#pragma once /// @file AP_L1_Control.h /// @brief L1 Control algorithm. This is a instance of an /// AP_Navigation class /* * Originally written by Brandon Jones 2013 * * Modified by Paul Riseborough 2013 to provide: * - Explicit control over frequency and damping * - Explicit control over track capture angle * - Ability to use loiter radius smaller than L1 length */ #include #include #include #include #include class AP_L1_Control : public AP_Navigation { public: AP_L1_Control(AP_AHRS &ahrs, const AP_SpdHgtControl * spdHgtControl) : _ahrs(ahrs), _spdHgtControl(spdHgtControl) { AP_Param::setup_object_defaults(this, var_info); } /* see AP_Navigation.h for the definitions and units of these * functions */ int32_t nav_roll_cd(void) const; float lateral_acceleration(void) const; // return the desired track heading angle(centi-degrees) int32_t nav_bearing_cd(void) const; // return the heading error angle (centi-degrees) +ve to left of track int32_t bearing_error_cd(void) const; float crosstrack_error(void) const { return _crosstrack_error; } float crosstrack_error_integrator(void) const { return _L1_xtrack_i; } int32_t target_bearing_cd(void) const; float turn_distance(float wp_radius) const; float turn_distance(float wp_radius, float turn_angle) const; float loiter_radius (const float loiter_radius) const; void update_waypoint(const struct Location &prev_WP, const struct Location &next_WP); void update_loiter(const struct Location ¢er_WP, float radius, int8_t loiter_direction); void update_heading_hold(int32_t navigation_heading_cd); void update_level_flight(void); bool reached_loiter_target(void); // set the default NAVL1_PERIOD void set_default_period(float period) { _L1_period.set_default(period); } void set_data_is_stale(void) { _data_is_stale = true; } bool data_is_stale(void) const { return _data_is_stale; } // this supports the NAVl1_* user settable parameters static const struct AP_Param::GroupInfo var_info[]; void set_reverse(bool reverse) { _reverse = reverse; } private: // reference to the AHRS object AP_AHRS &_ahrs; // pointer to the SpdHgtControl object const AP_SpdHgtControl *_spdHgtControl; // lateral acceration in m/s required to fly to the // L1 reference point (+ve to right) float _latAccDem; // L1 tracking distance in meters which is dynamically updated float _L1_dist; // Status which is true when the vehicle has started circling the WP bool _WPcircle; // bearing angle (radians) to L1 point float _nav_bearing; // bearing error angle (radians) +ve to left of track float _bearing_error; // crosstrack error in meters float _crosstrack_error; // target bearing in centi-degrees from last update int32_t _target_bearing_cd; // L1 tracking loop period (sec) AP_Float _L1_period; // L1 tracking loop damping ratio AP_Float _L1_damping; // previous value of cross-track velocity float _last_Nu; // prevent indecision in waypoint tracking void _prevent_indecision(float &Nu); // integral feedback to correct crosstrack error. Used to ensure xtrack converges to zero. // For tuning purposes it's helpful to clear the integrator when it changes so a _prev is used float _L1_xtrack_i = 0; AP_Float _L1_xtrack_i_gain; float _L1_xtrack_i_gain_prev = 0; uint32_t _last_update_waypoint_us; bool _data_is_stale = true; AP_Float _loiter_bank_limit; bool _reverse = false; float get_yaw(); float get_yaw_sensor(); };