mirror of https://github.com/ArduPilot/ardupilot
Copter: integrate attitude control EKF inertial-frame-reset
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@ -196,10 +196,10 @@ void Copter::failsafe_ekf_off_event(void)
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void Copter::check_ekf_reset()
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{
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// check for yaw reset
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float yaw_angle_change_rad = 0.0f;
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float yaw_angle_change_rad;
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uint32_t new_ekfYawReset_ms = ahrs.getLastYawResetAngle(yaw_angle_change_rad);
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if (new_ekfYawReset_ms != ekfYawReset_ms) {
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attitude_control->shift_ef_yaw_target(ToDeg(yaw_angle_change_rad) * 100.0f);
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attitude_control->inertial_frame_reset();
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ekfYawReset_ms = new_ekfYawReset_ms;
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Log_Write_Event(DATA_EKF_YAW_RESET);
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}
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@ -207,6 +207,7 @@ void Copter::check_ekf_reset()
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#if AP_AHRS_NAVEKF_AVAILABLE
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// check for change in primary EKF (log only, AC_WPNav handles position target adjustment)
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if ((EKF2.getPrimaryCoreIndex() != ekf_primary_core) && (EKF2.getPrimaryCoreIndex() != -1)) {
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attitude_control->inertial_frame_reset();
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ekf_primary_core = EKF2.getPrimaryCoreIndex();
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Log_Write_Error(ERROR_SUBSYSTEM_EKF_PRIMARY, ekf_primary_core);
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gcs().send_text(MAV_SEVERITY_WARNING, "EKF primary changed:%d", (unsigned)ekf_primary_core);
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