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https://github.com/ArduPilot/ardupilot
synced 2025-03-02 19:53:57 -04:00
AC_WPNav: allow position control to get ekf navigation scalars directly
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@ -159,7 +159,7 @@ void AC_Circle::update()
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}
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// update position controller
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_pos_control.update_xy_controller(1.0f);
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_pos_control.update_xy_controller();
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}
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// get_closest_point_on_circle - returns closest point on the circle
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@ -203,7 +203,7 @@ float AC_Loiter::get_angle_max_cd() const
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}
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/// run the loiter controller
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void AC_Loiter::update(float ekfGndSpdLimit, float ekfNavVelGainScaler)
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void AC_Loiter::update()
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{
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// calculate dt
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float dt = _pos_control.time_since_last_xy_update();
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@ -215,8 +215,8 @@ void AC_Loiter::update(float ekfGndSpdLimit, float ekfNavVelGainScaler)
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_pos_control.set_max_speed_xy(_speed_cms);
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_pos_control.set_max_accel_xy(_accel_cmss);
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calc_desired_velocity(dt,ekfGndSpdLimit);
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_pos_control.update_xy_controller(ekfNavVelGainScaler);
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calc_desired_velocity(dt);
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_pos_control.update_xy_controller();
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}
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// sanity check parameters
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@ -228,8 +228,11 @@ void AC_Loiter::sanity_check_params()
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/// calc_desired_velocity - updates desired velocity (i.e. feed forward) with pilot requested acceleration and fake wind resistance
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/// updated velocity sent directly to position controller
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void AC_Loiter::calc_desired_velocity(float nav_dt, float ekfGndSpdLimit)
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void AC_Loiter::calc_desired_velocity(float nav_dt)
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{
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float ekfGndSpdLimit, ekfNavVelGainScaler;
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AP::ahrs_navekf().getEkfControlLimits(ekfGndSpdLimit, ekfNavVelGainScaler);
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// calculate a loiter speed limit which is the minimum of the value set by the LOITER_SPEED
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// parameter and the value set by the EKF to observe optical flow limits
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float gnd_speed_limit_cms = MIN(_speed_cms, ekfGndSpdLimit*100.0f);
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@ -51,7 +51,7 @@ public:
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float get_angle_max_cd() const;
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/// run the loiter controller
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void update(float ekfGndSpdLimit, float ekfNavVelGainScaler);
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void update();
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/// get desired roll, pitch which should be fed into stabilize controllers
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int32_t get_roll() const { return _pos_control.get_roll(); }
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@ -66,7 +66,7 @@ protected:
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/// updates desired velocity (i.e. feed forward) with pilot requested acceleration and fake wind resistance
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/// updated velocity sent directly to position controller
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void calc_desired_velocity(float nav_dt, float ekfGndSpdLimit);
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void calc_desired_velocity(float nav_dt);
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// references and pointers to external libraries
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const AP_InertialNav& _inav;
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@ -118,11 +118,11 @@ void AC_WPNav::init_brake_target(float accel_cmss)
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}
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// update_brake - run the stop controller - gets called at 400hz
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void AC_WPNav::update_brake(float ekfGndSpdLimit, float ekfNavVelGainScaler)
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void AC_WPNav::update_brake()
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{
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// send adjusted feed forward velocity back to position controller
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_pos_control.set_desired_velocity_xy(0.0f, 0.0f);
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_pos_control.update_xy_controller(ekfNavVelGainScaler);
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_pos_control.update_xy_controller();
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}
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///
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@ -522,7 +522,7 @@ bool AC_WPNav::update_wpnav()
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_pos_control.freeze_ff_z();
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}
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_pos_control.update_xy_controller(1.0f);
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_pos_control.update_xy_controller();
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check_wp_leash_length();
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_wp_last_update = AP_HAL::millis();
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@ -814,7 +814,7 @@ bool AC_WPNav::update_spline()
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}
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// run horizontal position controller
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_pos_control.update_xy_controller(1.0f);
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_pos_control.update_xy_controller();
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_wp_last_update = AP_HAL::millis();
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@ -64,7 +64,7 @@ public:
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void init_brake_target(float accel_cmss);
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///
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/// update_brake - run the brake controller - should be called at 400hz
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void update_brake(float ekfGndSpdLimit, float ekfNavVelGainScaler);
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void update_brake();
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///
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/// waypoint controller
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