ardupilot/ArduPlane/mode_auto.cpp

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

bool ModeAuto::_enter()
{
    plane.throttle_allows_nudging = true;
    plane.auto_throttle_mode = true;
    plane.auto_navigation_mode = true;
    if (plane.quadplane.available() && plane.quadplane.enable == 2) {
        plane.auto_state.vtol_mode = true;
    } else {
        plane.auto_state.vtol_mode = false;
    }
    plane.next_WP_loc = plane.prev_WP_loc = plane.current_loc;
    // start or resume the mission, based on MIS_AUTORESET
    plane.mission.start_or_resume();

#if SOARING_ENABLED == ENABLED
    plane.g2.soaring_controller.init_cruising();
#endif

    return true;
}

void ModeAuto::_exit()
{
    if (plane.mission.state() == AP_Mission::MISSION_RUNNING) {
        plane.mission.stop();

        if (plane.mission.get_current_nav_cmd().id == MAV_CMD_NAV_LAND &&
            !plane.quadplane.is_vtol_land(plane.mission.get_current_nav_cmd().id))
        {
            plane.landing.restart_landing_sequence();
        }
    }
    plane.auto_state.started_flying_in_auto_ms = 0;
}

void ModeAuto::update()
{
    if (plane.mission.state() != AP_Mission::MISSION_RUNNING) {
        // this could happen if AP_Landing::restart_landing_sequence() returns false which would only happen if:
        // restart_landing_sequence() is called when not executing a NAV_LAND or there is no previous nav point
        plane.set_mode(plane.mode_rtl, MODE_REASON_MISSION_END);
        gcs().send_text(MAV_SEVERITY_INFO, "Aircraft in auto without a running mission");
        return;
    }

    uint16_t nav_cmd_id = plane.mission.get_current_nav_cmd().id;

    if (plane.quadplane.in_vtol_auto()) {
        plane.quadplane.control_auto(plane.next_WP_loc);
    } else if (nav_cmd_id == MAV_CMD_NAV_TAKEOFF ||
        (nav_cmd_id == MAV_CMD_NAV_LAND && plane.flight_stage == AP_Vehicle::FixedWing::FLIGHT_ABORT_LAND)) {
        plane.takeoff_calc_roll();
        plane.takeoff_calc_pitch();
        plane.calc_throttle();
    } else if (nav_cmd_id == MAV_CMD_NAV_LAND) {
        plane.calc_nav_roll();
        plane.calc_nav_pitch();

        // allow landing to restrict the roll limits
        plane.nav_roll_cd = plane.landing.constrain_roll(plane.nav_roll_cd, plane.g.level_roll_limit*100UL);

        if (plane.landing.is_throttle_suppressed()) {
            // if landing is considered complete throttle is never allowed, regardless of landing type
            SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, 0);
        } else {
            plane.calc_throttle();
        }
    } else {
        // we are doing normal AUTO flight, the special cases
        // are for takeoff and landing
        if (nav_cmd_id != MAV_CMD_NAV_CONTINUE_AND_CHANGE_ALT) {
            plane.steer_state.hold_course_cd = -1;
        }
        plane.calc_nav_roll();
        plane.calc_nav_pitch();
        plane.calc_throttle();
    }
}