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alanbjohnston 5 years ago committed by GitHub
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spacecraft/FoxTelem_11a/CubeSatSim_rttelemetry.csv
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@ -1,47 +1,94 @@
46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,RT,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
1,RT,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
2,RT,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,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,Acceleration around X Axis
4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,Acceleration around Y Axis
5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,Acceleration around Z Axis
6,RT,TOTAL_BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Current,Total Battery DC current
7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,Temperature,STEM Payload Sensor Temperature
8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,+X Panel
9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,-X Panel
10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,+Y Panel,8,1,3,Voltage,+Y Panel
11,RT,PANEL_MINUS_Y_V,12,V,cubesatsim_voltage|FLOAT2,-Y Panel,11,1,3,Voltage,-Y Panel
12,RT,PANEL_PLUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,+Z Panel,9,1,3,Voltage,+Z Panel
13,RT,PANEL_MINUS_Z_V,12,V,cubesatsim_voltage|FLOAT2,-Z Panel,12,1,3,Voltage,-Z Panel
14,RT,PANEL_PLUS_X_I,12,mA,cubesatsim_current,+X Panel,7,2,3,Current,+X Panel
15,RT,PANEL_MINUS_X_I,12,mA,cubesatsim_current,-X Panel,10,2,3,Current,-X Panel
16,RT,PANEL_PLUS_Y_I,12,mA,cubesatsim_current,+Y Panel,8,2,3,Current,+Y Panel
17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,-Y Panel
18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,+Z Panel
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,-Z Panel
20,RT,PSUVoltage,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Voltage,Power Supply 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,Pressure,STEM Payload Sensor Pressure
23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,Altitude,STEM Payload Sensor 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,Temperature,Internal Temperature of IHU
27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+X Panel,7,3,3,Rotation,Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,Angular Veolcity around Z Axis
30,RT,Sensor1,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,Humidity
30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,Humidity,Humidity
31,RT,PSUCurrent,12,mA,cubesatsim_current,PSU,5,2,3,Current,Power Supply DC Current
32,RT,Sensor2,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,RT,Sensor3,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
32,RT,Sensor1,12,signed raw,cubesatsim_sensor2|INT,Experiments,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,RT,Sensor2,12,signed scaled,cubesatsim_sensor3|FLOAT2,Experiments,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload,STEM Payload Board Status
35,RT,Nominal Mode,1,-,17,Computer Software,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,RT,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator
37,RT,PayloadStatus2,1,-,17,NONE,6,8,0,Exp 3,STEM Payload status 2 failure indicator
38,RT,I2CBus0Failure,1,-,17,Computer Hardware,2,2,0,I2C Bus 0,I2C bus 0 failure indicator
39,RT,I2CBus1Failure,1,-,17,Computer Hardware,2,3,0,I2C Bus 1,I2C bus 1 failure indicator
40,RT,I2CBus3Failure,1,-,17,Computer Hardware,2,4,0,I2C Bus 3,I2C bus 3 failure indicator
41,RT,CameraFailure,1,-,17,Computer Hardware,2,5,0,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,Pad,58,-,0,NONE,0,0,0,NONE,NONE

1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHORT_NAME DESCRIPTION DESCRIPTION
2 0 RT BATT_A_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Battery A voltage (0-2.5V scale)
3 0 1 RT BATT_A_V BATT_B_V 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Cell A+B Battery A voltage (0-2.5V scale) Battery A+B voltage (0-3.3V scale)
4 2 RT 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 1 3 RT BATT_B_V SatelliteXAxisAcceleration 12 V g cubesatsim_voltage|FLOAT2 cubesatsim_acceleration|FLOAT2 NONE +X Panel 0 7 0 4 3 Cell A+B Acceleration Battery A+B voltage (0-3.3V scale) Acceleration around X Axis
6 4 RT SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 +Y Panel 8 4 3 Acceleration Acceleration around Y Axis
7 2 5 RT BATT_V SatelliteZAxisAcceleration 12 V g cubesatsim_voltage|FLOAT2 cubesatsim_acceleration|FLOAT2 Battery +Z Panel 4 9 1 4 3 Cell A+B+C Voltage Acceleration Battery A+B+C voltage (0-5.0V scale) Acceleration around Z Axis
8 6 RT TOTAL_BATT_I 12 mA cubesatsim_current Battery 4 2 3 Current Total Battery DC current
9 3 7 RT SatelliteXAxisAcceleration Temperature 12 g C cubesatsim_acceleration|FLOAT2 cubesatsim_temperature +X Panel Experiments 7 6 4 2 3 Acceleration Temperature Acceleration around X Axis STEM Payload Sensor Temperature
10 8 RT PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 +X Panel 7 1 3 Voltage +X Panel
11 4 9 RT SatelliteYAxisAcceleration PANEL_MINUS_X_V 12 g V cubesatsim_acceleration|FLOAT2 cubesatsim_voltage|FLOAT2 +Y Panel -X Panel 8 10 4 1 3 Acceleration Voltage Acceleration around Y Axis -X Panel
12 10 RT PANEL_PLUS_Y_V 12 V cubesatsim_voltage|FLOAT2 +Y Panel 8 1 3 Voltage +Y Panel
13 5 11 RT SatelliteZAxisAcceleration PANEL_MINUS_Y_V 12 g V cubesatsim_acceleration|FLOAT2 cubesatsim_voltage|FLOAT2 +Z Panel -Y Panel 9 11 4 1 3 Acceleration Voltage Acceleration around Z Axis -Y Panel
14 12 RT PANEL_PLUS_Z_V 12 V cubesatsim_voltage|FLOAT2 +Z Panel 9 1 3 Voltage +Z Panel
15 6 13 RT TOTAL_BATT_I PANEL_MINUS_Z_V 12 mA V cubesatsim_current cubesatsim_voltage|FLOAT2 Battery -Z Panel 4 12 2 1 3 Current Voltage Total Battery DC current -Z Panel
16 14 RT PANEL_PLUS_X_I 12 mA cubesatsim_current +X Panel 7 2 3 Current +X Panel
17 7 15 RT Temperature PANEL_MINUS_X_I 12 C mA cubesatsim_temperature cubesatsim_current Experiments -X Panel 6 10 2 3 Temperature Current STEM Payload Sensor Temperature -X Panel
18 16 RT PANEL_PLUS_Y_I 12 mA cubesatsim_current +Y Panel 8 2 3 Current +Y Panel
19 8 17 RT PANEL_PLUS_X_V PANEL_MINUS_Y_I 12 V mA cubesatsim_voltage|FLOAT2 cubesatsim_current +X Panel -Y Panel 7 11 1 2 3 Voltage Current +X Panel -Y Panel
20 18 RT PANEL_PLUS_Z_I 12 mA cubesatsim_current +Z Panel 9 2 3 Current +Z Panel
21 9 19 RT PANEL_MINUS_X_V PANEL_MINUS_Z_I 12 V mA cubesatsim_voltage|FLOAT2 cubesatsim_current -X Panel -Z Panel 10 12 1 2 3 Voltage Current -X Panel -Z Panel
22 20 RT PSUVoltage 12 V cubesatsim_voltage|FLOAT2 PSU 5 1 3 Voltage Power Supply Voltage
23 10 21 RT PANEL_PLUS_Y_V SPIN 12 V rpm cubesatsim_voltage|FLOAT2 cubesatsim_rpm +Y Panel Computer Software 8 3 1 3 Voltage Spacecraft Spin +Y Panel Calculated spin rate using solar cells
24 22 RT Pressure 12 hPa cubesatsim_pressure Experiments 6 3 3 Pressure STEM Payload Sensor Pressure
25 11 23 RT PANEL_MINUS_Y_V Altitude 12 V m cubesatsim_voltage|FLOAT2 cubesatsim_altitude -Y Panel Experiments 11 6 1 4 3 Voltage Altitude -Y Panel STEM Payload Sensor Altitude
26 24 RT Resets 12 - 12 NONE 3 2 3 Reset Count Software Reset Count
27 12 25 RT PANEL_PLUS_Z_V RSSI 12 V dBm cubesatsim_voltage|FLOAT2 cubesatsim_rssi|INT +Z Panel Radio 9 1 1 3 Voltage RSSI +Z Panel Received Signal Strength Indication
28 26 RT IHUTemperature 12 C cubesatsim_temperature Computer Hardware 2 1 3 Temperature Internal Temperature of IHU
29 13 27 RT PANEL_MINUS_Z_V SatelliteXAxisAngularVelocity 12 V dps cubesatsim_voltage|FLOAT2 cubesatsim_rotation|INT -Z Panel +X Panel 12 7 1 3 3 Voltage Rotation -Z Panel Angular Veolcity around X Axis
30 28 RT SatelliteYAxisAngularVelocity 12 dps cubesatsim_rotation|INT +Y Panel 8 3 3 Rotation Angular Veolcity around Y Axis
31 14 29 RT PANEL_PLUS_X_I SatelliteZAxisAngularVelocity 12 mA dps cubesatsim_current cubesatsim_rotation|INT +X Panel +Z Panel 7 9 2 3 3 Current Rotation +X Panel Angular Veolcity around Z Axis
32 30 RT Humidity 12 % cubesatsim_temperature Experiments 6 5 3 Humidity Humidity
33 15 31 RT PANEL_MINUS_X_I PSUCurrent 12 mA cubesatsim_current -X Panel PSU 10 5 2 3 Current -X Panel Power Supply DC Current
34 32 RT Sensor1 12 signed raw cubesatsim_sensor2|INT Experiments 6 6 3 Sensor 1 STEM Payload Extra Sensor 1
35 16 33 RT PANEL_PLUS_Y_I Sensor2 12 mA signed scaled cubesatsim_current cubesatsim_sensor3|FLOAT2 +Y Panel Experiments 8 6 2 7 3 Current Sensor 2 +Y Panel STEM Payload Extra Sensor 2
36 34 RT STEMPayloadStatus 1 - 17 Experiments 6 1 0 STEM Payload STEM Payload Board Status
37 17 35 RT PANEL_MINUS_Y_I Nominal Mode 12 1 mA - cubesatsim_current 17 -Y Panel Computer Software 11 3 2 3 0 Current Nominal Mode -Y Panel Nominal Mode (Not Safe Mode)
38 36 RT PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
39 18 37 RT PANEL_PLUS_Z_I PayloadStatus2 12 1 mA - cubesatsim_current 17 +Z Panel NONE 9 6 2 8 3 0 Current Exp 3 +Z Panel STEM Payload status 2 failure indicator
40 38 RT I2CBus0Failure 1 - 17 Computer Hardware 2 2 0 I2C Bus 0 I2C bus 0 failure indicator
41 19 39 RT PANEL_MINUS_Z_I I2CBus1Failure 12 1 mA - cubesatsim_current 17 -Z Panel Computer Hardware 12 2 2 3 3 0 Current I2C Bus 1 -Z Panel I2C bus 1 failure indicator
42 40 RT I2CBus3Failure 1 - 17 Computer Hardware 2 4 0 I2C Bus 3 I2C bus 3 failure indicator
43 20 41 RT PSUVoltage CameraFailure 12 1 V - cubesatsim_voltage|FLOAT2 17 PSU Computer Hardware 5 2 1 5 3 0 Voltage Camera Power Supply Voltage Camera failure indicator
44 42 RT GroundCommands 4 - 1 Computer Software 3 3 0 Ground Commands Number of ground commands received
45 21 43 RT SPIN RXAntenna 12 1 rpm - cubesatsim_rpm 16 Computer Software Radio 3 1 1 3 3 0 Spacecraft Spin RX Antenna Calculated spin rate using solar cells Receive antenna status
46 44 RT TXAntenna 1 - 16 Radio 1 2 0 TX Antenna Transmit antenna status
47 22 45 RT Pressure Pad 12 58 hPa - cubesatsim_pressure 0 Experiments NONE 6 0 3 0 3 0 Pressure NONE STEM Payload Sensor Pressure NONE
48
49 STEM Payload Sensor Altitude
50
51 Software Reset Count
52
53 Received Signal Strength Indication
54
55 Internal Temperature of IHU
56
57 Angular Veolcity around X Axis
58
59 Angular Veolcity around Y Axis
60
61 Angular Veolcity around Z Axis
62 Humidity
63
64
65 Power Supply DC Current
66 STEM Payload Extra Sensor 1
67 STEM Payload Extra Sensor 2
68
69
70
71 STEM Payload Board Status
72
73 Nominal Mode (Not Safe Mode)
74
75 STEM Payload status 1 failure indicator
76
77 STEM Payload status 2 failure indicator
78
79 I2C bus 0 failure indicator
80
81 I2C bus 1 failure indicator
82
83 I2C bus 3 failure indicator
84
85 Camera failure indicator
86
87 Number of ground commands received
88
89 Receive antenna status
90
91 Transmit antenna status
92
93 NONE
94
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