ardupilot/libraries/AP_Navigation/AP_Navigation.h

/// @file    AP_Navigation.h
/// @brief   generic navigation controller interface

/*
  This defines a generic interface for navigation controllers. Each
  specific controller should be a subclass of this generic
  interface. All variables used by controllers should be in their
  own class.
 */
#pragma once

#include <AP_Common/AP_Common.h>

class AP_Navigation {
public:
    // return the desired roll angle in centi-degrees to move towards
    // the target waypoint
    virtual int32_t nav_roll_cd(void) const = 0;

    // return the desired lateral acceleration in m/s/s to move towards
    // the target waypoint
    virtual float lateral_acceleration(void) const = 0;

    // note: all centi-degree values returned in AP_Navigation should
    // be wrapped at -18000 to 18000 in centi-degrees.

    // return the tracking bearing that the navigation controller is
    // using in centi-degrees. This is used to display an arrow on
    // ground stations showing the effect of the cross-tracking in the
    // controller
    virtual int32_t nav_bearing_cd(void) const = 0;

    // return the difference between the vehicles current course and
    // the nav_bearing_cd() in centi-degrees. A positive value means
    // the vehicle is tracking too far to the left of the correct
    // bearing.
    virtual int32_t bearing_error_cd(void) const = 0;

    // return the target bearing in centi-degrees. This is the bearing
    // from the vehicles current position to the target waypoint. This
    // should be calculated in the update_*() functions below.
    virtual int32_t target_bearing_cd(void) const = 0;

    // return the crosstrack error in meters. This is the distance in
    // the X-Y plane that we are off the desired track
    virtual float crosstrack_error(void) const = 0;
    virtual float crosstrack_error_integrator(void) const = 0;

    // return the distance in meters at which a turn should commence
    // to allow the vehicle to neatly move to the next track in the
    // mission when approaching a waypoint. Assumes 90 degree turn
    virtual float turn_distance(float wp_radius) const = 0;

    // return the distance in meters at which a turn should commence
    // to allow the vehicle to neatly move to the next track in the
    // mission when approaching a waypoint
    virtual float turn_distance(float wp_radius, float turn_angle) const = 0;

    // return the target loiter radius for the current location that
    // will not cause excessive airframe loading
    virtual float loiter_radius(const float radius) const = 0;

    // update the internal state of the navigation controller, given
    // the previous and next waypoints. This is the step function for
    // navigation control for path following between two points.  This
    // function is called at regular intervals (typically 10Hz). The
    // main flight code will call an output function (such as
    // nav_roll_cd()) after this function to ask for the new required
    // navigation attitude/steering.
    virtual void update_waypoint(const struct Location &prev_WP, const struct Location &next_WP, float dist_min = 0.0f) = 0;

    // update the internal state of the navigation controller for when
    // the vehicle has been commanded to circle about a point.  This
    // is the step function for navigation control for circling.  This
    // function is called at regular intervals (typically 10Hz). The
    // main flight code will call an output function (such as
    // nav_roll_cd()) after this function to ask for the new required
    // navigation attitude/steering.
    virtual void update_loiter(const struct Location &center_WP, float radius, int8_t loiter_direction) = 0;

    // update the internal state of the navigation controller, given a
    // fixed heading. This is the step function for navigation control
    // for a fixed heading.  This function is called at regular
    // intervals (typically 10Hz). The main flight code will call an
    // output function (such as nav_roll_cd()) after this function to
    // ask for the new required navigation attitude/steering.
    virtual void update_heading_hold(int32_t navigation_heading_cd) = 0;

    // update the internal state of the navigation controller for
    // level flight on the current heading. This is the step function
    // for navigation control for level flight.  This function is
    // called at regular intervals (typically 10Hz). The main flight
    // code will call an output function (such as nav_roll_cd()) after
    // this function to ask for the new required navigation
    // attitude/steering.
    virtual void update_level_flight(void) = 0;

    // return true if we have reached the target loiter location. This
    // may be a fuzzy decision, depending on internal navigation
    // parameters. For example the controller may return true only
    // when on the circular path around the waypoint, and not when
    // tracking towards the center. This function is only valid when
    // the update_loiter() method is used
    virtual bool reached_loiter_target(void) = 0;

    // notify Navigation controller that a new waypoint has just been
    // processed. This means that until we handle an update_XXX() function
    // the data is stale with old navigation information.
    virtual void set_data_is_stale(void) = 0;

    // return true if a new waypoint has been processed by mission
    // controller but the navigation controller still has old stale data
    // from previous waypoint navigation handling. This gets cleared on
    // every update_XXXXXX() call.
    virtual bool data_is_stale(void) const = 0;

    virtual void set_reverse(bool reverse) = 0;

    // add new navigation controllers to this enum. Users can then
    // select which navigation controller to use by setting the
    // NAV_CONTROLLER parameter
    enum ControllerType {
        CONTROLLER_DEFAULT      = 0,
        CONTROLLER_L1           = 1
    };
};