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Update CubeSatSim_PSK_mintelemetry.csv from rt

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beta-ft2
Alan Johnston 1 year ago committed by GitHub
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spacecraft/FoxTelem_1.13e/CubeSatSim_PSK_mintelemetry.csv
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@ -1,59 +1,59 @@
61,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,MIN,Sensor2,12,integer,1,NONE,6,8,3,Cell A,Battery pair A voltage (0-2.5V scale)
1,MIN,Sensor3,12,integer,1,NONE,6,9,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
6,MIN,battCurr,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temp,STEM Payload Sensor Temperature
8,MIN,posXv,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X solar Panel voltage
9,MIN,posYv,12,V,cubesatsim_voltage|FLOAT2,NONE,8,1,3,Voltage,+Y solar Panel voltage
10,MIN,posZv,12,V,cubesatsim_voltage|FLOAT2,NONE,9,1,3,Voltage,+Z solar Panel voltage
11,MIN,negXv,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X solar Panel voltage
12,MIN,negYv,12,V,cubesatsim_voltage|FLOAT2,NONE,11,1,3,Voltage,-Y solar Panel voltage
13,MIN,negZv,12,V,cubesatsim_voltage|FLOAT2,NONE,12,1,3,Voltage,-Z solar Panel voltage
14,MIN,posXi,12,mA,cubesatsim_current,NONE,7,2,3,Current,+X solar Panel current
15,MIN,posYi,12,mA,cubesatsim_current,NONE,8,2,3,Current,+Y solar Panel current
16,MIN,posZi,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z solar Panel current
17,MIN,negXi,12,mA,cubesatsim_current,NONE,10,2,3,Current,-X solar Panel current
18,MIN,negYi,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y solar Panel current
19,MIN,negZi,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z solar Panel current
20,MIN,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Board Voltage,Power Supply Voltage
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,Pressure,STEM Payload Sensor Pressure
23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude
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,Temperature,Internal Temperature of IHU
27,MIN,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,7,3,3,Rotation,Angular Veolcity around X Axis
28,MIN,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,8,3,3,Rotation,Angular Veolcity around Y Axis
29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,Humidity
31,MIN,PSUCurrent,12,mA,cubesatsim_current,NONE,5,2,3,Current,Power Supply DC Current
32,MIN,DiodeTemp,12,C,cubesatsim_rpm ,NONE,6,6,3,Diode Temperature,STEM Payload Extra Sensor 1 (Diode Temperature)
33,MIN,Sensor1,12,integer,1,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,MIN,ICR3VProt,12,V,43,NONE,7,2,3,3V Prot,ICR 3V Proteted
35,MIN,ICR2dot5V,12,V,43,NONE,7,3,3,2.5V,ICR 2.5V
36,MIN,ICR2dot5VProt,12,V,43,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
37,MIN,rf6,12,-,0,NONE,0,0,0,None,None
38,MIN,rf7,12,-,0,NONE,0,0,0,None,None
39,MIN,MuxTest,12,V,43,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
40,MIN,LtVGACtl,12,V,42,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
41,MIN,pad,4,-,34,NONE,0,0,0,None,Unused
42,MIN,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
43,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status, STEM Payload STEM Payload Board Failure Indicator
44,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
45,MIN,expFailure2,1,-,17,NONE,7,7,0,Exp 2,Experiment 2 Failure Indicator
46,MIN,expFailure3,1,-,17,NONE,7,8,0,Exp 3,Experiment 3 Failure Indicator
47,MIN,I2CfailureBatt,1,-,17,NONE,2,2,0,Battery I2C,Battery I2C Bus failure indicator
48,MIN,I2CfailurePSU1,1,-,17,NONE,2,3,0,PSU1 I2C,PSU2 I2C Bus failure indicator
49,MIN,I2CfailurePSU2,1,-,17,NONE,2,4,0,PSU2 I2C,PSU2 I2C Bus failure indicator
50,MIN,TLMresets,4,-,1,NONE,2,6,0,Ground Resets,Number of times command stations reset stored telemetry
51,MIN,RxAntDeploy,1,-,16,NONE,1,3,0,RX Antenna,2m Antenna status
52,MIN,TxAntDeploy,1,-,16,NONE,1,2,0,TX Antenna,70cm Antenna status
53,MIN,C2CStatus,1,-,STATUS_ON_OFF,NONE,3,5,0,Command Control Status, Command & Control Status
54,MIN,I2CfailureRF,1,-,17,NONE,2,5,0,RF I2C,RF I2C Bus failure indicator
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,1,-,STATUS_ON_OFF,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

1 61 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 MIN Sensor2 Sensor 2 12 integer 1 NONE 6 8 3 Cell A Sensor 2 Battery pair A voltage (0-2.5V scale) STEM Payload Extra Sensor 2
3 1 MIN Sensor3 Sensor 3 12 integer 1 NONE 6 9 3 Cell A + B Sensor 3 Battery pairs A+B voltage (0-3.3V scale) STEM Payload Extra Sensor 3
4 2 MIN BATT_V 12 V cubesatsim_voltage|FLOAT2 NONE 4 1 3 Cell A+B+C Voltage Battery Voltage Battery A+B+C voltage (0-5.0V scale) INA219 Battery Voltage
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis STEM Payload Board MPU6050 Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis STEM Payload Board MPU6050 Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis STEM Payload Board MPU6050 Acceleration around Z Axis
8 6 MIN battCurr BATT_I 12 mA cubesatsim_current NONE 4 2 3 Current Battery Current Total Battery DC current INA219 Battery Current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temp BME280 Temp STEM Payload Sensor Temperature BME280 STEM Payload sensor temperature
10 8 MIN posXv 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X solar Panel voltage INA219 +X solar panel Voltage
11 9 MIN posYv 12 V cubesatsim_voltage|FLOAT2 NONE 8 1 3 Voltage +Y solar Panel voltage INA219 +Y solar panel Voltage
12 10 MIN posZv 12 V cubesatsim_voltage|FLOAT2 NONE 9 1 3 Voltage +Z solar Panel voltage INA219 +Z solar panel Voltage
13 11 MIN negXv 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X solar Panel voltage INA219 -X solar panel Voltage
14 12 MIN negYv 12 V cubesatsim_voltage|FLOAT2 NONE 11 1 3 Voltage -Y solar Panel voltage INA219 -Y solar panel Voltage
15 13 MIN negZv 12 V cubesatsim_voltage|FLOAT2 NONE 12 1 3 Voltage -Z solar Panel voltage INA219 -Z solar panel Voltage
16 14 MIN posXi 12 mA cubesatsim_current NONE 7 2 3 Current +X solar Panel current INA219 +X solar panel Current
17 15 MIN posYi 12 mA cubesatsim_current NONE 8 2 3 Current +Y solar Panel current INA219 +Y solar panel Current
18 16 MIN posZi 12 mA cubesatsim_current NONE 9 2 3 Current +Z solar Panel current INA219 +Z solar panel Current
19 17 MIN negXi 12 mA cubesatsim_current NONE 10 2 3 Current -X solar Panel current INA219 -X solar panel Current
20 18 MIN negYi 12 mA cubesatsim_current NONE 11 2 3 Current -Y solar Panel current INA219 -Y solar panel Current
21 19 MIN negZi 12 mA cubesatsim_current NONE 12 2 3 Current -Z solar Panel current INA219 -Z solar panel Current
22 20 MIN PSUVoltage BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Board Voltage Battery 2 Voltage Power Supply 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 Pressure BME280 Pressure STEM Payload Sensor Pressure BME280 STEM Payload sensor pressure
25 23 MIN Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude BME280 Altitude STEM Payload Sensor 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 Temperature IHU Temp (Pi) Internal Temperature of IHU Internal temperature of IHU from Pi
29 27 MIN SatelliteXAxisAngularVelocity 12 dps cubesatsim_rotation cubesatsim_rotation|INT NONE 7 3 3 Rotation Angular Veolcity around X Axis STEM Payload Board MPU6050 Angular veolcity around X Axis
30 28 MIN SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation cubesatsim_rotation|INT NONE 8 3 3 Rotation Angular Veolcity around Y Axis STEM Payload Board MPU6050 Angular veolcity around Y Axis
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation cubesatsim_rotation|INT NONE 9 3 3 Rotation Angular Veolcity around Z Axis STEM Payload Board MPU6050 Angular veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 Humidity BME280 Humidity Humidity BME280 Humidity
33 31 MIN PSUCurrent BAT2_I 12 mA cubesatsim_current NONE 5 2 3 Current Battery 2 Current Power Supply DC Current INA219 Battery 2 Current
34 32 MIN DiodeTemp 12 C cubesatsim_rpm cubesatsim_rpm NONE 6 6 3 Diode Temperature Diode Temp STEM Payload Extra Sensor 1 (Diode Temperature) STEM Payload Diode Temperature
35 33 MIN Sensor1 Sensor 1 12 integer 1 NONE 6 7 3 Sensor 2 Sensor 1 STEM Payload Extra Sensor 2 STEM Payload Extra Sensor 1
36 34 MIN ICR3VProt STEMPayloadStatus 12 1 V - 43 17 NONE 7 6 2 1 3 0 3V Prot STEM Payload Status ICR 3V Proteted STEM Payload STEM Payload board failure Indicator
37 35 MIN ICR2dot5V SafeMode 12 1 V - 43 STATUS_ON_OFF NONE 7 3 3 2 3 0 2.5V Safe Mode ICR 2.5V Safe Mode (Low Battery Voltage)
38 36 MIN ICR2dot5VProt SimulatedTelemetry 12 1 V - 43 STATUS_ON_OFF NONE 7 3 4 3 0 2.5V Prot Simulated Telemetry ICR 2.5V Protected Simulated Telemetry Indicator
39 37 MIN rf6 PayloadStatus1 12 1 - 0 17 NONE 0 6 0 8 0 None Exp 3 None STEM Payload status 1 failure indicator
40 38 MIN rf7 I2CBus0Failure 12 1 - 0 17 NONE 0 2 0 2 0 None I2C Bus 0 None I2C bus 0 failure indicator
41 39 MIN MuxTest I2CBus1Failure 12 1 V - 43 17 NONE 7 2 5 2 3 0 Sensor Power I2C Bus 1 Sensor Power Voltage at the ICR I2C bus 1 failure indicator
42 40 MIN LtVGACtl I2CBus3Failure 12 1 V - 42 17 NONE 1 2 4 3 3 0 VGA Control I2C Bus 3 Control Voltage to the Variable Gain Amplifier (VGA) I2C bus 3 failure indicator
43 41 MIN pad CameraFailure 4 1 - 34 17 NONE 0 2 0 4 0 None Camera Unused Camera failure indicator
44 42 MIN IHUdiagData GroundCommands 32 4 - 18 1 NONE 3 2 3 0 Diagnostic Info Ground Commands Diagnostic Data on IHU Performance Number of ground commands received
45 43 MIN STEMPayloadStatus RxAntenna 1 - 17 16 NONE 6 1 1 3 0 STEM Payload Status RX Antenna STEM Payload STEM Payload Board Failure Indicator Receive antenna status
46 44 MIN Nominal Mode TxAntenna 1 - 17 16 NONE 3 1 2 0 Nominal Mode TX Antenna Nominal Mode (Not Safe Mode) Transmit antenna status
47 45 MIN expFailure2 C2CStatus 1 - 17 STATUS_ON_OFF NONE 7 3 7 5 0 Exp 2 Command Control Experiment 2 Failure Indicator Command & Control Status
48 46 MIN expFailure3 ICR3VProt 1 12 - V 17 43 NONE 7 8 2 0 3 Exp 3 3V Prot Experiment 3 Failure Indicator ICR 3V Proteted
49 47 MIN I2CfailureBatt ICR2dot5V 1 12 - V 17 43 NONE 2 7 2 3 0 3 Battery I2C 2.5V Battery I2C Bus failure indicator ICR 2.5V
50 48 MIN I2CfailurePSU1 ICR2dot5VProt 1 12 - V 17 43 NONE 2 7 3 4 0 3 PSU1 I2C 2.5V Prot PSU2 I2C Bus failure indicator ICR 2.5V Protected
51 49 MIN I2CfailurePSU2 rf6 1 12 - 17 0 NONE 2 0 4 0 0 PSU2 I2C None PSU2 I2C Bus failure indicator None
52 50 MIN TLMresets rf7 4 12 - 1 0 NONE 2 0 6 0 0 Ground Resets None Number of times command stations reset stored telemetry None
53 51 MIN RxAntDeploy MuxTest 1 12 - V 16 43 NONE 1 7 3 5 0 3 RX Antenna Sensor Power 2m Antenna status Sensor Power Voltage at the ICR
54 52 MIN TxAntDeploy LtVGACtl 1 12 - V 16 42 NONE 1 2 4 0 3 TX Antenna VGA Control 70cm Antenna status Control Voltage to the Variable Gain Amplifier (VGA)
55 53 MIN C2CStatus pad 1 4 - STATUS_ON_OFF 34 NONE 3 0 5 0 0 Command Control Status None Command & Control Status Unused
56 54 MIN I2CfailureRF IHUdiagData 1 32 - 17 18 NONE 2 3 5 2 0 RF I2C Diagnostic Info RF I2C Bus failure indicator 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
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