| 1 |
46 |
46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHORT_NAME,DESCRIPTION |
TYPE |
FIELD |
BITS |
UNIT |
CONVERSION |
MODULE |
MODULE_NUM |
MODULE_LINE |
LINE_TYPE |
SHORT_NAME |
DESCRIPTION |
| 2 |
0 |
0,RT,Sensor2,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor2,STEM Payload Extra Sensor2 |
RT |
BATT_A_V |
12 |
V |
cubesatsim_voltage|FLOAT2 |
NONE |
0 |
0 |
3 |
Cell A |
Battery A voltage (0-2.5V scale) |
| 3 |
1 |
1,RT,Sensor3,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor23,STEM Payload Extra Sensor3 |
RT |
BATT_B_V |
12 |
V |
cubesatsim_voltage|FLOAT2 |
NONE |
0 |
0 |
3 |
Cell A+B |
Battery A+B voltage (0-3.3V scale) |
| 4 |
2 |
2,RT,BATT_V,12,V,cubesatsim_voltage|FLOAT2,Battery,4,1,3,Cell A+B+C Voltage,INA219 Battery A+B+C Voltage |
RT |
BATT_V |
12 |
V |
cubesatsim_voltage|FLOAT2 |
Battery |
4 |
1 |
3 |
Cell A+B+C Voltage |
INA219 Battery A+B+C Voltage |
| 5 |
3 |
3,RT,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+X Panel,7,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around X Axis |
RT |
SatelliteXAxisAcceleration |
12 |
g |
cubesatsim_acceleration|FLOAT2 |
+X Panel |
7 |
4 |
3 |
Acceleration |
STEM Payload Board MPU6050 Acceleration around X Axis |
| 6 |
4 |
4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Y Panel,8,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Y Axis |
RT |
SatelliteYAxisAcceleration |
12 |
g |
cubesatsim_acceleration|FLOAT2 |
+Y Panel |
8 |
4 |
3 |
Acceleration |
STEM Payload Board MPU6050 Acceleration around Y Axis |
| 7 |
5 |
5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,+Z Panel,9,4,3,Acceleration,STEM Payload Board MPU6050 Acceleration around Z Axis |
RT |
SatelliteZAxisAcceleration |
12 |
g |
cubesatsim_acceleration|FLOAT2 |
+Z Panel |
9 |
4 |
3 |
Acceleration |
STEM Payload Board MPU6050 Acceleration around Z Axis |
| 8 |
6 |
6,RT,BATT_I,12,mA,cubesatsim_current,Battery,4,2,3,Battery Current,Battery Current |
RT |
TOTAL_BATT_I |
12 |
mA |
cubesatsim_current |
Battery |
4 |
2 |
3 |
Current |
Total INA219 Battery DC Current |
| 9 |
7 |
7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,6,2,3,BME280 Temp,STEM Payload Sensor BME280 Temperature |
RT |
Temperature |
12 |
C |
cubesatsim_temperature |
Experiments |
6 |
2 |
3 |
BME280 Temp |
STEM Payload Sensor BME280 Temperature |
| 10 |
8 |
8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,+X Panel,7,1,3,Voltage,INA219 +X Panel Voltage |
RT |
PANEL_PLUS_X_V |
12 |
V |
cubesatsim_voltage|FLOAT2 |
+X Panel |
7 |
1 |
3 |
Voltage |
INA219 +X Panel Voltage |
| 11 |
9 |
9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,-X Panel,10,1,3,Voltage,INA219 -X Panel Voltage |
RT |
PANEL_MINUS_X_V |
12 |
V |
cubesatsim_voltage|FLOAT2 |
-X Panel |
10 |
1 |
3 |
Voltage |
INA219 -X Panel Voltage |
| 19 |
17 |
17,RT,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,-Y Panel,11,2,3,Current,INA219 -Y Panel Current |
RT |
PANEL_MINUS_Y_I |
12 |
mA |
cubesatsim_current |
-Y Panel |
11 |
2 |
3 |
Current |
INA219 -Y Panel Current |
| 20 |
18 |
18,RT,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,+Z Panel,9,2,3,Current,INA219 +Z Panel Current |
RT |
PANEL_PLUS_Z_I |
12 |
mA |
cubesatsim_current |
+Z Panel |
9 |
2 |
3 |
Current |
INA219 +Z Panel Current |
| 21 |
19 |
19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,-Z Panel,12,2,3,Current,INA219 -Z Panel Current |
RT |
PANEL_MINUS_Z_I |
12 |
mA |
cubesatsim_current |
-Z Panel |
12 |
2 |
3 |
Current |
INA219 -Z Panel Current |
| 22 |
20 |
20,RT,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,PSU,5,1,3,Battery2 Voltage,Battery2 Voltage |
RT |
PSUVoltage |
12 |
V |
cubesatsim_voltage|FLOAT2 |
PSU |
5 |
1 |
3 |
Voltage |
INA219 Power Supply Voltage |
| 23 |
21 |
21,RT,SPIN,12,rpm,cubesatsim_rpm,Computer Software,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells |
RT |
SPIN |
12 |
rpm |
cubesatsim_rpm |
Computer Software |
3 |
1 |
3 |
Spacecraft Spin |
Calculated spin rate using solar cells |
| 24 |
22 |
22,RT,Pressure,hPa,cubesatsim_pressure,Experiments,6,3,3,BME280 Pressure,STEM Payload Sensor BME280 Pressure |
RT |
Pressure |
12 |
hPa |
cubesatsim_pressure |
Experiments |
6 |
3 |
3 |
BME280 Pressure |
STEM Payload Sensor BME280 Pressure |
| 25 |
23 |
23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,6,4,3,BME280 Altitude,STEM Payload Sensor BME280 Altitude |
RT |
Altitude |
12 |
m |
cubesatsim_altitude |
Experiments |
6 |
4 |
3 |
BME280 Altitude |
STEM Payload Sensor BME280 Altitude |
| 26 |
24 |
24,RT,Resets,12,-,12,NONE,3,2,3,Reset Count, Software Reset Count |
RT |
Resets |
12 |
- |
12 |
NONE |
3 |
2 |
3 |
Reset Count |
Software Reset Count |
| 27 |
25 |
25,RT,RSSI,12,dBm,cubesatsim_rssi|INT,Radio,1,1,3,RSSI,Received Signal Strength Indication |
RT |
RSSI |
12 |
dBm |
cubesatsim_rssi|INT |
Radio |
1 |
1 |
3 |
RSSI |
Received Signal Strength Indication |
| 30 |
28 |
28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Y Panel,8,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Y Axis |
RT |
SatelliteYAxisAngularVelocity |
12 |
dps |
cubesatsim_rotation|INT |
+Y Panel |
8 |
3 |
3 |
Rotation |
STEM Payload Board MPU6050 Angular Veolcity around Y Axis |
| 31 |
29 |
29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,+Z Panel,9,3,3,Rotation,STEM Payload Board MPU6050 Angular Veolcity around Z Axis |
RT |
SatelliteZAxisAngularVelocity |
12 |
dps |
cubesatsim_rotation|INT |
+Z Panel |
9 |
3 |
3 |
Rotation |
STEM Payload Board MPU6050 Angular Veolcity around Z Axis |
| 32 |
30 |
30,RT,Humidity,12,%,cubesatsim_temperature,Experiments,6,5,3,BME280 Humidity,STEM Payload Sensor BME280 Humidity |
RT |
Humidity |
12 |
% |
cubesatsim_temperature |
Experiments |
6 |
5 |
3 |
BME280 Humidity |
STEM Payload Sensor BME280 Humidity |
| 33 |
31 |
31,RT,BATT2_I,12,mA,cubesatsim_current,PSU,5,2,3,Battery2 Current,Battery2 Current |
RT |
PSUCurrent |
12 |
mA |
cubesatsim_current |
PSU |
5 |
2 |
3 |
Current |
INA219 Power Supply DC Current |
| 34 |
32 |
32,RT,DiodeTemp,12,C,cubesatsim_rpm,Experiments,6,6,3,Diode Temp,STEM Payload Diode Temperature |
RT |
Sensor1 |
12 |
C |
cubesatsim_rpm |
Experiments |
6 |
6 |
3 |
Diode Temp |
STEM Payload Extra Sensor 1 (Diode Temperature) |
| 35 |
33 |
33,RT,Sensor1,12,signed scaled,cubesatsim_rpm,Experiments,6,7,3,Sensor 1,STEM Payload Extra Sensor 1 |
RT |
Sensor2 |
12 |
signed scaled |
cubesatsim_rpm |
Experiments |
6 |
7 |
3 |
Sensor 2 |
STEM Payload Extra Sensor 2 |
| 36 |
34 |
34,RT,STEMPayloadStatus,1,-,17,Experiments,6,1,0,STEM Payload Status,STEM Payload Board Status |
RT |
STEMPayloadStatus |
1 |
- |
17 |
Experiments |
6 |
1 |
0 |
STEM Payload Status |
STEM Payload Board Status |
| 37 |
35 |
35,RT,SafeMode,1,-,STATUS_ON_OFF,Computer Software,3,2,0,Safe Mode, Safe Mode (Low Battery Voltage) |
RT |
SafeMode |
1 |
- |
STATUS_ON_OFF |
Computer Software |
3 |
2 |
0 |
Safe Mode |
Safe Mode (Low Battery Voltage) |
| 38 |
36 |
36,RT,SimulatedTelemetry,1,-,STATUS_ON_OFF,Computer Software,3,4,0,Simulated Telemetry, Simulated Telemetry Indicator |
RT |
SimulatedTelemetry |
1 |
- |
STATUS_ON_OFF |
Computer Software |
3 |
4 |
0 |
Simulated Telemetry |
Simulated Telemetry Indicator |
|