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6.0 KiB
6.0 KiB
| 1 | 60 | TYPE | FIELD | BITS | UNIT | CONVERSION | MODULE | MODULE_NUM | MODULE_LINE | LINE_TYPE | SHORT_NAME | DESCRIPTION |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2 | 0 | realTime | BATT_A_V | 12 | V | cubesatsim_voltage|FLOAT2 | NONE | 4 | 1 | 3 | Cell A | Battery A voltage (0-2.5V scale) |
| 3 | 1 | realTime | BATT_B_V | 12 | V | cubesatsim_voltage|FLOAT2 | NONE | 4 | 2 | 3 | Cell A+B | Battery A+B voltage (0-3.3V scale) |
| 4 | 2 | realTime | BATT_V | 12 | V | cubesatsim_voltage|FLOAT2 | Battery | 4 | 1 | 3 | Cell A+B+C Voltage | INA219 Battery A+B+C Voltage |
| 5 | 3 | realTime | SatelliteXAxisAcceleration | 12 | g | cubesatsim_acceleration|FLOAT2 | +X Panel | 7 | 4 | 3 | Acceleration | STEM Payload Board MPU6050 Acceleration around X Axis |
| 6 | 4 | realTime | SatelliteYAxisAcceleration | 12 | g | cubesatsim_acceleration|FLOAT2 | +Y Panel | 8 | 4 | 3 | Acceleration | STEM Payload Board MPU6050 Acceleration around Y Axis |
| 7 | 5 | realTime | SatelliteZAxisAcceleration | 12 | g | cubesatsim_acceleration|FLOAT2 | +Z Panel | 9 | 4 | 3 | Acceleration | STEM Payload Board MPU6050 Acceleration around Z Axis |
| 8 | 6 | realTime | battCurr | 12 | mA | cubesatsim_current | Battery | 4 | 2 | 3 | Current | INA219 Total Battery DC Current |
| 9 | 7 | realTime | Temperature | 12 | C | cubesatsim_temperature | Experiments | 6 | 2 | 3 | BME280 Temp | BME280 STEM Payload sensor temperature |
| 10 | 8 | realTime | posXv | 12 | V | cubesatsim_voltage|FLOAT2 | +X Panel | 7 | 1 | 3 | Voltage | INA219 +X solar panel Voltage |
| 11 | 9 | realTime | posYv | 12 | V | cubesatsim_voltage|FLOAT2 | +Y Panel | 8 | 1 | 3 | Voltage | INA219 +Y solar panel Voltage |
| 12 | 10 | realTime | posZv | 12 | V | cubesatsim_voltage|FLOAT2 | +Z Panel | 9 | 1 | 3 | Voltage | INA219 +Z solar panel Voltage |
| 13 | 11 | realTime | negXv | 12 | V | cubesatsim_voltage|FLOAT2 | -X Panel | 10 | 1 | 3 | Voltage | INA219 -X solar panel Voltage |
| 14 | 12 | realTime | negYv | 12 | V | cubesatsim_voltage|FLOAT2 | -Y Panel | 11 | 1 | 3 | Voltage | INA219 -Y solar panel Voltage |
| 15 | 13 | realTime | negZv | 12 | V | cubesatsim_voltage|FLOAT2 | -Z Panel | 12 | 1 | 3 | Voltage | INA219 -Z solar panel Voltage |
| 16 | 14 | realTime | posXi | 12 | mA | cubesatsim_current | +X Panel | 7 | 2 | 3 | Current | INA219 +X solar panel Current |
| 17 | 15 | realTime | posYi | 12 | mA | cubesatsim_current | +Y Panel | 8 | 2 | 3 | Current | INA219 +Y solar panel Current |
| 18 | 16 | realTime | posZi | 12 | mA | cubesatsim_current | +Z Panel | 9 | 2 | 3 | Current | INA219 +Z solar panel Current |
| 19 | 17 | realTime | negXi | 12 | mA | cubesatsim_current | -X Panel | 10 | 2 | 3 | Current | INA219 -X solar panel Current |
| 20 | 18 | realTime | negYi | 12 | mA | cubesatsim_current | -Y Panel | 11 | 2 | 3 | Current | INA219 -Y solar panel Current |
| 21 | 19 | realTime | negZi | 12 | mA | cubesatsim_current | -Z Panel | 12 | 2 | 3 | Current | INA219 -Z solar panel Current |
| 22 | 20 | realTime | PSUVoltage | 12 | V | cubesatsim_voltage|FLOAT2 | PSU | 5 | 1 | 3 | Voltage | INA219 Power Supply Voltage |
| 23 | 21 | realTime | spin | 12 | rpm | cubesatsim_rpm | Computer Software | 3 | 1 | 3 | Spacecraft Spin | Calculated spin rate using solar cells |
| 24 | 22 | realTime | Pressure | 12 | hPa | cubesatsim_pressure | Experiments | 6 | 3 | 3 | BME280 Pressure | BME280 STEM Payload sensor pressure |
| 25 | 23 | realTime | Altitude | 12 | m | cubesatsim_altitude | Experiments | 6 | 4 | 3 | BME280 Altitude | BME280 STEM Payload sensor altitude |
| 26 | 24 | realTime | Resets | 12 | - | 12 | NONE | 3 | 2 | 3 | Reset Count | Software Reset Count |
| 27 | 25 | realTime | rssi | 12 | dBm | cubesatsim_rssi|INT | Radio | 1 | 1 | 3 | RSSI | Received Signal Strength Indication |
| 28 | 26 | realTime | IHUcpuTemp | 12 | C | cubesatsim_temperature | Computer Hardware | 2 | 1 | 3 | IHU Temp (Pi) | Internal temperature of IHU from Pi |
| 29 | 27 | realTime | SatelliteXAxisAngularVelocity | 12 | dps | cubesatsim_rotation|INT | +X Panel | 7 | 3 | 3 | Rotation | STEM Payload Board MPU6050 Angular veolcity around X Axis |
| 30 | 28 | realTime | SatelliteYAxisAngularVelocity | 12 | dps | cubesatsim_rotation|INT | +Y Panel | 8 | 3 | 3 | Rotation | STEM Payload Board MPU6050 Angular veolcity around Y Axis |
| 31 | 29 | realTime | SatelliteZAxisAngularVelocity | 12 | dps | cubesatsim_rotation|INT | +Z Panel | 9 | 3 | 3 | Rotation | STEM Payload Board MPU6050 Angular veolcity around Z Axis |
| 32 | 30 | realTime | Humidity | 12 | % | cubesatsim_temperature | Experiments | 6 | 5 | 3 | BME280 Humidity | BME280 Humidity |
| 33 | 31 | realTime | PSUCurrent | 12 | mA | cubesatsim_current | PSU | 5 | 2 | 3 | Current | INA219 Power Supply DC Current |
| 34 | 32 | realTime | Sensor1 | 12 | C | cubesatsim_rpm | Experiments | 6 | 6 | 3 | Diode Temp | STEM Payload extra Sensor 1 (Diode Temperature) |
| 35 | 33 | realTime | Sensor2 | 12 | signed scaled | cubesatsim_rpm | Experiments | 6 | 7 | 3 | Sensor 2 | STEM Payload extra Sensor 2 |
| 36 | 34 | realTime | STEMPayloadStatus | 1 | - | 17 | Experiments | 6 | 1 | 0 | STEM Payload Status | STEM Payload STEM Payload board failure Indicator |
| 37 | 35 | realTime | SafeMode | 1 | - | STATUS_ON_OFF | Computer Software | 3 | 2 | 0 | Safe Mode | Safe Mode (Low Battery Voltage) |
| 38 | 36 | realTime | SimulatedTelemetry | 1 | - | STATUS_ON_OFF | Computer Software | 3 | 4 | 0 | Simulated Telemetry | Simulated Telemetry Indicator |
| 39 | 37 | realTime | PayloadStatus1 | 1 | - | 17 | NONE | 6 | 8 | 0 | Exp 3 | STEM Payload status 1 failure indicator |
| 40 | 38 | realTime | I2CBus0Failure | 1 | - | 17 | NONE | 2 | 2 | 0 | I2C Bus 0 | I2C bus 0 failure indicator |
| 41 | 39 | realTime | I2CBus1Failure | 1 | - | 17 | Computer Hardware | 2 | 2 | 0 | I2C Bus 1 | I2C bus 1 failure indicator |
| 42 | 40 | realTime | I2CBus3Failure | 1 | - | 17 | Computer Hardware | 2 | 3 | 0 | I2C Bus 3 | I2C bus 3 failure indicator |
| 43 | 41 | realTime | CameraFailure | 1 | - | 17 | Computer Hardware | 2 | 4 | 0 | Camera | Camera failure indicator |
| 44 | 42 | realTime | GroundCommands | 4 | - | 1 | Computer Software | 3 | 3 | 0 | Ground Commands | Number of ground commands received |
| 45 | 43 | realTime | RxAntenna | 1 | - | 16 | Radio | 1 | 3 | 0 | RX Antenna | Receive antenna status |
| 46 | 44 | realTime | TxAntenna | 2 | - | 16 | Radio | 1 | 2 | 0 | TX Antenna | Transmit antenna status |
| 47 | 45 | realTime | ICR3VProt | 12 | V | 43 | NONE | 7 | 2 | 3 | 3V Prot | ICR 3V Proteted |
| 48 | 46 | realTime | ICR2dot5V | 12 | V | 43 | NONE | 7 | 3 | 3 | 2.5V | ICR 2.5V |
| 49 | 47 | realTime | ICR2dot5VProt | 12 | V | 43 | NONE | 7 | 4 | 3 | 2.5V Prot | ICR 2.5V Protected |
| 50 | 48 | realTime | rf6 | 12 | - | 0 | NONE | 0 | 0 | 0 | None | None |
| 51 | 49 | realTime | rf7 | 12 | - | 0 | NONE | 0 | 0 | 0 | None | None |
| 52 | 50 | realTime | MuxTest | 12 | V | 43 | NONE | 7 | 5 | 3 | Sensor Power | Sensor Power Voltage at the ICR |
| 53 | 51 | realTime | LtVGACtl | 12 | V | 42 | NONE | 1 | 4 | 3 | VGA Control | Control Voltage to the Variable Gain Amplifier (VGA) |
| 54 | 52 | realTime | pad | 4 | - | 34 | NONE | 0 | 0 | 0 | None | Unused |
| 55 | 53 | realTime | IHUdiagData | 32 | - | 18 | NONE | 3 | 2 | 0 | Diagnostic Info | Diagnostic Data on IHU Performance |
| 56 | 54 | realTime | pad1 | 1 | - | 0 | NONE | 0 | 0 | 0 | NONE | Filler |
| 57 | 55 | 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 |
| 58 | 56 | realTime | swCmds | 32 | - | 35 | NONE | 7 | 6 | 0 | Diagnostic | ICR Diagnostic information |
| 59 | 57 | realTime | hwCmdCnt | 6 | - | 1 | NONE | 7 | 7 | 0 | HW Command Count | Number of hardware commands since last reset |
| 60 | 58 | realTime | swCmdCnt | 6 | - | 1 | NONE | 7 | 8 | 0 | SW Command Count | Number of software commands since last reset |
| 61 | 59 | realTime | pad2 | 28 | - | 0 | NONE | 0 | 0 | 0 | NONE | Filler |