mirror of https://github.com/ArduPilot/ardupilot
91 lines
3.6 KiB
C++
91 lines
3.6 KiB
C++
#pragma once
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#include <AP_Common/AP_Common.h>
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#include <AP_Param/AP_Param.h>
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#include <AP_Math/AP_Math.h>
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#include <AP_Common/Location.h>
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#include <AP_InertialNav/AP_InertialNav.h>
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#include <AC_AttitudeControl/AC_PosControl.h>
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#include <AC_AttitudeControl/AC_AttitudeControl.h>
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#include <AC_Avoidance/AC_Avoid.h>
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class AC_Loiter
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{
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public:
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/// Constructor
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AC_Loiter(const AP_InertialNav& inav, const AP_AHRS_View& ahrs, AC_PosControl& pos_control, const AC_AttitudeControl& attitude_control);
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/// init_target to a position in cm from ekf origin
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void init_target(const Vector3f& position);
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/// initialize's position and feed-forward velocity from current pos and velocity
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void init_target();
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/// reduce response for landing
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void soften_for_landing();
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/// set pilot desired acceleration in centi-degrees
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// dt should be the time (in seconds) since the last call to this function
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void set_pilot_desired_acceleration(float euler_roll_angle_cd, float euler_pitch_angle_cd);
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/// gets pilot desired acceleration, body frame, [forward,right]
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Vector2f get_pilot_desired_acceleration() const { return Vector2f{_desired_accel.x, _desired_accel.y}; }
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/// clear pilot desired acceleration
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void clear_pilot_desired_acceleration() { _desired_accel.zero(); }
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/// get vector to stopping point based on a horizontal position and velocity
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void get_stopping_point_xy(Vector3f& stopping_point) const;
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/// get horizontal distance to loiter target in cm
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float get_distance_to_target() const { return _pos_control.get_pos_error_xy_cm(); }
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/// get bearing to target in centi-degrees
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int32_t get_bearing_to_target() const { return _pos_control.get_bearing_to_target_cd(); }
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/// get maximum lean angle when using loiter
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float get_angle_max_cd() const;
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/// run the loiter controller
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void update(bool avoidance_on = true);
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/// get desired roll, pitch which should be fed into stabilize controllers
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float get_roll() const { return _pos_control.get_roll_cd(); }
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float get_pitch() const { return _pos_control.get_pitch_cd(); }
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Vector3f get_thrust_vector() const { return _pos_control.get_thrust_vector(); }
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static const struct AP_Param::GroupInfo var_info[];
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protected:
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// sanity check parameters
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void sanity_check_params();
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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, bool avoidance_on = true);
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// references and pointers to external libraries
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const AP_InertialNav& _inav;
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const AP_AHRS_View& _ahrs;
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AC_PosControl& _pos_control;
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const AC_AttitudeControl& _attitude_control;
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// parameters
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AP_Float _angle_max; // maximum pilot commanded angle in degrees. Set to zero for 2/3 Angle Max
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AP_Float _speed_cms; // maximum horizontal speed in cm/s while in loiter
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AP_Float _accel_cmss; // loiter's max acceleration in cm/s/s
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AP_Float _brake_accel_cmss; // loiter's acceleration during braking in cm/s/s
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AP_Float _brake_jerk_max_cmsss;
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AP_Float _brake_delay; // delay (in seconds) before loiter braking begins after sticks are released
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// loiter controller internal variables
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Vector2f _desired_accel; // slewed pilot's desired acceleration in lat/lon frame
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Vector2f _predicted_accel;
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Vector2f _predicted_euler_angle;
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Vector2f _predicted_euler_rate;
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float _brake_timer;
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float _brake_accel;
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};
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