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Add renamed BPSK telem files from FoxTelem

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pacsat-v2.2-tlm
Alan Johnston 2 months ago committed by GitHub
parent 103a98c3e5
commit d3f8697120
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GPG Key ID: B5690EEEBB952194
7 changed files with 287 additions and 0 deletions
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13
spacecraft/PacSatGround_0.46o/PacSatSim_Type1_HEALTH.frame
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number_of_payloads=6
payload0.name=rttelemetry
payload0.length=78
payload1.name=rttelemetry
payload1.length=78
payload2.name=rttelemetry
payload2.length=78
payload3.name=rttelemetry
payload3.length=78
payload4.name=rttelemetry
payload4.length=78
payload5.name=wodtelemetry
payload5.length=78

13
spacecraft/PacSatGround_0.46o/PacSatSim_Type2_MINMAX.frame
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number_of_payloads=6
payload0.name=rttelemetry
payload0.length=78
payload1.name=rttelemetry
payload1.length=78
payload2.name=rttelemetry
payload2.length=78
payload3.name=maxtelemetry
payload3.length=78
payload4.name=mintelemetry
payload4.length=78
payload5.name=wodtelemetry
payload5.length=78

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spacecraft/PacSatGround_0.46o/PacSatSim_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,0,0.1,0,0,0,0,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
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 0.1 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

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spacecraft/PacSatGround_0.46o/PacSatSim_maxtelemetry.csv
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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
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 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

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spacecraft/PacSatGround_0.46o/PacSatSim_mintelemetry.csv
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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
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 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/PacSatGround_0.46o/PacSatSim_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,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 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

62
spacecraft/PacSatGround_0.46o/PacSatSim_wodtelemetry.csv
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61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,WOD,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A,Battery A voltage (0-2.5V scale)
1,WOD,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,2,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,WOD,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,WOD,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
4,WOD,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
5,WOD,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
6,WOD,battCurr,12,mA,cubesatsim_current,Battery,4,2,4,Current,Total Battery DC current
7,WOD,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature
8,WOD,posXv,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X solar Panel voltage
9,WOD,posYv,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y solar Panel voltage
10,WOD,posZv,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z solar Panel voltage
11,WOD,negXv,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X solar Panel voltage
12,WOD,negYv,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y solar Panel voltage
13,WOD,negZv,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z solar Panel voltage
14,WOD,posXi,12,mA,cubesatsim_current,+X Panel,7,2,4,Current,+X solar Panel current
15,WOD,posYi,12,mA,cubesatsim_current,+Y Panel,8,2,4,Current,+Y solar Panel current
16,WOD,posZi,12,mA,cubesatsim_current,+Z Panel,9,2,4,Current,+Z solar Panel current
17,WOD,negXi,12,mA,cubesatsim_current,-X Panel,10,2,4,Current,-X solar Panel current
18,WOD,negYi,12,mA,cubesatsim_current,-Y Panel,11,2,4,Current,-Y solar Panel current
19,WOD,negZi,12,mA,cubesatsim_current,-Z Panel,12,2,4,Current,-Z solar Panel current
20,WOD,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply Voltage
21,WOD,spin,12,rpm,12,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,WOD,Pressure,12,bar,cubesatsim_pressure,Experiments,6,3,3,Pressure,STEM Payload Sensor Pressure
23,WOD,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor Altitude
24,WOD,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
25,WOD,rssi,12,dBm,14,Radio,1,1,3,RSSI,Received Signal Strength Indication
26,WOD,IHUcpuTemp,12,C,cubesatsim_temperature,Computer Hardware,2,1,3,Temperature,Internal Temperature of IHU
27,WOD,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis
28,WOD,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis
29,WOD,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis
30,WOD,Sensor1,12,raw,cubesatsim_sensor1|INT,Experiments,6,5,3,Sensor 1,STEM Payload Extra Sensor 1
31,WOD,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,WOD,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 2,STEM Payload Extra Sensor 2
33,WOD,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 3,STEM Payload Extra Sensor 3
34,WOD,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
35,WOD,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,WOD,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
37,WOD,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
38,WOD,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,WOD,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
40,WOD,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
41,WOD,CameraFailure,1,-,17,Computer Hardware,2,5,0,Camera,Camera failure indicator
42,WOD,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
43,WOD,RxAntDeploy,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
44,WOD,TxAntDeploy,2,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
45,WOD,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
46,WOD,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
47,WOD,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
48,WOD,rf6,12,-,0,NONE,0,0,0,None,None
49,WOD,rf7,12,-,0,NONE,0,0,0,None,None
50,WOD,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
51,WOD,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
52,WOD,pad,4,-,34,NONE,0,0,0,None,Unused
53,WOD,WODTimeStampReset,16,-,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected
54,WOD,pad1,17,-,0,NONE,0,0,0,NONE,Filler
55,WOD,wodSize,8,000s,36,NONE,3,3,0,WOD Stored,Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
56,WOD,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
57,WOD,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
58,WOD,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
59,WOD,WODTimeStampUpTime,25,s,1,NONE,0,0,0,MAX Timestamp Uptime, Time Whole Orbit Data was collected
60,WOD,pad2,3,-,0,NONE,0,0,0,NONE,Filler
1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 WOD BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A Battery A voltage (0-2.5V scale)
3 1 WOD BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 2 3 Cell A+B Battery A+B voltage (0-3.3V scale)
4 2 WOD BATT_V 12 V cubesatsim_voltage|FLOAT2 Battery 4 1 3 Cell A+B+C Voltage Battery A+B+C voltage (0-5.0V scale)
5 3 WOD SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +X Panel 7 4 3 Acceleration Acceleration around X Axis
6 4 WOD SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
7 5 WOD SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Z Panel 9 4 3 Acceleration Acceleration around Z Axis
8 6 WOD battCurr 12 mA cubesatsim_current Battery 4 2 4 Current Total Battery DC current
9 7 WOD Temperature 12 C cubesatsim_temperature Experiments 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 WOD posXv 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X solar Panel voltage
11 9 WOD posYv 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y solar Panel voltage
12 10 WOD posZv 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z solar Panel voltage
13 11 WOD negXv 12 V cubesatsim_voltage|FLOAT2 -X Panel 10 1 3 Voltage -X solar Panel voltage
14 12 WOD negYv 12 V cubesatsim_voltage|FLOAT2 -Y Panel 11 1 3 Voltage -Y solar Panel voltage
15 13 WOD negZv 12 V cubesatsim_voltage|FLOAT2 -Z Panel 12 1 3 Voltage -Z solar Panel voltage
16 14 WOD posXi 12 mA cubesatsim_current +X Panel 7 2 4 Current +X solar Panel current
17 15 WOD posYi 12 mA cubesatsim_current +Y Panel 8 2 4 Current +Y solar Panel current
18 16 WOD posZi 12 mA cubesatsim_current +Z Panel 9 2 4 Current +Z solar Panel current
19 17 WOD negXi 12 mA cubesatsim_current -X Panel 10 2 4 Current -X solar Panel current
20 18 WOD negYi 12 mA cubesatsim_current -Y Panel 11 2 4 Current -Y solar Panel current
21 19 WOD negZi 12 mA cubesatsim_current -Z Panel 12 2 4 Current -Z solar Panel current
22 20 WOD PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply Voltage
23 21 WOD spin 12 rpm 12 Computer Software 3 1 3 Spacecraft Spin Calculated spin rate using solar cells
24 22 WOD Pressure 12 bar cubesatsim_pressure Experiments 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 WOD Altitude 12 m cubesatsim_altitude Experiments 6 4 3 Altitude STEM Payload Sensor Altitude
26 24 WOD Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 25 WOD rssi 12 dBm 14 Radio 1 1 3 RSSI Received Signal Strength Indication
28 26 WOD IHUcpuTemp 12 C cubesatsim_temperature Computer Hardware 2 1 3 Temperature Internal Temperature of IHU
29 27 WOD SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation|INT +X Panel 7 3 3 Rotation Angular Veolcity around X Axis
30 28 WOD SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation Angular Veolcity around Y Axis
31 29 WOD SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Z Panel 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 WOD Sensor1 12 raw cubesatsim_sensor1|INT Experiments 6 5 3 Sensor 1 STEM Payload Extra Sensor 1
33 31 WOD PSUCurrent 12 mA cubesatsim_current PSU 5 2 3 Current Power Supply DC Current
34 32 WOD Sensor2 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 2 STEM Payload Extra Sensor 2
35 33 WOD Sensor3 12 signed scaled cubesatsim_sensor3|FLOAT2 Experiments 6 7 3 Sensor 3 STEM Payload Extra Sensor 3
36 34 WOD STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload Status STEM Payload STEM Payload Board Failure Indicator
37 35 WOD Nominal Mode 1 - 17 Computer Software 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 WOD PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 37 WOD PayloadStatus2 1 - 17 NONE 6 8 0 Exp 3 STEM Payload status 2 failure indicator
40 38 WOD I2CBus0Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 39 WOD I2CBus1Failure 1 - 17 Computer Hardware 2 3 0 I2C Bus 1 I2C bus 1 failure indicator
42 40 WOD I2CBus3Failure 1 - 17 Computer Hardware 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 41 WOD CameraFailure 1 - 17 Computer Hardware 2 5 0 Camera Camera failure indicator
44 42 WOD GroundCommands 4 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
45 43 WOD RxAntDeploy 1 - 16 Radio 1 3 0 RX Antenna Receive antenna status
46 44 WOD TxAntDeploy 2 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 45 WOD ICR3VProt 12 V 43 NONE 7 2 3 3V Prot ICR 3V Proteted
48 46 WOD ICR2dot5V 12 V 43 NONE 7 3 3 2.5V ICR 2.5V
49 47 WOD ICR2dot5VProt 12 V 43 NONE 7 4 3 2.5V Prot ICR 2.5V Protected
50 48 WOD rf6 12 - 0 NONE 0 0 0 None None
51 49 WOD rf7 12 - 0 NONE 0 0 0 None None
52 50 WOD MuxTest 12 V 43 NONE 7 5 3 Sensor Power Sensor Power Voltage at the ICR
53 51 WOD LtVGACtl 12 V 42 NONE 1 4 3 VGA Control Control Voltage to the Variable Gain Amplifier (VGA)
54 52 WOD pad 4 - 34 NONE 0 0 0 None Unused
55 53 WOD WODTimeStampReset 16 - 1 NONE 0 0 0 MAX Timestamp Uptime Time Whole Orbit Data was collected
56 54 WOD pad1 17 - 0 NONE 0 0 0 NONE Filler
57 55 WOD wodSize 8 000s 36 NONE 3 3 0 WOD Stored Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
58 56 WOD swCmds 32 - 35 NONE 7 6 0 Diagnostic ICR Diagnostic information
59 57 WOD hwCmdCnt 6 - 1 NONE 7 7 0 HW Command Count Number of hardware commands since last reset
60 58 WOD swCmdCnt 6 - 1 NONE 7 8 0 SW Command Count Number of software commands since last reset
61 59 WOD WODTimeStampUpTime 25 s 1 NONE 0 0 0 MAX Timestamp Uptime Time Whole Orbit Data was collected
62 60 WOD pad2 3 - 0 NONE 0 0 0 NONE Filler
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