONE Filler
58 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
59 57 MIN swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
60 58 MIN hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
61 59 MIN swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
62 60 MIN pad2 27 - 0 NONE 0 0 0 NONE Filler

62
spacecraft/FoxTelem_1.13i/CubeSatSim_PSK_rttelemetry.csv
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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|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
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
1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 realTime Sensor 2 12 integer 1 Experiments 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 realTime Sensor 3 12 integer 1 Experiments 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 realTime BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 realTime SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 realTime SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 realTime SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 realTime BATT_I 12 mA cubesatsim_current Battery 4 2 3 Battery Current INA219 Battery Current
9 7 realTime Temperature 12 C cubesatsim_temperature Experiments 6 2 3 BME280 Temp BME280 STEM Payload sensor temperature
10 8 realTime posXv 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage INA219 +X solar panel Voltage
11 9 realTime posYv 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage INA219 +Y solar panel Voltage
12 10 realTime posZv 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage INA219 +Z solar panel Voltage
13 11 realTime negXv 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage INA219 -X solar panel Voltage
14 12 realTime negYv 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage INA219 -Y solar panel Voltage
15 13 realTime negZv 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage INA219 -Z solar panel Voltage
16 14 realTime posXi 12 mA cubesatsim_current +X Panel 7 2 3 Current INA219 +X solar panel Current
17 15 realTime posYi 12 mA cubesatsim_current +Y Panel 8 2 3 Current INA219 +Y solar panel Current
18 16 realTime posZi 12 mA cubesatsim_current +Z Panel 9 2 3 Current INA219 +Z solar panel Current
19 17 realTime negXi 12 mA cubesatsim_current -X Panel 10 2 3 Current INA219 -X solar panel Current
20 18 realTime negYi 12 mA cubesatsim_current -Y Panel 11 2 3 Current INA219 -Y solar panel Current
21 19 realTime negZi 12 mA cubesatsim_current -Z Panel 12 2 3 Current INA219 -Z solar panel Current
22 20 realTime BATT2_V 12 V cubesatsim_voltage|FLOAT2 Battery2 5 1 3 Battery2 Voltage INA219 Battery2 Voltage
23 21 realTime spin 12 rpm cubesatsim_rpm Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 realTime Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 BME280 Pressure BME280 STEM Payload sensor pressure
25 23 realTime Altitude 12 m cubesatsim_altitude|INT Experiments 6 4 3 BME280 Altitude BME280 STEM Payload sensor altitude
26 24 realTime Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 realTime rssi 12 dBm cubesatsim_rssi|INT Radio 1 1 3 RSSI Received Signal Strength Indication
28 26 realTime IHUcpuTemp 12 C cubesatsim_temperature Computer Hardware 2 1 3 IHU Temp (Pi) Internal temperature of IHU from Pi
29 27 realTime SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around X Axis
30 28 realTime SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 realTime SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 realTime Humidity 12 % cubesatsim_temperature Experiments 6 5 3 BME280 Humidity BME280 Humidity
33 31 realTime BAT2_I 12 mA cubesatsim_current Battery2 5 2 3 Battery2 Current INA219 Battery2 Current
34 32 realTime DiodeTemp 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 realTime Sensor 1 12 integer 1 Experiments 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 realTime STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload board failure Indicator
37 35 realTime SafeMode 1 - STATUS_ON_OFF Computer Software 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 realTime SimulatedTelemetry 1 - STATUS_ON_OFF Computer Software 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 realTime PayloadStatus1 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 1 failure indicator
40 38 realTime I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 realTime I2CBus1Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 realTime I2CBus3Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 realTime CameraFailure 1 - 17 Computer Hardware 2 4 0 Camera Camera failure indicator
44 42 realTime GroundCommands 4 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
45 43 realTime RxAntenna 1 - 16 Radio 1 3 0 RX Antenna Receive antenna status
46 44 realTime TxAntenna 1 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 realTime C2CStatus 2 - COMMAND_STATUS Computer Software 3 5 0 Command Control Command & Control Status
48 46 realTime ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
49 47 realTime ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
50 48 realTime ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
51 49 realTime rf6 12 - 0 NONE 0 0 0 None None
52 50 realTime rf7 12 - 0 NONE 0 0 0 None None
53 51 realTime MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
54 52 realTime LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
55 53 realTime pad 4 - 34 NONE 0 0 0 None Unused
56 54 realTime IHUdiagData 32 - 18 NONE 3 2 0 Diagnostic Info Diagnostic Data on IHU Performance
57 55 realTime pad1 1 - 0 NONE 0 0 0 NONE Filler
58 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
59 57 realTime swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
60 58 realTime hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
61 59 realTime swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
62 60 realTime pad2 27 - 0 NONE 0 0 0 NONE Filler

13
spacecraft/FoxTelem_1.13i/CubeSatSim_conversion_curves.csv
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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,0,10,0,0,0,0,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
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
1 CurveName a bx cx^2 dx^3 ex^4 fx^5 Description
2 cubesatsim_voltage 0 0.01 0 0 0 0 Converts voltages read from the INA219 sensors
3 cubesatsim_current -2048 1 0 0 0 0 Converts positive and negative currents read from the INA219 sensors
4 cubesatsim_temperature 0 0.1 0 0 0 0 Converts temperature of Pi
5 cubesatsim_rotation -2048 1 0 0 0 0 Converts positive and negative dps rotation
6 cubesatsim_acceleration -20.48 0.01 0 0 0 0 Converts positive and negative g acceleration
7 cubesatsim_altitude 0 10 0 0 0 0 Converts altitude
8 cubesatsim_pressure 0 1 0 0 0 0 Converts pressure
9 cubesatsim_sensor1 0 1 0 0 0 0 Conversion of Sensor 1
10 cubesatsim_sensor2 -2048 1 0 0 0 0 Conversion of Sensor 2
11 cubesatsim_sensor3 -20.48 0.01 0 0 0 0 Conversion of Sensor 3
12 cubesatsim_rpm -204.8 0.1 0 0 0 0 Conversion of calculated RPM
13 cubesatsim_rssi -2048 1 0 0 0 0 Conversion of Received Signal Strength

48
spacecraft/FoxTelem_1.13i/CubeSatSim_maxtelemetry.csv
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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|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
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
1 47 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MAX Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MAX Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MAX BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MAX SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MAX SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MAX SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MAX BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MAX Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp STEM Payload Sensor BME280 Temperature
10 8 MAX PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X Panel Voltage
11 9 MAX PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X Panel Voltage
12 10 MAX PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y Panel Voltage
13 11 MAX PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y Panel Voltage
14 12 MAX PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z Panel Voltage
15 13 MAX PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z Panel Voltage
16 14 MAX PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X Panel Current
17 15 MAX PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X Panel Current
18 16 MAX PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y Panel Current
19 17 MAX PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y Panel Current
20 18 MAX PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z Panel Current
21 19 MAX PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z Panel Current
22 20 MAX BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MAX SPIN 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MAX Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure STEM Payload Sensor BME280 Pressure
25 23 MAX Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude STEM Payload Sensor BME280 Altitude
26 24 MAX Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MAX RSSI 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MAX IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal Temperature of Pi IHU
29 27 MAX SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 MAX SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 MAX SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 MAX Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity STEM Payload Sensor BME280 Humidity
33 31 MAX BATT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MAX DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MAX Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MAX STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MAX SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MAX SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MAX PayloadStatus1 1 - 17 NONE 0 0 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MAX I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MAX I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MAX I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MAX CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MAX GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MAX RXAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MAX TXAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MAX C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MAX Pad 56 - 0 NONE 0 0 0 NONE NONE

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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|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
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
1 47 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MIN Sensor 2 12 integer 1 NONE 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 MIN Sensor 3 12 integer 1 NONE 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 MIN BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MIN BATT_I 12 mA cubesatsim_current NONE 4 2 3 Battery Current INA219 Battery Current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 BME280 Temp STEM Payload Sensor BME280 Temperature
10 8 MIN PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage INA219 +X Panel Voltage
11 9 MIN PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage INA219 -X Panel Voltage
12 10 MIN PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage INA219 +Y Panel Voltage
13 11 MIN PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage INA219 -Y Panel Voltage
14 12 MIN PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage INA219 +Z Panel Voltage
15 13 MIN PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage INA219 -Z Panel Voltage
16 14 MIN PANEL_PLUS_X_I 12 mA cubesatsim_current NONE 7 2 3 Current INA219 +X Panel Current
17 15 MIN PANEL_MINUS_X_I 12 mA cubesatsim_current NONE 10 2 3 Current INA219 -X Panel Current
18 16 MIN PANEL_PLUS_Y_I 12 mA cubesatsim_current NONE 8 2 3 Current INA219 +Y Panel Current
19 17 MIN PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current INA219 -Y Panel Current
20 18 MIN PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current INA219 +Z Panel Current
21 19 MIN PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current INA219 -Z Panel Current
22 20 MIN BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery 2 Voltage INA219 Battery 2 Voltage
23 21 MIN SPIN 12 rpm cubesatsim_rpm NONE 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 MIN Pressure 12 hPa cubesatsim_pressure NONE 6 3 3 BME280 Pressure STEM Payload Sensor BME280 Pressure
25 23 MIN Altitude 12 m cubesatsim_altitude|INT NONE 6 4 3 BME280 Altitude STEM Payload Sensor BME280 Altitude
26 24 MIN Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 MIN RSSI 12 dBm cubesatsim_rssi|INT NONE 1 1 3 RSSI Received Signal Strength Indication
28 26 MIN IHUTemperature 12 C cubesatsim_temperature NONE 2 1 3 IHU Temp (Pi) Internal Temperature of Pi IHU
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 7 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 8 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 BME280 Humidity STEM Payload Sensor BME280 Humidity
33 31 MIN BATT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery 2 Current INA219 Battery 2 Current
34 32 MIN DiodeTemp 12 C cubesatsim_rpm NONE 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 MIN Sensor 1 12 integer 1 NONE 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MIN SafeMode 1 - STATUS_ON_OFF NONE 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 MIN SimulatedTelemetry 1 - STATUS_ON_OFF NONE 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 MIN PayloadStatus1 1 - 17 NONE 0 0 0 Exp 3 STEM Payload status 1 failure indicator
40 38 MIN I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 MIN I2CBus1Failure 1 - 17 NONE 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 MIN I2CBus3Failure 1 - 17 NONE 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 MIN CameraFailure 1 - 17 NONE 2 4 0 Camera Camera failure indicator
44 42 MIN GroundCommands 4 - 1 NONE 3 3 0 Ground Commands Number of ground commands received
45 43 MIN RXAntenna 1 - 16 NONE 1 3 0 RX Antenna Receive antenna status
46 44 MIN TXAntenna 1 - 16 NONE 1 2 0 TX Antenna Transmit antenna status
47 45 MIN C2CStatus 2 - COMMAND_STATUS NONE 3 5 0 Command Control Command & Control Status
48 46 MIN Pad 56 - 0 NONE 0 0 0 NONE NONE

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spacecraft/FoxTelem_1.13i/CubeSatSim_rttelemetry.csv
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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|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
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
1 47 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 RT Sensor 2 12 integer 1 Experiments 6 8 3 Sensor 2 STEM Payload Extra Sensor 2
3 1 RT Sensor 3 12 integer 1 Experiments 6 9 3 Sensor 3 STEM Payload Extra Sensor 3
4 2 RT BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Battery Voltage INA219 Battery Voltage
5 3 RT SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around X Axis
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 RT SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 RT BATT_I 12 mA cubesatsim_current Battery 4 2 3 Battery Current INA219 Battery Current
9 7 RT Temperature 12 C cubesatsim_temperature Experiments 6 2 3 BME280 Temp STEM Payload Sensor BME280 Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage INA219 +X Panel Voltage
11 9 RT PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage INA219 -X Panel Voltage
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage INA219 +Y Panel Voltage
13 11 RT PANEL_MINUS_Y_V 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage INA219 -Y Panel Voltage
14 12 RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage INA219 +Z Panel Voltage
15 13 RT PANEL_MINUS_Z_V 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage INA219 -Z Panel Voltage
16 14 RT PANEL_PLUS_X_I 12 mA cubesatsim_current +X Panel 7 2 3 Current INA219 +X Panel Current
17 15 RT PANEL_MINUS_X_I 12 mA cubesatsim_current -X Panel 10 2 3 Current INA219 -X Panel Current
18 16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_current +Y Panel 8 2 3 Current INA219 +Y Panel Current
19 17 RT PANEL_MINUS_Y_I 12 mA cubesatsim_current -Y Panel 11 2 3 Current INA219 -Y Panel Current
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_current +Z Panel 9 2 3 Current INA219 +Z Panel Current
21 19 RT PANEL_MINUS_Z_I 12 mA cubesatsim_current -Z Panel 12 2 3 Current INA219 -Z Panel Current
22 20 RT BATT2_V 12 V cubesatsim_voltage|FLOAT2 Battery2 5 1 3 Battery2 Voltage INA219 Battery2 Voltage
23 21 RT SPIN 12 rpm cubesatsim_rpm Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 RT Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 BME280 Pressure STEM Payload Sensor BME280 Pressure
25 23 RT Altitude 12 m cubesatsim_altitude|INT Experiments 6 4 3 BME280 Altitude STEM Payload Sensor BME280 Altitude
26 24 RT Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 RT RSSI 12 dBm cubesatsim_rssi|INT Radio 1 1 3 RSSI Received Signal Strength Indication
28 26 RT IHUTemperature 12 C cubesatsim_temperature Computer Hardware 2 1 3 IHU Temp (Pi) Internal Temperature of Pi IHU
29 27 RT SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Y Axis
31 29 RT SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation STEM Payload Board MPU6050 Angular Veolcity around Z Axis
32 30 RT Humidity 12 % cubesatsim_temperature Experiments 6 5 3 BME280 Humidity STEM Payload Sensor BME280 Humidity
33 31 RT BATT2_I 12 mA cubesatsim_current Battery2 5 2 3 Battery2 Current INA219 Battery2 Current
34 32 RT DiodeTemp 12 C cubesatsim_rpm Experiments 6 6 3 Diode Temp STEM Payload Diode Temperature
35 33 RT Sensor 1 12 integer 1 Experiments 6 7 3 Sensor 1 STEM Payload Extra Sensor 1
36 34 RT STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 RT SafeMode 1 - STATUS_ON_OFF Computer Software 3 2 0 Safe Mode Safe Mode (Low Battery Voltage)
38 36 RT SimulatedTelemetry 1 - STATUS_ON_OFF Computer Software 3 4 0 Simulated Telemetry Simulated Telemetry Indicator
39 37 RT PayloadStatus1 1 - 17 NONE 0 0 0 Exp 3 STEM Payload status 1 failure indicator
40 38 RT I2CBus0Failure 1 - 17 NONE 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 RT I2CBus1Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 RT I2CBus3Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 RT CameraFailure 1 - 17 Computer Hardware 2 4 0 Camera Camera failure indicator
44 42 RT GroundCommands 4 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
45 43 RT RXAntenna 1 - 16 Radio 1 3 0 RX Antenna Receive antenna status
46 44 RT TXAntenna 1 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 RT C2CStatus 2 - COMMAND_STATUS Computer Software 3 5 0 Command Control Command & Control Status
48 46 RT Pad 56 - 0 NONE 0 0 0 NONE NONE

7
spacecraft/FoxTelem_1.13i/README.md
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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/23217474/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.
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