forked from Archive/PX4-Autopilot
EKF: Add on ground movement detector
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@ -87,6 +87,19 @@ void EstimatorInterface::setIMUData(uint64_t time_usec, uint64_t delta_ang_dt, u
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_delta_vel_prev = imu_sample_new.delta_vel;
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_vibe_metrics[2] = 0.99f * _vibe_metrics[2] + 0.01f * temp.norm();
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// detect if the vehicle is not moving when on ground
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if (!_control_status.flags.in_air) {
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if ((_vibe_metrics[1] * 4.0E4f > 1.0f)
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|| (_vibe_metrics[2] * 2.1E2f > 1.0f)
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|| ((imu_sample_new.delta_ang.norm() / dt) > 0.05f)) {
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_time_last_move_detect_us = _imu_sample_new.time_us;
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}
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_vehicle_at_rest = ((_imu_sample_new.time_us - _time_last_move_detect_us) > (uint64_t)1E6);
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} else {
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_time_last_move_detect_us = _imu_sample_new.time_us;
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_vehicle_at_rest = false;
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}
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// accumulate and down-sample imu data and push to the buffer when new downsampled data becomes available
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if (collect_imu(imu_sample_new)) {
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_imu_buffer.push(imu_sample_new);
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@ -457,13 +457,15 @@ protected:
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bool _deadreckon_time_exceeded{false}; // true if the horizontal nav solution has been deadreckoning for too long and is invalid
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bool _is_wind_dead_reckoning{false}; // true if we are navigating reliant on wind relative measurements
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// IMU vibration monitoring
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// IMU vibration and movement monitoring
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Vector3f _delta_ang_prev; // delta angle from the previous IMU measurement
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Vector3f _delta_vel_prev; // delta velocity from the previous IMU measurement
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float _vibe_metrics[3] {}; // IMU vibration metrics
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// [0] Level of coning vibration in the IMU delta angles (rad^2)
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// [1] high frequency vibraton level in the IMU delta angle data (rad)
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// [2] high frequency vibration level in the IMU delta velocity data (m/s)
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bool _vehicle_at_rest{false}; // true when the vehicle is at rest
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uint64_t _time_last_move_detect_us{0}; // timestamp of last movement detection event in microseconds
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// data buffer instances
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RingBuffer<imuSample> _imu_buffer;
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