__max_num_sensor_instances: &max_num_sensor_instances 4 module_name: sensors parameters: - group: Sensor Calibration definitions: # Accelerometer calibration CAL_ACC${i}_ID: description: short: Accelerometer ${i} calibration device ID long: Device ID of the accelerometer this calibration applies to. category: System type: int32 default: 0 decimal: 3 num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_PRIO: description: short: Accelerometer ${i} priority category: System type: enum values: -1: Uninitialized 0: Disabled 1: Min 25: Low 50: Medium (Default) 75: High 100: Max default: -1 decimal: 3 num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_ROT: description: short: Accelerometer ${i} rotation relative to airframe long: | An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero. category: System type: enum values: -1: Internal 0: No rotation 1: Yaw 45° 2: Yaw 90° 3: Yaw 135° 4: Yaw 180° 5: Yaw 225° 6: Yaw 270° 7: Yaw 315° 8: Roll 180° 9: Roll 180°, Yaw 45° 10: Roll 180°, Yaw 90° 11: Roll 180°, Yaw 135° 12: Pitch 180° 13: Roll 180°, Yaw 225° 14: Roll 180°, Yaw 270° 15: Roll 180°, Yaw 315° 16: Roll 90° 17: Roll 90°, Yaw 45° 18: Roll 90°, Yaw 90° 19: Roll 90°, Yaw 135° 20: Roll 270° 21: Roll 270°, Yaw 45° 22: Roll 270°, Yaw 90° 23: Roll 270°, Yaw 135° 24: Pitch 90° 25: Pitch 270° 26: Pitch 180°, Yaw 90° 27: Pitch 180°, Yaw 270° 28: Roll 90°, Pitch 90° 29: Roll 180°, Pitch 90° 30: Roll 270°, Pitch 90° 31: Roll 90°, Pitch 180° 32: Roll 270°, Pitch 180° 33: Roll 90°, Pitch 270° 34: Roll 180°, Pitch 270° 35: Roll 270°, Pitch 270° 36: Roll 90°, Pitch 180°, Yaw 90° 37: Roll 90°, Yaw 270° 38: Roll 90°, Pitch 68°, Yaw 293° 39: Pitch 315° 40: Roll 90°, Pitch 315° min: -1 max: 40 default: -1 num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_XOFF: description: short: Accelerometer ${i} X-axis offset category: System type: float default: 0.0 unit: m/s^2 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_YOFF: description: short: Accelerometer ${i} Y-axis offset category: System type: float default: 0.0 unit: m/s^2 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_ZOFF: description: short: Accelerometer ${i} Z-axis offset category: System type: float default: 0.0 unit: m/s^2 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_XSCALE: description: short: Accelerometer ${i} X-axis scaling factor category: System type: float default: 1.0 decimal: 3 min: 0.1 max: 3.0 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_YSCALE: description: short: Accelerometer ${i} Y-axis scaling factor category: System type: float default: 1.0 decimal: 3 min: 0.1 max: 3.0 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_ACC${i}_ZSCALE: description: short: Accelerometer ${i} Z-axis scaling factor category: System type: float default: 1.0 decimal: 3 min: 0.1 max: 3.0 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 # Barometer calibration CAL_BARO${i}_ID: description: short: Barometer ${i} calibration device ID long: Device ID of the barometer this calibration applies to. category: System type: int32 default: 0 num_instances: *max_num_sensor_instances instance_start: 0 CAL_BARO${i}_PRIO: description: short: Barometer ${i} priority category: System type: enum values: -1: Uninitialized 0: Disabled 1: Min 25: Low 50: Medium (Default) 75: High 100: Max default: -1 num_instances: *max_num_sensor_instances instance_start: 0 CAL_BARO${i}_OFF: description: short: Barometer ${i} offset category: System type: float default: 0.0 decimal: 3 #unit: Pa volatile: true num_instances: *max_num_sensor_instances instance_start: 0 # Gyroscope calibration CAL_GYRO${i}_ID: description: short: Gyroscope ${i} calibration device ID long: Device ID of the gyroscope this calibration applies to. category: System type: int32 default: 0 num_instances: *max_num_sensor_instances instance_start: 0 CAL_GYRO${i}_PRIO: description: short: Gyroscope ${i} priority category: System type: enum values: -1: Uninitialized 0: Disabled 1: Min 25: Low 50: Medium (Default) 75: High 100: Max default: -1 num_instances: *max_num_sensor_instances instance_start: 0 CAL_GYRO${i}_ROT: description: short: Gyroscope ${i} rotation relative to airframe long: | An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero. category: System type: enum values: -1: Internal 0: No rotation 1: Yaw 45° 2: Yaw 90° 3: Yaw 135° 4: Yaw 180° 5: Yaw 225° 6: Yaw 270° 7: Yaw 315° 8: Roll 180° 9: Roll 180°, Yaw 45° 10: Roll 180°, Yaw 90° 11: Roll 180°, Yaw 135° 12: Pitch 180° 13: Roll 180°, Yaw 225° 14: Roll 180°, Yaw 270° 15: Roll 180°, Yaw 315° 16: Roll 90° 17: Roll 90°, Yaw 45° 18: Roll 90°, Yaw 90° 19: Roll 90°, Yaw 135° 20: Roll 270° 21: Roll 270°, Yaw 45° 22: Roll 270°, Yaw 90° 23: Roll 270°, Yaw 135° 24: Pitch 90° 25: Pitch 270° 26: Pitch 180°, Yaw 90° 27: Pitch 180°, Yaw 270° 28: Roll 90°, Pitch 90° 29: Roll 180°, Pitch 90° 30: Roll 270°, Pitch 90° 31: Roll 90°, Pitch 180° 32: Roll 270°, Pitch 180° 33: Roll 90°, Pitch 270° 34: Roll 180°, Pitch 270° 35: Roll 270°, Pitch 270° 36: Roll 90°, Pitch 180°, Yaw 90° 37: Roll 90°, Yaw 270° 38: Roll 90°, Pitch 68°, Yaw 293° 39: Pitch 315° 40: Roll 90°, Pitch 315° min: -1 max: 40 default: -1 num_instances: *max_num_sensor_instances instance_start: 0 CAL_GYRO${i}_XOFF: description: short: Gyroscope ${i} X-axis offset category: System type: float default: 0.0 decimal: 3 unit: rad/s volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_GYRO${i}_YOFF: description: short: Gyroscope ${i} Y-axis offset category: System type: float default: 0.0 decimal: 3 unit: rad/s volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_GYRO${i}_ZOFF: description: short: Gyroscope ${i} Z-axis offset category: System type: float default: 0.0 decimal: 3 unit: rad/s volatile: true num_instances: *max_num_sensor_instances instance_start: 0 # Magnetometer calibration CAL_MAG${i}_ID: description: short: Magnetometer ${i} calibration device ID long: Device ID of the magnetometer this calibration applies to. category: System type: int32 default: 0 num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_PRIO: description: short: Magnetometer ${i} priority category: System type: enum values: -1: Uninitialized 0: Disabled 1: Min 25: Low 50: Medium (Default) 75: High 100: Max default: -1 num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_ROT: description: short: Magnetometer ${i} rotation relative to airframe long: | An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero. category: System type: enum values: -1: Internal 0: No rotation 1: Yaw 45° 2: Yaw 90° 3: Yaw 135° 4: Yaw 180° 5: Yaw 225° 6: Yaw 270° 7: Yaw 315° 8: Roll 180° 9: Roll 180°, Yaw 45° 10: Roll 180°, Yaw 90° 11: Roll 180°, Yaw 135° 12: Pitch 180° 13: Roll 180°, Yaw 225° 14: Roll 180°, Yaw 270° 15: Roll 180°, Yaw 315° 16: Roll 90° 17: Roll 90°, Yaw 45° 18: Roll 90°, Yaw 90° 19: Roll 90°, Yaw 135° 20: Roll 270° 21: Roll 270°, Yaw 45° 22: Roll 270°, Yaw 90° 23: Roll 270°, Yaw 135° 24: Pitch 90° 25: Pitch 270° 26: Pitch 180°, Yaw 90° 27: Pitch 180°, Yaw 270° 28: Roll 90°, Pitch 90° 29: Roll 180°, Pitch 90° 30: Roll 270°, Pitch 90° 31: Roll 90°, Pitch 180° 32: Roll 270°, Pitch 180° 33: Roll 90°, Pitch 270° 34: Roll 180°, Pitch 270° 35: Roll 270°, Pitch 270° 36: Roll 90°, Pitch 180°, Yaw 90° 37: Roll 90°, Yaw 270° 38: Roll 90°, Pitch 68°, Yaw 293° 39: Pitch 315° 40: Roll 90°, Pitch 315° min: -1 max: 40 default: -1 num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_XOFF: description: short: Magnetometer ${i} X-axis offset category: System type: float default: 0.0 decimal: 3 unit: gauss volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_YOFF: description: short: Magnetometer ${i} Y-axis offset category: System type: float default: 0.0 decimal: 3 unit: gauss volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_ZOFF: description: short: Magnetometer ${i} Z-axis offset category: System type: float default: 0.0 decimal: 3 unit: gauss volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_XSCALE: description: short: Magnetometer ${i} X-axis scaling factor category: System type: float default: 1.0 decimal: 3 min: 0.1 max: 3.0 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_YSCALE: description: short: Magnetometer ${i} Y-axis scaling factor category: System type: float default: 1.0 decimal: 3 min: 0.1 max: 3.0 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_ZSCALE: description: short: Magnetometer ${i} Z-axis scaling factor category: System type: float default: 1.0 decimal: 3 min: 0.1 max: 3.0 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_XODIAG: description: short: Magnetometer ${i} X-axis off diagonal scale factor category: System type: float default: 0.0 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_YODIAG: description: short: Magnetometer ${i} Y-axis off diagonal scale factor category: System type: float default: 0.0 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_ZODIAG: description: short: Magnetometer ${i} Z-axis off diagonal scale factor category: System type: float default: 0.0 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_XCOMP: description: short: Magnetometer ${i} X Axis throttle compensation long: | Coefficient describing linear relationship between X component of magnetometer in body frame axis and either current or throttle depending on value of CAL_MAG_COMP_TYP. Unit for throttle-based compensation is [G] and for current-based compensation [G/kA] category: System type: float default: 0.0 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_YCOMP: description: short: Magnetometer ${i} Y Axis throttle compensation long: | Coefficient describing linear relationship between Y component of magnetometer in body frame axis and either current or throttle depending on value of CAL_MAG_COMP_TYP. Unit for throttle-based compensation is [G] and for current-based compensation [G/kA] category: System type: float default: 0.0 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0 CAL_MAG${i}_ZCOMP: description: short: Magnetometer ${i} Z Axis throttle compensation long: | Coefficient describing linear relationship between Z component of magnetometer in body frame axis and either current or throttle depending on value of CAL_MAG_COMP_TYP. Unit for throttle-based compensation is [G] and for current-based compensation [G/kA] category: System type: float default: 0.0 decimal: 3 volatile: true num_instances: *max_num_sensor_instances instance_start: 0