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4.3 KiB
4.3 KiB
| 1 | 46 | TYPE | FIELD | BITS | UNIT | CONVERSION | MODULE | MODULE_NUM | MODULE_LINE | LINE_TYPE | SHORT_NAME | 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 | 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) |
| 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 | 3 | RT | SatelliteXAxisAcceleration | 12 | g | cubesatsim_acceleration|FLOAT2 | +X Panel | 7 | 4 | 3 | Acceleration | Acceleration around X Axis |
| 6 | 4 | RT | SatelliteYAxisAcceleration | 12 | g | cubesatsim_acceleration|FLOAT2 | +Y Panel | 8 | 4 | 3 | Acceleration | Acceleration around Y Axis |
| 7 | 5 | RT | SatelliteZAxisAcceleration | 12 | g | cubesatsim_acceleration|FLOAT2 | +Z Panel | 9 | 4 | 3 | Acceleration | Acceleration around Z Axis |
| 8 | 6 | RT | TOTAL_BATT_I | 12 | mA | cubesatsim_current | Battery | 4 | 2 | 3 | Current | Total Battery DC current |
| 9 | 7 | RT | Temperature | 12 | C | cubesatsim_temperature | Experiments | 6 | 2 | 3 | Temperature | 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 | 9 | RT | PANEL_MINUS_X_V | 12 | V | cubesatsim_voltage|FLOAT2 | -X Panel | 10 | 1 | 3 | Voltage | -X Panel |
| 12 | 10 | RT | PANEL_PLUS_Y_V | 12 | V | cubesatsim_voltage|FLOAT2 | +Y Panel | 8 | 1 | 3 | Voltage | +Y Panel |
| 13 | 11 | RT | PANEL_MINUS_Y_V | 12 | V | cubesatsim_voltage|FLOAT2 | -Y Panel | 11 | 1 | 3 | Voltage | -Y Panel |
| 14 | 12 | RT | PANEL_PLUS_Z_V | 12 | V | cubesatsim_voltage|FLOAT2 | +Z Panel | 9 | 1 | 3 | Voltage | +Z Panel |
| 15 | 13 | RT | PANEL_MINUS_Z_V | 12 | V | cubesatsim_voltage|FLOAT2 | -Z Panel | 12 | 1 | 3 | Voltage | -Z Panel |
| 16 | 14 | RT | PANEL_PLUS_X_I | 12 | mA | cubesatsim_current | +X Panel | 7 | 2 | 3 | Current | +X Panel |
| 17 | 15 | RT | PANEL_MINUS_X_I | 12 | mA | cubesatsim_current | -X Panel | 10 | 2 | 3 | Current | -X Panel |
| 18 | 16 | RT | PANEL_PLUS_Y_I | 12 | mA | cubesatsim_current | +Y Panel | 8 | 2 | 3 | Current | +Y Panel |
| 19 | 17 | RT | PANEL_MINUS_Y_I | 12 | mA | cubesatsim_current | -Y Panel | 11 | 2 | 3 | Current | -Y Panel |
| 20 | 18 | RT | PANEL_PLUS_Z_I | 12 | mA | cubesatsim_current | +Z Panel | 9 | 2 | 3 | Current | +Z Panel |
| 21 | 19 | RT | PANEL_MINUS_Z_I | 12 | mA | cubesatsim_current | -Z Panel | 12 | 2 | 3 | Current | -Z Panel |
| 22 | 20 | RT | PSUVoltage | 12 | V | cubesatsim_voltage|FLOAT2 | PSU | 5 | 1 | 3 | Voltage | Power Supply Voltage |
| 23 | 21 | RT | SPIN | 12 | rpm | cubesatsim_rpm | Computer Software | 3 | 1 | 3 | Spacecraft Spin | Calculated spin rate using solar cells |
| 24 | 22 | RT | Pressure | 12 | bar | cubesatsim_pressure | Experiments | 6 | 3 | 3 | Pressure | STEM Payload Sensor Pressure |
| 25 | 23 | RT | Altitude | 12 | m | cubesatsim_altitude | Experiments | 6 | 4 | 3 | Altitude | STEM Payload Sensor Altitude |
| 26 | 24 | RT | Resets | 12 | - | 12 | NONE | 3 | 2 | 3 | Reset Count | Software Reset Count |
| 27 | 25 | RT | RSSI | 12 | dBm | cubesatsim_rssi|INT | Radio | 1 | 1 | 3 | RSSI | Received Signal Strength Indication |
| 28 | 26 | RT | IHUTemperature | 12 | C | cubesatsim_temperature | Computer Hardware | 2 | 1 | 3 | Temperature | Internal Temperature of IHU |
| 29 | 27 | RT | SatelliteXAxisAngularVelocity | 12 | dps | cubesatsim_rotation|INT | +X Panel | 7 | 3 | 3 | Rotation | 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 | 29 | RT | SatelliteZAxisAngularVelocity | 12 | dps | cubesatsim_rotation|INT | +Z Panel | 9 | 3 | 3 | Rotation | Angular Veolcity around Z Axis |
| 32 | 30 | RT | Humidity | 12 | % | cubesatsim_temperature | Experiments | 6 | 5 | 3 | Humidity | STEM Payload Sensor Humidity |
| 33 | 31 | RT | PSUCurrent | 12 | mA | cubesatsim_current | PSU | 5 | 2 | 3 | Current | Power Supply DC Current |
| 34 | 32 | RT | Sensor1 | 12 | C | cubesatsim_rpm | Experiments | 6 | 6 | 3 | Diode Temperature | STEM Payload Extra Sensor 1 (Diode Temperature) |
| 35 | 33 | RT | Sensor2 | 12 | signed scaled | cubesatsim_rpm | Experiments | 6 | 7 | 3 | Sensor 2 | STEM Payload Extra Sensor 2 |
| 36 | 34 | RT | STEMPayloadStatus | 1 | - | 17 | Experiments | 6 | 1 | 0 | STEM Payload | STEM Payload Board Status |
| 37 | 35 | RT | Nominal Mode | 1 | - | 17 | Computer Software | 3 | 2 | 0 | Nominal Mode | Nominal Mode (Not Safe Mode) |
| 38 | 36 | RT | SimulatedTelemetry | 1 | - | 17 | Computer Software | 3 | 4 | 0 | Simulated Telemetry | Simulated Telemetry indicator |
| 39 | 37 | RT | PayloadStatus1 | 1 | - | 17 | NONE | 6 | 8 | 0 | Exp 3 | STEM Payload status 1 failure indicator |
| 40 | 38 | RT | I2CBus0Failure | 1 | - | 17 | Computer Hardware | 2 | 2 | 0 | I2C Bus 0 | I2C bus 0 failure indicator |
| 41 | 39 | RT | I2CBus1Failure | 1 | - | 17 | Computer Hardware | 2 | 3 | 0 | I2C Bus 1 | 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 | 41 | RT | CameraFailure | 1 | - | 17 | Computer Hardware | 2 | 5 | 0 | Camera | Camera failure indicator |
| 44 | 42 | RT | GroundCommands | 4 | - | 1 | Computer Software | 3 | 3 | 0 | Ground Commands | Number of ground commands received |
| 45 | 43 | RT | RXAntenna | 1 | - | 16 | Radio | 1 | 3 | 0 | RX Antenna | Receive antenna status |
| 46 | 44 | RT | TXAntenna | 1 | - | 16 | Radio | 1 | 2 | 0 | TX Antenna | Transmit antenna status |
| 47 | 45 | RT | Pad | 58 | - | 0 | NONE | 0 | 0 | 0 | NONE | NONE |