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ekf2: allow wind dead-reckoning after manual position reset
Reset velocity using airspeed and start navigating
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@@ -93,7 +93,7 @@ void Ekf::controlAirDataFusion(const imuSample &imu_delayed)
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const bool is_airspeed_significant = airspeed_sample.true_airspeed > _params.arsp_thr;
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const bool is_airspeed_consistent = (_aid_src_airspeed.test_ratio > 0.f && _aid_src_airspeed.test_ratio < 1.f);
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const bool starting_conditions_passing = continuing_conditions_passing && is_airspeed_significant
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&& (is_airspeed_consistent || !_control_status.flags.wind); // if wind isn't already estimated, the states are reset when starting airspeed fusion
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&& (is_airspeed_consistent || !_control_status.flags.wind || _control_status.flags.inertial_dead_reckoning);
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if (_control_status.flags.fuse_aspd) {
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if (continuing_conditions_passing) {
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@@ -118,17 +118,16 @@ void Ekf::controlAirDataFusion(const imuSample &imu_delayed)
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} else if (starting_conditions_passing) {
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ECL_INFO("starting airspeed fusion");
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// If starting wind state estimation, reset the wind states and covariances before fusing any data
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// Also catch the case where sideslip fusion enabled wind estimation recently and didn't converge yet.
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const Vector2f wind_var_xy = getWindVelocityVariance();
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if (_control_status.flags.inertial_dead_reckoning && !is_airspeed_consistent) {
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resetVelUsingAirspeed(airspeed_sample);
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if (!_control_status.flags.wind || (wind_var_xy(0) + wind_var_xy(1) > sq(_params.initial_wind_uncertainty))) {
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// activate the wind states
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_control_status.flags.wind = true;
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// reset the wind speed states and corresponding covariances
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} else if (!_control_status.flags.wind || getWindVelocityVariance().longerThan(_params.initial_wind_uncertainty)) {
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// If starting wind state estimation, reset the wind states and covariances before fusing any data
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// Also catch the case where sideslip fusion enabled wind estimation recently and didn't converge yet.
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resetWindUsingAirspeed(airspeed_sample);
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}
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_control_status.flags.wind = true;
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_control_status.flags.fuse_aspd = true;
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}
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@@ -247,3 +246,18 @@ void Ekf::resetWindUsingAirspeed(const airspeedSample &airspeed_sample)
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_aid_src_airspeed.time_last_fuse = _time_delayed_us;
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}
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void Ekf::resetVelUsingAirspeed(const airspeedSample &airspeed_sample)
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{
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const float euler_yaw = getEulerYaw(_R_to_earth);
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// Estimate velocity using zero sideslip assumption and airspeed measurement
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Vector2f horizontal_velocity;
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horizontal_velocity(0) = _state.wind_vel(0) + airspeed_sample.true_airspeed * cosf(euler_yaw);
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horizontal_velocity(1) = _state.wind_vel(1) + airspeed_sample.true_airspeed * sinf(euler_yaw);
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float vel_var = NAN; // Do not reset the velocity variance as wind variance estimate is most likely not correct
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resetHorizontalVelocityTo(horizontal_velocity, vel_var);
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_aid_src_airspeed.time_last_fuse = _time_delayed_us;
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}
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@@ -788,6 +788,7 @@ private:
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// Reset the wind states using the current airspeed measurement, ground relative nav velocity, yaw angle and assumption of zero sideslip
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void resetWindUsingAirspeed(const airspeedSample &airspeed_sample);
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void resetVelUsingAirspeed(const airspeedSample &airspeed_sample);
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#endif // CONFIG_EKF2_AIRSPEED
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#if defined(CONFIG_EKF2_SIDESLIP)
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