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Modify telemetry CSV to add timestamp and update data types

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Updated telemetry data format to include timestamp and change data types from integer to float for various sensors.
pacsat-v2.2-tlm2
Alan Johnston 4 weeks ago committed by GitHub
parent 195f8fac1a
commit 903c4e1e1a
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GPG Key ID: B5690EEEBB952194
1 changed files with 63 additions and 62 deletions
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spacecraft/PacSatGround_0.46o/PacSatSim_rttelemetry.csv
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@ -1,62 +1,63 @@
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,29,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
3,realTime,SatelliteXAxisAcceleration,12,g,30,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
4,realTime,SatelliteYAxisAcceleration,12,g,30,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
5,realTime,SatelliteZAxisAcceleration,12,g,30,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
6,realTime,BATT_I,12,mA,31,Battery,4,2,3,Battery Current,INA219 Battery Current
7,realTime,Temperature,12,C,5,Experiments,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
8,realTime,posXv,12,V,29,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage
9,realTime,posYv,12,V,29,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage
10,realTime,posZv,12,V,29,+Z Panel,9,1,3,Voltage,INA219 +Z solar panel Voltage
11,realTime,negXv,12,V,29,-X Panel,10,1,3,Voltage,INA219 -X solar panel Voltage
12,realTime,negYv,12,V,29,-Y Panel,11,1,3,Voltage,INA219 -Y solar panel Voltage
13,realTime,negZv,12,V,29,-Z Panel,12,1,3,Voltage,INA219 -Z solar panel Voltage
14,realTime,posXi,12,mA,31,+X Panel,7,2,3,Current,INA219 +X solar panel Current
15,realTime,posYi,12,mA,31,+Y Panel,8,2,3,Current,INA219 +Y solar panel Current
16,realTime,posZi,12,mA,31,+Z Panel,9,2,3,Current,INA219 +Z solar panel Current
17,realTime,negXi,12,mA,31,-X Panel,10,2,3,Current,INA219 -X solar panel Current
18,realTime,negYi,12,mA,31,-Y Panel,11,2,3,Current,INA219 -Y solar panel Current
19,realTime,negZi,12,mA,31,-Z Panel,12,2,3,Current,INA219 -Z solar panel Current
20,realTime,BATT2_V,12,V,29,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
21,realTime,spin,12,rpm,32,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,realTime,Pressure,12,hPa,0,Experiments,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure
23,realTime,Altitude,12,m,12,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,31,Radio,1,1,3,RSSI,Received Signal Strength Indication
26,realTime,IHUcpuTemp,12,C,5,Computer Hardware,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi
27,realTime,SatelliteXAxisAngularVelocity,12,dps,31,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis
28,realTime,SatelliteYAxisAngularVelocity,12,dps,31,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
29,realTime,SatelliteZAxisAngularVelocity,12,dps,31,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
30,realTime,Humidity,12,%,5,Experiments,6,5,3,BME280 Humidity,BME280 Humidity
31,realTime,BAT2_I,12,mA,31,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
32,realTime,DiodeTemp,12,C,32,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,-,33,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
36,realTime,SimulatedTelemetry,1,-,33,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,-,34,Computer Software,3,5,0,Command Control, Command & Control Status
46,realTime,ICR3VProt,12,V,0,NONE,7,2,3,3V Prot,ICR 3V Proteted
47,realTime,ICR2dot5V,12,V,0,NONE,7,3,3,2.5V,ICR 2.5V
48,realTime,ICR2dot5VProt,12,V,0,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,0,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
52,realTime,LtVGACtl,12,V,0,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
62,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,long,timestamp,32,Sec,0,NONE,0,0,0,timestamp,This is the unix time in seconds
1,float,Sensor 2,12,integer,1,Experiments,6,8,3,Sensor 2,STEM Payload Extra Sensor 2
2,float,Sensor 3,12,integer,1,Experiments,6,9,3,Sensor 3,STEM Payload Extra Sensor 3
3,float,BATT_V,12,V,29,Battery,4,1,3,Battery Voltage,INA219 Battery Voltage
4,float,SatelliteXAxisAcceleration,12,g,30,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis
5,float,SatelliteYAxisAcceleration,12,g,30,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis
6,float,SatelliteZAxisAcceleration,12,g,30,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis
7,float,BATT_I,12,mA,31,Battery,4,2,3,Battery Current,INA219 Battery Current
8,float,Temperature,12,C,5,Experiments,6,2,3,BME280 Temp,BME280 STEM Payload sensor temperature
9,float,posXv,12,V,29,+X Panel,7,1,3,Voltage,INA219 +X solar panel Voltage
10,float,posYv,12,V,29,+Y Panel,8,1,3,Voltage,INA219 +Y solar panel Voltage
11,float,posZv,12,V,29,+Z Panel,9,1,3,Voltage,INA219 +Z solar panel Voltage
12,float,negXv,12,V,29,-X Panel,10,1,3,Voltage,INA219 -X solar panel Voltage
13,float,negYv,12,V,29,-Y Panel,11,1,3,Voltage,INA219 -Y solar panel Voltage
14,float,negZv,12,V,29,-Z Panel,12,1,3,Voltage,INA219 -Z solar panel Voltage
15,float,posXi,12,mA,31,+X Panel,7,2,3,Current,INA219 +X solar panel Current
16,float,posYi,12,mA,31,+Y Panel,8,2,3,Current,INA219 +Y solar panel Current
17,float,posZi,12,mA,31,+Z Panel,9,2,3,Current,INA219 +Z solar panel Current
18,float,negXi,12,mA,31,-X Panel,10,2,3,Current,INA219 -X solar panel Current
19,float,negYi,12,mA,31,-Y Panel,11,2,3,Current,INA219 -Y solar panel Current
20,float,negZi,12,mA,31,-Z Panel,12,2,3,Current,INA219 -Z solar panel Current
21,float,BATT2_V,12,V,29,Battery2,5,1,3,Battery2 Voltage,INA219 Battery2 Voltage
22,float,spin,12,rpm,32,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
23,float,Pressure,12,hPa,0,Experiments,6,3,3,BME280 Pressure,BME280 STEM Payload sensor pressure
24,float,Altitude,12,m,12,Experiments,6,4,3,BME280 Altitude,BME280 STEM Payload sensor altitude
25,float,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count
26,float,rssi,12,dBm,31,Radio,1,1,3,RSSI,Received Signal Strength Indication
27,float,IHUcpuTemp,12,C,5,Computer Hardware,2,1,3,IHU Temp (Pi),Internal temperature of IHU from Pi
28,float,SatelliteXAxisAngularVelocity,12,dps,31,+X Panel,7,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around X Axis
29,float,SatelliteYAxisAngularVelocity,12,dps,31,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Y Axis
30,float,SatelliteZAxisAngularVelocity,12,dps,31,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular veolcity around Z Axis
31,float,Humidity,12,%,5,Experiments,6,5,3,BME280 Humidity,BME280 Humidity
32,float,BAT2_I,12,mA,31,Battery2,5,2,3,Battery2 Current,INA219 Battery2 Current
33,float,DiodeTemp,12,C,32,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature
34,float,Sensor 1,12,integer,1,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
35,float,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status, STEM Payload STEM Payload board failure Indicator
36,float,SafeMode,1,-,33,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage)
37,float,SimulatedTelemetry,1,-,33,Computer Software,3,4,0,Simulated Telemetry,Simulated Telemetry Indicator
38,float,PayloadStatus1,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 1 failure indicator
39,float,I2CBus0Failure,1,-,17,NONE,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
40,float,I2CBus1Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 1,I2C bus 1 failure indicator
41,float,I2CBus3Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 3,I2C bus 3 failure indicator
42,float,CameraFailure,1,-,17,Computer Hardware,2,4,0,Camera,Camera failure indicator
43,float,GroundCommands,4,-,1,Computer Software,3,3,0,Ground Commands,Number of ground commands received
44,float,RxAntenna,1,-,16,Radio,1,3,0,RX Antenna,Receive antenna status
45,float,TxAntenna,1,-,16,Radio,1,2,0,TX Antenna,Transmit antenna status
46,float,C2CStatus,2,-,34,Computer Software,3,5,0,Command Control, Command & Control Status
47,float,ICR3VProt,12,V,0,NONE,7,2,3,3V Prot,ICR 3V Proteted
48,float,ICR2dot5V,12,V,0,NONE,7,3,3,2.5V,ICR 2.5V
49,float,ICR2dot5VProt,12,V,0,NONE,7,4,3,2.5V Prot,ICR 2.5V Protected
50,float,rf6,12,-,0,NONE,0,0,0,None,None
51,float,rf7,12,-,0,NONE,0,0,0,None,None
52,float,MuxTest,12,V,0,NONE,7,5,3,Sensor Power,Sensor Power Voltage at the ICR
53,float,LtVGACtl,12,V,0,NONE,1,4,3,VGA Control,Control Voltage to the Variable Gain Amplifier (VGA)
54,float,pad,4,-,34,NONE,0,0,0,None,Unused
55,float,IHUdiagData,32,-,18,NONE,3,2,0,Diagnostic Info,Diagnostic Data on IHU Performance
56,float,pad1,1,-,0,NONE,0,0,0,NONE,Filler
57,float,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,float,swCmds,32,-,35,NONE,7,6,0,Diagnostic,ICR Diagnostic information
59,float,hwCmdCnt,6,-,1,NONE,7,7,0,HW Command Count,Number of hardware commands since last reset
60,float,swCmdCnt,6,-,1,NONE,7,8,0,SW Command Count,Number of software commands since last reset
61,float,pad2,27,-,0,NONE,0,0,0,NONE,Filler

1 61 62 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION
2 0 realTime long Sensor 2 timestamp 12 32 integer Sec 1 0 Experiments NONE 6 0 8 0 3 0 Sensor 2 timestamp STEM Payload Extra Sensor 2 This is the unix time in seconds
3 1 realTime float Sensor 3 Sensor 2 12 integer 1 Experiments 6 9 8 3 Sensor 3 Sensor 2 STEM Payload Extra Sensor 3 STEM Payload Extra Sensor 2
4 2 realTime float BATT_V Sensor 3 12 V integer 29 1 Battery Experiments 4 6 1 9 3 Battery Voltage Sensor 3 INA219 Battery Voltage STEM Payload Extra Sensor 3
5 3 realTime float SatelliteXAxisAcceleration BATT_V 12 g V 30 29 +X Panel Battery 7 4 4 1 3 Acceleration Battery Voltage STEM Payload Board MPU6050 Acceleration around X Axis INA219 Battery Voltage
6 4 realTime float SatelliteYAxisAcceleration SatelliteXAxisAcceleration 12 g 30 +Y Panel +X Panel 8 7 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Y Axis STEM Payload Board MPU6050 Acceleration around X Axis
7 5 realTime float SatelliteZAxisAcceleration SatelliteYAxisAcceleration 12 g 30 +Z Panel +Y Panel 9 8 4 3 Acceleration STEM Payload Board MPU6050 Acceleration around Z Axis STEM Payload Board MPU6050 Acceleration around Y Axis
8 6 realTime float BATT_I SatelliteZAxisAcceleration 12 mA g 31 30 Battery +Z Panel 4 9 2 4 3 Battery Current Acceleration INA219 Battery Current STEM Payload Board MPU6050 Acceleration around Z Axis
9 7 realTime float Temperature BATT_I 12 C mA 5 31 Experiments Battery 6 4 2 3 BME280 Temp Battery Current BME280 STEM Payload sensor temperature INA219 Battery Current
10 8 realTime float posXv Temperature 12 V C 29 5 +X Panel Experiments 7 6 1 2 3 Voltage BME280 Temp INA219 +X solar panel Voltage BME280 STEM Payload sensor temperature
11 9 realTime float posYv posXv 12 V 29 +Y Panel +X Panel 8 7 1 3 Voltage INA219 +Y solar panel Voltage INA219 +X solar panel Voltage
12 10 realTime float posZv posYv 12 V 29 +Z Panel +Y Panel 9 8 1 3 Voltage INA219 +Z solar panel Voltage INA219 +Y solar panel Voltage
13 11 realTime float negXv posZv 12 V 29 -X Panel +Z Panel 10 9 1 3 Voltage INA219 -X solar panel Voltage INA219 +Z solar panel Voltage
14 12 realTime float negYv negXv 12 V 29 -Y Panel -X Panel 11 10 1 3 Voltage INA219 -Y solar panel Voltage INA219 -X solar panel Voltage
15 13 realTime float negZv negYv 12 V 29 -Z Panel -Y Panel 12 11 1 3 Voltage INA219 -Z solar panel Voltage INA219 -Y solar panel Voltage
16 14 realTime float posXi negZv 12 mA V 31 29 +X Panel -Z Panel 7 12 2 1 3 Current Voltage INA219 +X solar panel Current INA219 -Z solar panel Voltage
17 15 realTime float posYi posXi 12 mA 31 +Y Panel +X Panel 8 7 2 3 Current INA219 +Y solar panel Current INA219 +X solar panel Current
18 16 realTime float posZi posYi 12 mA 31 +Z Panel +Y Panel 9 8 2 3 Current INA219 +Z solar panel Current INA219 +Y solar panel Current
19 17 realTime float negXi posZi 12 mA 31 -X Panel +Z Panel 10 9 2 3 Current INA219 -X solar panel Current INA219 +Z solar panel Current
20 18 realTime float negYi negXi 12 mA 31 -Y Panel -X Panel 11 10 2 3 Current INA219 -Y solar panel Current INA219 -X solar panel Current
21 19 realTime float negZi negYi 12 mA 31 -Z Panel -Y Panel 12 11 2 3 Current INA219 -Z solar panel Current INA219 -Y solar panel Current
22 20 realTime float BATT2_V negZi 12 V mA 29 31 Battery2 -Z Panel 5 12 1 2 3 Battery2 Voltage Current INA219 Battery2 Voltage INA219 -Z solar panel Current
23 21 realTime float spin BATT2_V 12 rpm V 32 29 Computer Software Battery2 3 5 1 3 Spacecraft Spin Battery2 Voltage Calculated spin rate using solar cells INA219 Battery2 Voltage
24 22 realTime float Pressure spin 12 hPa rpm 0 32 Experiments Computer Software 6 3 3 1 3 BME280 Pressure Spacecraft Spin BME280 STEM Payload sensor pressure Calculated spin rate using solar cells
25 23 realTime float Altitude Pressure 12 m hPa 12 0 Experiments 6 4 3 3 BME280 Altitude BME280 Pressure BME280 STEM Payload sensor altitude BME280 STEM Payload sensor pressure
26 24 realTime float Resets Altitude 12 - m 12 NONE Experiments 3 6 2 4 3 Reset Count BME280 Altitude Software Reset Count BME280 STEM Payload sensor altitude
27 25 realTime float rssi Resets 12 dBm - 31 12 Radio NONE 1 3 1 2 3 RSSI Reset Count Received Signal Strength Indication Software Reset Count
28 26 realTime float IHUcpuTemp rssi 12 C dBm 5 31 Computer Hardware Radio 2 1 1 3 IHU Temp (Pi) RSSI Internal temperature of IHU from Pi Received Signal Strength Indication
29 27 realTime float SatelliteXAxisAngularVelocity IHUcpuTemp 12 dps C 31 5 +X Panel Computer Hardware 7 2 3 1 3 Rotation IHU Temp (Pi) STEM Payload Board MPU6050 Angular veolcity around X Axis Internal temperature of IHU from Pi
30 28 realTime float SatelliteYAxisAngularVelocity SatelliteXAxisAngularVelocity 12 dps 31 +Y Panel +X Panel 8 7 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Y Axis STEM Payload Board MPU6050 Angular veolcity around X Axis
31 29 realTime float SatelliteZAxisAngularVelocity SatelliteYAxisAngularVelocity 12 dps 31 +Z Panel +Y Panel 9 8 3 3 Rotation STEM Payload Board MPU6050 Angular veolcity around Z Axis STEM Payload Board MPU6050 Angular veolcity around Y Axis
32 30 realTime float Humidity SatelliteZAxisAngularVelocity 12 % dps 5 31 Experiments +Z Panel 6 9 5 3 3 BME280 Humidity Rotation BME280 Humidity STEM Payload Board MPU6050 Angular veolcity around Z Axis
33 31 realTime float BAT2_I Humidity 12 mA % 31 5 Battery2 Experiments 5 6 2 5 3 Battery2 Current BME280 Humidity INA219 Battery2 Current BME280 Humidity
34 32 realTime float DiodeTemp BAT2_I 12 C mA 32 31 Experiments Battery2 6 5 6 2 3 Diode Temp Battery2 Current STEM Payload Diode Temperature INA219 Battery2 Current
35 33 realTime float Sensor 1 DiodeTemp 12 integer C 1 32 Experiments 6 7 6 3 Sensor 1 Diode Temp STEM Payload Extra Sensor 1 STEM Payload Diode Temperature
36 34 realTime float STEMPayloadStatus Sensor 1 1 12 - integer 17 1 Experiments 6 1 7 0 3 STEM Payload Status Sensor 1 STEM Payload STEM Payload board failure Indicator STEM Payload Extra Sensor 1
37 35 realTime float SafeMode STEMPayloadStatus 1 - 33 17 Computer Software Experiments 3 6 2 1 0 Safe Mode STEM Payload Status Safe Mode (Low Battery Voltage) STEM Payload STEM Payload board failure Indicator
38 36 realTime float SimulatedTelemetry SafeMode 1 - 33 Computer Software 3 4 2 0 Simulated Telemetry Safe Mode Simulated Telemetry Indicator Safe Mode (Low Battery Voltage)
39 37 realTime float PayloadStatus1 SimulatedTelemetry 1 - 17 33 NONE Computer Software 6 3 8 4 0 Exp 3 Simulated Telemetry STEM Payload status 1 failure indicator Simulated Telemetry Indicator
40 38 realTime float I2CBus0Failure PayloadStatus1 1 - 17 NONE 2 6 2 8 0 I2C Bus 0 Exp 3 I2C bus 0 failure indicator STEM Payload status 1 failure indicator
41 39 realTime float I2CBus1Failure I2CBus0Failure 1 - 17 Computer Hardware NONE 2 2 0 I2C Bus 1 I2C Bus 0 I2C bus 1 failure indicator I2C bus 0 failure indicator
42 40 realTime float I2CBus3Failure I2CBus1Failure 1 - 17 Computer Hardware 2 3 2 0 I2C Bus 3 I2C Bus 1 I2C bus 3 failure indicator I2C bus 1 failure indicator
43 41 realTime float CameraFailure I2CBus3Failure 1 - 17 Computer Hardware 2 4 3 0 Camera I2C Bus 3 Camera failure indicator I2C bus 3 failure indicator
44 42 realTime float GroundCommands CameraFailure 4 1 - 1 17 Computer Software Computer Hardware 3 2 3 4 0 Ground Commands Camera Number of ground commands received Camera failure indicator
45 43 realTime float RxAntenna GroundCommands 1 4 - 16 1 Radio Computer Software 1 3 3 0 RX Antenna Ground Commands Receive antenna status Number of ground commands received
46 44 realTime float TxAntenna RxAntenna 1 - 16 Radio 1 2 3 0 TX Antenna RX Antenna Transmit antenna status Receive antenna status
47 45 realTime float C2CStatus TxAntenna 2 1 - 34 16 Computer Software Radio 3 1 5 2 0 Command Control TX Antenna Command & Control Status Transmit antenna status
48 46 realTime float ICR3VProt C2CStatus 12 2 V - 0 34 NONE Computer Software 7 3 2 5 3 0 3V Prot Command Control ICR 3V Proteted Command & Control Status
49 47 realTime float ICR2dot5V ICR3VProt 12 V 0 NONE 7 3 2 3 2.5V 3V Prot ICR 2.5V ICR 3V Proteted
50 48 realTime float ICR2dot5VProt ICR2dot5V 12 V 0 NONE 7 4 3 3 2.5V Prot 2.5V ICR 2.5V Protected ICR 2.5V
51 49 realTime float rf6 ICR2dot5VProt 12 - V 0 NONE 0 7 0 4 0 3 None 2.5V Prot None ICR 2.5V Protected
52 50 realTime float rf7 rf6 12 - 0 NONE 0 0 0 None None
53 51 realTime float MuxTest rf7 12 V - 0 NONE 7 0 5 0 3 0 Sensor Power None Sensor Power Voltage at the ICR None
54 52 realTime float LtVGACtl MuxTest 12 V 0 NONE 1 7 4 5 3 VGA Control Sensor Power Control Voltage to the Variable Gain Amplifier (VGA) Sensor Power Voltage at the ICR
55 53 realTime float pad LtVGACtl 4 12 - V 34 0 NONE 0 1 0 4 0 3 None VGA Control Unused Control Voltage to the Variable Gain Amplifier (VGA)
56 54 realTime float IHUdiagData pad 32 4 - 18 34 NONE 3 0 2 0 0 Diagnostic Info None Diagnostic Data on IHU Performance Unused
57 55 realTime float pad1 IHUdiagData 1 32 - 0 18 NONE 0 3 0 2 0 NONE Diagnostic Info Filler Diagnostic Data on IHU Performance
58 56 realTime float wodSize pad1 8 1 000s - 36 0 NONE 3 0 3 0 0 WOD Stored NONE Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds Filler
59 57 realTime float swCmds wodSize 32 8 - 000s 35 36 NONE 7 3 6 3 0 Diagnostic WOD Stored ICR Diagnostic information Number of WOD data payloads kept for each of Science and Housekeeping. In hundreds
60 58 realTime float hwCmdCnt swCmds 6 32 - 1 35 NONE 7 7 6 0 HW Command Count Diagnostic Number of hardware commands since last reset ICR Diagnostic information
61 59 realTime float swCmdCnt hwCmdCnt 6 - 1 NONE 7 8 7 0 SW Command Count HW Command Count Number of software commands since last reset Number of hardware commands since last reset
62 60 realTime float pad2 swCmdCnt 27 6 - 0 1 NONE 0 7 0 8 0 NONE SW Command Count Filler Number of software commands since last reset
63 61 float pad2 27 - 0 NONE 0 0 0 NONE Filler
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