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AlphaFilter add constructor that takes alpha and use in EKF
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@@ -48,9 +48,6 @@ bool Ekf::init(uint64_t timestamp)
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{
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bool ret = initialise_interface(timestamp);
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reset();
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_accel_lpf.setAlpha(.1f);
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_gyro_lpf.setAlpha(.1f);
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_mag_lpf.setAlpha(.1f);
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return ret;
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}
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@@ -468,11 +468,11 @@ private:
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bool _is_first_imu_sample{true};
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uint32_t _baro_counter{0}; ///< number of baro samples read during initialisation
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uint32_t _mag_counter{0}; ///< number of magnetometer samples read during initialisation
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AlphaFilter<Vector3f> _accel_lpf; ///< filtered accelerometer measurement used to align tilt (m/s/s)
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AlphaFilter<Vector3f> _gyro_lpf; ///< filtered gyro measurement used for alignment excessive movement check (rad/sec)
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AlphaFilter<Vector3f> _accel_lpf{0.1f}; ///< filtered accelerometer measurement used to align tilt (m/s/s)
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AlphaFilter<Vector3f> _gyro_lpf{0.1f}; ///< filtered gyro measurement used for alignment excessive movement check (rad/sec)
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// Variables used to perform in flight resets and switch between height sources
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AlphaFilter<Vector3f> _mag_lpf; ///< filtered magnetometer measurement for instant reset (Gauss)
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AlphaFilter<Vector3f> _mag_lpf{0.1f}; ///< filtered magnetometer measurement for instant reset (Gauss)
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float _hgt_sensor_offset{0.0f}; ///< set as necessary if desired to maintain the same height after a height reset (m)
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float _baro_hgt_offset{0.0f}; ///< baro height reading at the local NED origin (m)
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