#include "Copter.h"

#if MODE_CIRCLE_ENABLED == ENABLED

/*
 * Init and run calls for circle flight mode
 */

// circle_init - initialise circle controller flight mode
bool Copter::ModeCircle::init(bool ignore_checks)
{
    pilot_yaw_override = false;

    // initialize speeds and accelerations
    pos_control->set_max_speed_xy(wp_nav->get_default_speed_xy());
    pos_control->set_max_accel_xy(wp_nav->get_wp_acceleration());
    pos_control->set_max_speed_z(-get_pilot_speed_dn(), g.pilot_speed_up);
    pos_control->set_max_accel_z(g.pilot_accel_z);

    // initialise circle controller including setting the circle center based on vehicle speed
    copter.circle_nav->init();

    return true;
}

// circle_run - runs the circle flight mode
// should be called at 100hz or more
void Copter::ModeCircle::run()
{
    // initialize speeds and accelerations
    pos_control->set_max_speed_xy(wp_nav->get_default_speed_xy());
    pos_control->set_max_accel_xy(wp_nav->get_wp_acceleration());
    pos_control->set_max_speed_z(-get_pilot_speed_dn(), g.pilot_speed_up);
    pos_control->set_max_accel_z(g.pilot_accel_z);

    // get pilot's desired yaw rate (or zero if in radio failsafe)
    float target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
    if (!is_zero(target_yaw_rate)) {
        pilot_yaw_override = true;
    }

    // get pilot desired climb rate (or zero if in radio failsafe)
    float target_climb_rate = get_pilot_desired_climb_rate(channel_throttle->get_control_in());
    // adjust climb rate using rangefinder
    if (copter.rangefinder_alt_ok()) {
        // if rangefinder is ok, use surface tracking
        target_climb_rate = get_surface_tracking_climb_rate(target_climb_rate);
    }

    // if not armed set throttle to zero and exit immediately
    if (is_disarmed_or_landed()) {
        make_safe_spool_down();
        return;
    }

    // set motors to full range
    motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);

    // run circle controller
    copter.circle_nav->update();

    // call attitude controller
    if (pilot_yaw_override) {
        attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(copter.circle_nav->get_roll(),
                                                                      copter.circle_nav->get_pitch(),
                                                                      target_yaw_rate);
    } else {
        attitude_control->input_euler_angle_roll_pitch_yaw(copter.circle_nav->get_roll(),
                                                           copter.circle_nav->get_pitch(),
                                                           copter.circle_nav->get_yaw(), true);
    }

    // update altitude target and call position controller
    // protects heli's from inflight motor interlock disable
    if (motors->get_desired_spool_state() == AP_Motors::DesiredSpoolState::GROUND_IDLE && !ap.land_complete) {
        pos_control->set_alt_target_from_climb_rate(-abs(g.land_speed), G_Dt, false);
    } else {
        pos_control->set_alt_target_from_climb_rate(target_climb_rate, G_Dt, false);
    }
    pos_control->update_z_controller();
}

uint32_t Copter::ModeCircle::wp_distance() const
{
    return copter.circle_nav->get_distance_to_target();
}

int32_t Copter::ModeCircle::wp_bearing() const
{
    return copter.circle_nav->get_bearing_to_target();
}

#endif