#include "mode.h"
#include "Plane.h"

bool ModeLoiter::_enter()
{
    plane.throttle_allows_nudging = true;
    plane.auto_throttle_mode = true;
    plane.auto_navigation_mode = true;
    plane.do_loiter_at_location();
    plane.loiter_angle_reset();

#if SOARING_ENABLED == ENABLED
    if (plane.g2.soaring_controller.is_active()) {
        plane.g2.soaring_controller.init_thermalling();
        plane.g2.soaring_controller.get_target(plane.next_WP_loc); // ahead on flight path
    }
#endif

    return true;
}

void ModeLoiter::update()
{
    plane.calc_nav_roll();
    plane.calc_nav_pitch();
    plane.calc_throttle();
}

bool ModeLoiter::isHeadingLinedUp(const Location loiterCenterLoc, const Location targetLoc)
{
    // Return true if current heading is aligned to vector to targetLoc.
    // Tolerance is initially 10 degrees and grows at 10 degrees for each loiter circle completed.

    const uint16_t loiterRadius = abs(plane.aparm.loiter_radius);
    if (loiterCenterLoc.get_distance(targetLoc) < loiterRadius + loiterRadius*0.05) {
        /* Whenever next waypoint is within the loiter radius plus 5%,
           maintaining loiter would prevent us from ever pointing toward the next waypoint.
           Hence break out of loiter immediately
         */
        return true;
    }

    // Bearing in centi-degrees
    const int32_t bearing_cd = plane.current_loc.get_bearing_to(targetLoc);
    return isHeadingLinedUp_cd(bearing_cd);
}


bool ModeLoiter::isHeadingLinedUp_cd(const int32_t bearing_cd)
{
    // Return true if current heading is aligned to bearing_cd.
    // Tolerance is initially 10 degrees and grows at 10 degrees for each loiter circle completed.

    // get current heading.
    const int32_t heading_cd = (wrap_360(degrees(plane.ahrs.groundspeed_vector().angle())))*100;

    const int32_t heading_err_cd = wrap_180_cd(bearing_cd - heading_cd);

    /*
      Check to see if the the plane is heading toward the land
      waypoint. We use 20 degrees (+/-10 deg) of margin so that
      we can handle 200 degrees/second of yaw.

      After every full circle, extend acceptance criteria to ensure
      aircraft will not loop forever in case high winds are forcing
      it beyond 200 deg/sec when passing the desired exit course
    */

    // Use integer division to get discrete steps
    const int32_t expanded_acceptance = 1000 * (labs(plane.loiter.sum_cd) / 36000);

    if (labs(heading_err_cd) <= 1000 + expanded_acceptance) {
        // Want to head in a straight line from _here_ to the next waypoint instead of center of loiter wp

        // 0 to xtrack from center of waypoint, 1 to xtrack from tangent exit location
        if (plane.next_WP_loc.loiter_xtrack) {
            plane.next_WP_loc = plane.current_loc;
        }
        return true;
    }
    return false;
}