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https://github.com/ArduPilot/ardupilot
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AC_AttitudeControl: apply EKF Z gain scaler
for flying with DCM
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parent
53e7436525
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@ -625,8 +625,8 @@ void AC_PosControl::update_xy_controller()
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}
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_last_update_xy_us = AP_HAL::micros64();
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float ekfGndSpdLimit, ekfNavVelGainScaler;
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AP::ahrs().getEkfControlLimits(ekfGndSpdLimit, ekfNavVelGainScaler);
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float ahrsGndSpdLimit, ahrsControlScaleXY;
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AP::ahrs().getControlLimits(ahrsGndSpdLimit, ahrsControlScaleXY);
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// Position Controller
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@ -634,7 +634,7 @@ void AC_PosControl::update_xy_controller()
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Vector2f vel_target = _p_pos_xy.update_all(_pos_target.x, _pos_target.y, curr_pos, _limit.pos_xy);
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// add velocity feed-forward scaled to compensate for optical flow measurement induced EKF noise
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vel_target *= ekfNavVelGainScaler;
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vel_target *= ahrsControlScaleXY;
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_vel_target.x = vel_target.x;
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_vel_target.y = vel_target.y;
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_vel_target.x += _vel_desired.x;
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@ -652,7 +652,7 @@ void AC_PosControl::update_xy_controller()
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}
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Vector2f accel_target = _pid_vel_xy.update_all(Vector2f{_vel_target.x, _vel_target.y}, _vehicle_horiz_vel, Vector2f(_limit_vector.x, _limit_vector.y));
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// acceleration to correct for velocity error and scale PID output to compensate for optical flow measurement induced EKF noise
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accel_target *= ekfNavVelGainScaler;
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accel_target *= ahrsControlScaleXY;
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// pass the correction acceleration to the target acceleration output
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_accel_target.x = accel_target.x;
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@ -962,6 +962,7 @@ void AC_PosControl::update_z_controller()
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float pos_target_zf = _pos_target.z;
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_vel_target.z = _p_pos_z.update_all(pos_target_zf, curr_alt, _limit.pos_down, _limit.pos_up);
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_vel_target.z *= AP::ahrs().getControlScaleZ();
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_pos_target.z = pos_target_zf;
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@ -972,6 +973,7 @@ void AC_PosControl::update_z_controller()
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const Vector3f& curr_vel = _inav.get_velocity();
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_accel_target.z = _pid_vel_z.update_all(_vel_target.z, curr_vel.z, _motors.limit.throttle_lower, _motors.limit.throttle_upper);
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_accel_target.z *= AP::ahrs().getControlScaleZ();
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// add feed forward component
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_accel_target.z += _accel_desired.z;
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