ardupilot/ArduCopter/control_rtl.pde

/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-

/*
 * control_rtl.pde - init and run calls for RTL flight mode
 *
 * There are two parts to RTL, the high level decision making which controls which state we are in
 * and the lower implementation of the waypoint or landing controllers within those states
 */

// rtl_init - initialise rtl controller
static bool rtl_init(bool ignore_checks)
{
    if (GPS_ok() || ignore_checks) {
        rtl_climb_start();
        return true;
    }else{
        return false;
    }
}

// rtl_run - runs the return-to-launch controller
// should be called at 100hz or more
static void rtl_run()
{
    // check if we need to move to next state
    if (rtl_state_complete) {
        switch (rtl_state) {
        case InitialClimb:
            rtl_return_start();
            break;
        case ReturnHome:
            rtl_loiterathome_start();
            break;
        case LoiterAtHome:
            if (g.rtl_alt_final > 0) {
                rtl_descent_start();
            }else{
                rtl_land_start();
            }
            break;
        case FinalDescent:
            // do nothing
            break;
        case Land:
            // do nothing
            break;
        }
    }

    // call the correct run function
    switch (rtl_state) {

    case InitialClimb:
        rtl_climb_return_descent_run();
        break;

    case ReturnHome:
        rtl_climb_return_descent_run();
        break;

    case LoiterAtHome:
        rtl_loiterathome_run();
        break;

    case FinalDescent:
        rtl_climb_return_descent_run();
        break;

    case Land:
        rtl_land_run();
        break;
    }
}

// rtl_climb_start - initialise climb to RTL altitude
static void rtl_climb_start()
{
    rtl_state = InitialClimb;
    rtl_state_complete = false;

    // get horizontal stopping point
    Vector3f destination;
    wp_nav.get_wp_stopping_point_xy(destination);
    destination.z = get_RTL_alt();

    wp_nav.set_wp_destination(destination);

    // hold current yaw during initial climb
    set_auto_yaw_mode(AUTO_YAW_HOLD);
}

// rtl_return_start - initialise return to home
static void rtl_return_start()
{
    rtl_state = ReturnHome;
    rtl_state_complete = false;

    // initialise original_wp_bearing which is used to point the nose home
    wp_bearing = wp_nav.get_wp_bearing_to_destination();
    original_wp_bearing = wp_bearing;

    // set target to above home
    Vector3f destination = Vector3f(0,0,get_RTL_alt());
    wp_nav.set_wp_destination(destination);

    // initialise yaw to point home (maybe)
    set_auto_yaw_mode(get_default_auto_yaw_mode(true));
}

// rtl_descent_start - initialise descent to final alt
static void rtl_descent_start()
{
    rtl_state = FinalDescent;
    rtl_state_complete = false;

    // set target to above home
    Vector3f destination = Vector3f(0,0,g.rtl_alt_final);
    wp_nav.set_wp_destination(destination);

    // initialise yaw to point home (maybe)
    set_auto_yaw_mode(AUTO_YAW_HOLD);
}

// rtl_climb_return_descent_run - implements the initial climb, return home and descent portions of RTL which all rely on the wp controller
//      called by rtl_run at 100hz or more
static void rtl_climb_return_descent_run()
{
    // if not auto armed set throttle to zero and exit immediately
    if(!ap.auto_armed) {
        // reset attitude control targets
        attitude_control.init_targets();
        attitude_control.set_throttle_out(0, false);
        // To-Do: re-initialise wpnav targets
        return;
    }

    // process pilot's yaw input
    float target_yaw_rate = 0;
    if (!failsafe.radio) {
        // get pilot's desired yaw rate
        target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
        if (target_yaw_rate != 0) {
            set_auto_yaw_mode(AUTO_YAW_HOLD);
        }
    }

    // run waypoint controller
    wp_nav.update_wpnav();

    // call z-axis position controller (wpnav should have already updated it's alt target)
    pos_control.update_z_controller();

    // call attitude controller
    if (auto_yaw_mode == AUTO_YAW_HOLD) {
        // roll & pitch from waypoint controller, yaw rate from pilot
        attitude_control.angleef_rp_rateef_y(wp_nav.get_roll(), wp_nav.get_pitch(), target_yaw_rate);
    }else{
        // roll, pitch from waypoint controller, yaw heading from auto_heading()
        attitude_control.angleef_rpy(wp_nav.get_roll(), wp_nav.get_pitch(), get_auto_heading());
    }

    // check if we've completed this stage of RTL
    rtl_state_complete = wp_nav.reached_wp_destination();

    // re-fetch angle targets for reporting
    const Vector3f angle_target = attitude_control.angle_ef_targets();
    control_roll = angle_target.x;
    control_pitch = angle_target.y;
    control_yaw = angle_target.z;
}

// rtl_return_start - initialise return to home
static void rtl_loiterathome_start()
{
    rtl_state = LoiterAtHome;
    rtl_state_complete = false;
    rtl_loiter_start_time = millis();

    // yaw back to initial take-off heading yaw unless pilot has already overridden yaw
    if(get_default_auto_yaw_mode(true) != AUTO_YAW_HOLD) {
        set_auto_yaw_mode(AUTO_YAW_RESETTOARMEDYAW);
    } else {
        set_auto_yaw_mode(AUTO_YAW_HOLD);
    }
}

// rtl_climb_return_descent_run - implements the initial climb, return home and descent portions of RTL which all rely on the wp controller
//      called by rtl_run at 100hz or more
static void rtl_loiterathome_run()
{
    // if not auto armed set throttle to zero and exit immediately
    if(!ap.auto_armed) {
        // reset attitude control targets
        attitude_control.init_targets();
        attitude_control.set_throttle_out(0, false);
        // To-Do: re-initialise wpnav targets
        return;
    }

    // process pilot's yaw input
    float target_yaw_rate = 0;
    if (!failsafe.radio) {
        // get pilot's desired yaw rate
        target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
        if (target_yaw_rate != 0) {
            set_auto_yaw_mode(AUTO_YAW_HOLD);
        }
    }

    // run waypoint controller
    wp_nav.update_wpnav();

    // call z-axis position controller (wpnav should have already updated it's alt target)
    pos_control.update_z_controller();

    // call attitude controller
    if (auto_yaw_mode == AUTO_YAW_HOLD) {
        // roll & pitch from waypoint controller, yaw rate from pilot
        attitude_control.angleef_rp_rateef_y(wp_nav.get_roll(), wp_nav.get_pitch(), target_yaw_rate);
    }else{
        // roll, pitch from waypoint controller, yaw heading from auto_heading()
        attitude_control.angleef_rpy(wp_nav.get_roll(), wp_nav.get_pitch(), get_auto_heading());
    }

    // check if we've completed this stage of RTL
    // To-Do: add extra check that we've reached the target yaw
    rtl_state_complete = ((millis() - rtl_loiter_start_time) > (uint32_t)g.rtl_loiter_time.get());

    // re-fetch angle targets for reporting
    const Vector3f angle_target = attitude_control.angle_ef_targets();
    control_roll = angle_target.x;
    control_pitch = angle_target.y;
    control_yaw = angle_target.z;
}

// rtl_loiterathome_start - initialise controllers to loiter over home
static void rtl_land_start()
{
    rtl_state = Land;
    rtl_state_complete = false;

    // Set wp navigation target to above home
    wp_nav.set_loiter_target(Vector3f(0,0,0));

    // initialise altitude target to stopping point
    pos_control.set_target_to_stopping_point_z();

    // initialise yaw
    set_auto_yaw_mode(AUTO_YAW_HOLD);
}

// rtl_returnhome_run - return home
//      called by rtl_run at 100hz or more
static void rtl_land_run()
{
    // if not auto armed set throttle to zero and exit immediately
    if(!ap.auto_armed) {
        attitude_control.init_targets();
        attitude_control.set_throttle_out(0, false);
        // set target to current position
        wp_nav.init_loiter_target();
        return;
    }

    // process pilot's yaw input
    float target_yaw_rate = 0;
    if (!failsafe.radio) {
        // get pilot's desired yaw rate
        target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
    }

    // run loiter controller
    wp_nav.update_loiter();

    // call z-axis position controller
    float cmb_rate = get_throttle_land();
    pos_control.set_alt_target_from_climb_rate(cmb_rate, G_Dt);
    pos_control.update_z_controller();

    // roll & pitch from waypoint controller, yaw rate from pilot
    attitude_control.angleef_rp_rateef_y(wp_nav.get_roll(), wp_nav.get_pitch(), target_yaw_rate);

    // check if we've completed this stage of RTL
    rtl_state_complete = ap.land_complete;

    // re-fetch angle targets for reporting
    const Vector3f angle_target = attitude_control.angle_ef_targets();
    control_roll = angle_target.x;
    control_pitch = angle_target.y;
    control_yaw = angle_target.z;
}