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CubeSatSim/spacecraft/FoxTelem_1.09b/CubeSatSim_rttelemetryFM.csv

46 lines
3.5 KiB

44,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION
0,RT,BATT_A_V,12,V,4,NONE,0,0,3,Cell A,Battery pair A voltage (0-2.5V scale)
1,RT,BATT_B_V,12,V,4,NONE,0,0,3,Cell A + B,Battery pairs A+B voltage (0-3.3V scale)
2,RT,BATT_V,12,V,4,Battery,3,1,3,Battery Voltage,Battery pairs A+B+C voltage (0-5.0V scale)
3,RT,BATT_A_T,12,C,8,NONE,0,0,3,Temperature A,Battery pair A temperature
4,RT,BATT_B_T,12,C,8,NONE,0,0,3,Temperature B,Battery pair B temperature
5,RT,BATT_C_T,12,C,8,NONE,0,0,3,Temperature C,Battery pair C temperature
6,RT,TOTAL_BATT_I,12,mA,4,Battery,3,2,3,Current,Total Battery DC current
7,RT,BATTBoardTemperature,12,C,8,NONE,0,0,3,Board Temp,Battery Card Temperature
8,RT,PANEL_PLUS_X_V,12,V,5,+X Panel,6,2,3,Voltage,+X Panel
9,RT,PANEL_MINUS_X_V,12,V,5,-X Panel,9,2,3,Voltage,-X Panel
10,RT,PANEL_PLUS_Y_V,12,V,5,+Y Panel,7,2,3,Voltage,+YPanel
11,RT,PANEL_MINUS_Y_V,12,V,5,-Y Panel,10,2,3,Voltage,-Y Panel
12,RT,PANEL_PLUS_Z_V,12,V,5,+Z Panel,8,2,3,Voltage,+Z Panel
13,RT,PANEL_MINUS_Z_V,12,V,5,-Z Panel,11,2,3,Voltage,-Z Panel
14,RT,PANEL_PLUS_X_I,12,mA,4,+X Panel,6,1,3,Current,+X Panel
15,RT,PANEL_MINUS_X_I,12,mA,4,-X Panel,9,1,3,Current,-X Panel
16,RT,PANEL_PLUS_Y_I,12,mA,4,+Y Panel,7,1,3,Current,+Y Panel
17,RT,PANEL_MINUS_Y_I,12,mA,4,-Y Panel,10,1,3,Current,-Y Panel
18,RT,PANEL_PLUS_Z_I,12,mA,4,+Z Panel,8,1,3,Current,+Z Panel
19,RT,PANEL_MINUS_Z_I,12,mA,4,-Z Panel,11,1,3,Current,-Z Panel
20,RT,PSUTemperature,12,C,7,PSU,4,2,3,Board Temp,Power Supply Card Temperature
21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells
22,RT,TXPACurrent,12,mA,10,NONE,1,0,3,PA Current,Transmit power amplifier current
23,RT,TXTemperature,12,C,7,NONE,1,0,3,TX Temperature,Transmitter card temperature
24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature
25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication
26,RT,IHUTemperature,12,C,15,Computer,2,1,3,Temperature,Internal Temperature of IHU
27,RT,SatelliteXAxisAngularVelocity,12,dps,13,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis
28,RT,SatelliteYAxisAngularVelocity,12,dps,13,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis
29,RT,SatelliteZAxisAngularVelocity,12,dps,13,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis
30,RT,EXP4Temperature,12,C,7,NONE,5,0,0,EXP4 Temperature,Not used
31,RT,PSUCurrent,12,mA,11,PSU,4,1,3,Current,Power Supply DC Current
32,RT,IHUDiagnosticData,32,-,18,Computer,2,7,0,Diagnostic Info,Diagnostic Data on IHU Performance
33,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,Vanderbilt Radiation,Vanderbilt University Vulcan Experiment Indicator
34,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used
35,RT,Experiment3FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used
36,RT,Experiment4FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used
37,RT,BATTI2CFailureIndications,1,-,17,Computer,2,3,0,Battery I2C,Battery I2C Bus failure indicator
38,RT,PSU1I2CFailureIndications,1,-,17,Computer,2,4,0,PSU1 I2C,PSU2 I2C Bus failure indicator
39,RT,PSU2I2CFailureIndications,1,-,17,Computer,2,5,0,PSU2 I2C,PSU2 I2C Bus failure indicator
40,RT,NumberofGroundCommandedTLMResets,4,-,1,Computer,2,6,0,Ground Resets,Number of times command stations reset stored telemetry
41,RT,RXAntenna,1,-,16,Radio,1,4,0,RX Antenna,70cm Antenna status
42,RT,TXAntenna,1,-,16,Radio,1,3,0,TX Antenna,2m Antenna status
43,RT,Pad,51,-,0,NONE,0,0,0,NONE,NONE

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