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EKF: Add function to reset yaw and magnetic field states
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@ -128,6 +128,8 @@ private:
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float _mag_innov_var[3]; // earth magnetic field innovation variance
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float _heading_innov_var; // heading measurement innovation variance
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float _mag_declination = 0.0f; // magnetic declination used by reset and fusion functions (rad)
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// complementary filter states
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Vector3f _delta_angle_corr; // delta angle correction vector
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Vector3f _delta_vel_corr; // delta velocity correction vector
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@ -195,6 +197,10 @@ private:
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// reset velocity states of the ekf
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void resetVelocity();
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// reset the heading and magnetic field states using the declination and magnetometer measurements
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// return true if successful
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bool resetMagHeading(Vector3f &mag_init);
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// reset position states of the ekf (only vertical position)
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void resetPosition();
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@ -94,6 +94,36 @@ void Ekf::resetHeight()
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}
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}
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// Reset heading and magnetic field states
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bool Ekf::resetMagHeading(Vector3f &mag_init)
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{
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// If we don't a tilt estimate then we cannot initialise the yaw
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if (!_control_status.flags.tilt_align) {
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return false;
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}
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// get the roll, pitch, yaw estimates and set the yaw to zero
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matrix::Quaternion<float> q(_state.quat_nominal(0), _state.quat_nominal(1), _state.quat_nominal(2),
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_state.quat_nominal(3));
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matrix::Euler<float> euler_init(q);
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euler_init(2) = 0.0f;
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// rotate the magnetometer measurements into earth axes
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matrix::Dcm<float> R_to_earth_zeroyaw(euler_init);
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Vector3f mag_ef_zeroyaw = R_to_earth_zeroyaw * mag_init;
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euler_init(2) = _mag_declination - atan2f(mag_ef_zeroyaw(1), mag_ef_zeroyaw(0));
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// calculate initial quaternion states
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_state.quat_nominal = Quaternion(euler_init);
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_output_new.quat_nominal = _state.quat_nominal;
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// calculate initial earth magnetic field states
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matrix::Dcm<float> R_to_earth(euler_init);
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_state.mag_I = R_to_earth * mag_init;
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return true;
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}
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// This function forces the covariance matrix to be symmetric
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void Ekf::makeSymmetrical()
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{
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