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Update CubeSatSim_rttelemetry.csv add Sensor2 and 3

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Alan Johnston 1 year ago committed by GitHub
parent 3e9ef0daf5
commit 280a29f798
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1 changed files with 7 additions and 7 deletions
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spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv
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@ -1,11 +1,11 @@
46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMIN_NAME,DESCRIPTION
0,MIN,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
1,MIN,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery 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)
0,MIN,SENSOR2,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor2,STEM Payload Extra Sensor2
1,MIN,SENSOR3,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor3,STEM Payload Extra Sensor3
2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,Battery Voltage
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,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
6,MIN,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,Battery current
7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature
8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel
9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel
@ -19,7 +19,7 @@
17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel
18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel
19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel
20,MIN,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery2 Voltage,Power Supply Voltage
20,MIN,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery2 Voltage,Battery2 Voltage
21,MIN,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
22,MIN,Pressure,12,bar,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
@ -31,8 +31,8 @@
29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,STEM Payload Sensor Humidity
31,MIN,BATT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery2 Current,Power Supply DC Current
32,MIN,Sensor1,12,signed raw,cubesatsim_rpm,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
33,MIN,Sensor2,12,signed scaled,cubesatsim_rpm,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
32,MIN,DIODE_T,12,signed raw,cubesatsim_rpm,NONE,6,6,3,Diode Temperature,Diode Temperature
33,MIN,Sensor1,12,signed scaled,cubesatsim_rpm,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 Board Status
35,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
36,MIN,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator

1 46 TYPE FIELD BITS UNIT CONVERSION MODULE MODULE_NUM MODULE_LINE LINE_TYPE SHOMIN_NAME DESCRIPTION
2 0 MIN BATT_A_V SENSOR2 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A Sensor2 Battery A voltage (0-2.5V scale) STEM Payload Extra Sensor2
3 1 MIN BATT_B_V SENSOR3 12 V cubesatsim_voltage|FLOAT2 NONE 0 0 3 Cell A+B Sensor3 Battery A+B voltage (0-3.3V scale) STEM Payload Extra Sensor3
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) Battery Voltage
5 3 MIN SatelliteXAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 7 4 3 Acceleration Acceleration around X Axis
6 4 MIN SatelliteYAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 8 4 3 Acceleration Acceleration around Y Axis
7 5 MIN SatelliteZAxisAcceleration 12 g cubesatsim_acceleration|FLOAT2 NONE 9 4 3 Acceleration Acceleration around Z Axis
8 6 MIN TOTAL_BATT_I BATT_I 12 mA cubesatsim_current NONE 4 2 3 Current Battery Current Total Battery DC current Battery current
9 7 MIN Temperature 12 C cubesatsim_temperature NONE 6 2 3 Temperature STEM Payload Sensor Temperature
10 8 MIN PANEL_PLUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 7 1 3 Voltage +X Panel
11 9 MIN PANEL_MINUS_X_V 12 V cubesatsim_voltage|FLOAT2 NONE 10 1 3 Voltage -X Panel
19 17 MIN PANEL_MINUS_Y_I 12 mA cubesatsim_current NONE 11 2 3 Current -Y Panel
20 18 MIN PANEL_PLUS_Z_I 12 mA cubesatsim_current NONE 9 2 3 Current +Z Panel
21 19 MIN PANEL_MINUS_Z_I 12 mA cubesatsim_current NONE 12 2 3 Current -Z Panel
22 20 MIN BATT2_V 12 V cubesatsim_voltage|FLOAT2 NONE 5 1 3 Battery2 Voltage Power Supply Voltage Battery2 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 bar cubesatsim_pressure NONE 6 3 3 Pressure STEM Payload Sensor Pressure
25 23 MIN Altitude 12 m cubesatsim_altitude NONE 6 4 3 Altitude STEM Payload Sensor Altitude
31 29 MIN SatelliteZAxisAngularVelocity 12 dps cubesatsim_rotation|INT NONE 9 3 3 Rotation Angular Veolcity around Z Axis
32 30 MIN Humidity 12 % cubesatsim_temperature NONE 6 5 3 Humidity STEM Payload Sensor Humidity
33 31 MIN BATT2_I 12 mA cubesatsim_current NONE 5 2 3 Battery2 Current Power Supply DC Current
34 32 MIN Sensor1 DIODE_T 12 signed raw cubesatsim_rpm NONE 6 6 3 Sensor 1 Diode Temperature STEM Payload Extra Sensor 1 Diode Temperature
35 33 MIN Sensor2 Sensor1 12 signed scaled cubesatsim_rpm NONE 6 7 3 Sensor 2 Sensor 1 STEM Payload Extra Sensor 2 STEM Payload Extra Sensor 1
36 34 MIN STEMPayloadStatus 1 - 17 NONE 6 1 0 STEM Payload Status STEM Payload Board Status
37 35 MIN Nominal Mode 1 - 17 NONE 3 2 0 Nominal Mode Nominal Mode (Not Safe Mode)
38 36 MIN PayloadStatus1 1 - 17 NONE 6 7 0 Exp 2 STEM Payload status 1 failure indicator
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