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 && !failsafe.radio) {
                rtl_descent_start();
            }else{
                rtl_land_start();
            }
            break;
        case FinalDescent:
            // do nothing
            break;
        case Land:
            // do nothing - rtl_land_run will take care of disarming motors
            break;
        }
    }

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

    case InitialClimb:
        rtl_climb_return_run();
        break;

    case ReturnHome:
        rtl_climb_return_run();
        break;

    case LoiterAtHome:
        rtl_loiterathome_run();
        break;

    case FinalDescent:
        rtl_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;

    // initialise waypoint and spline controller
    wp_nav.wp_and_spline_init();

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

#if AC_RALLY == ENABLED
    // rally_point.alt will be max of RTL_ALT and the height of the nearest rally point (if there is one)
    Location rally_point = rally.calc_best_rally_or_home_location(current_loc, get_RTL_alt());
    destination.z = rally_point.alt;
#else
    destination.z = get_RTL_alt();
#endif

    // set the destination
    wp_nav.set_wp_destination(destination);
    wp_nav.set_fast_waypoint(true);

    // 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;

    // set target to above home/rally point
#if AC_RALLY == ENABLED
    Vector3f destination = pv_location_to_vector(rally.calc_best_rally_or_home_location(current_loc, get_RTL_alt()));
#else
    Vector3f destination = Vector3f(0,0,get_RTL_alt());
#endif

    wp_nav.set_wp_destination(destination);

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

// rtl_climb_return_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_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.angle_ef_roll_pitch_rate_ef_yaw(wp_nav.get_roll(), wp_nav.get_pitch(), target_yaw_rate);
    }else{
        // roll, pitch from waypoint controller, yaw heading from auto_heading()
        attitude_control.angle_ef_roll_pitch_yaw(wp_nav.get_roll(), wp_nav.get_pitch(), get_auto_heading(),true);
    }

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

// 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.angle_ef_roll_pitch_rate_ef_yaw(wp_nav.get_roll(), wp_nav.get_pitch(), target_yaw_rate);
    }else{
        // roll, pitch from waypoint controller, yaw heading from auto_heading()
        attitude_control.angle_ef_roll_pitch_yaw(wp_nav.get_roll(), wp_nav.get_pitch(), get_auto_heading(),true);
    }

    // check if we've completed this stage of RTL
    if ((millis() - rtl_loiter_start_time) >= (uint32_t)g.rtl_loiter_time.get()) {
        if (auto_yaw_mode == AUTO_YAW_RESETTOARMEDYAW) {
            // check if heading is within 2 degrees of heading when vehicle was armed
            if (labs(wrap_180_cd(ahrs.yaw_sensor-initial_armed_bearing)) <= 200) {
                rtl_state_complete = true;
            }
        } else {
            // we have loitered long enough
            rtl_state_complete = true;
        }
    }
}

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

    // Set wp navigation target to above home
    wp_nav.init_loiter_target(wp_nav.get_wp_destination());

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

    // initialise yaw
    set_auto_yaw_mode(AUTO_YAW_HOLD);
}

// rtl_descent_run - implements the final descent to the RTL_ALT
//      called by rtl_run at 100hz or more
static void rtl_descent_run()
{
    // if not auto armed set throttle to zero and exit immediately
    if(!ap.auto_armed || !inertial_nav.position_ok()) {
        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 input
    float target_yaw_rate = 0;
    if (!failsafe.radio) {
        // apply SIMPLE mode transform to pilot inputs
        update_simple_mode();

        // process pilot's roll and pitch input
        wp_nav.set_pilot_desired_acceleration(g.rc_1.control_in, g.rc_2.control_in);

        // get pilot's desired yaw rate
        target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
    } else {
        // clear out pilot desired acceleration in case radio failsafe event occurs while descending
        wp_nav.clear_pilot_desired_acceleration();
    }

    // run loiter controller
    wp_nav.update_loiter();

    // call z-axis position controller
    pos_control.set_alt_target_with_slew(g.rtl_alt_final, G_Dt);
    pos_control.update_z_controller();

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

    // check if we've reached within 20cm of final altitude
    rtl_state_complete = fabs(g.rtl_alt_final - inertial_nav.get_altitude()) < 20.0f;
}

// 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.init_loiter_target(wp_nav.get_wp_destination());

    // 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 || !inertial_nav.position_ok()) {
        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) {
        // apply SIMPLE mode transform to pilot inputs
        update_simple_mode();

        // process pilot's roll and pitch input
        wp_nav.set_pilot_desired_acceleration(g.rc_1.control_in, g.rc_2.control_in);

        // get pilot's desired yaw rate
        target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
    } else {
        // clear out pilot desired acceleration in case radio failsafe event occurs while landing
        wp_nav.clear_pilot_desired_acceleration();
    }

    // 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.angle_ef_roll_pitch_rate_ef_yaw(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;

#if LAND_REQUIRE_MIN_THROTTLE_TO_DISARM == ENABLED
    // disarm when the landing detector says we've landed and throttle is at minimum
    if (ap.land_complete && (g.rc_3.control_in == 0 || failsafe.radio)) {
        init_disarm_motors();
    }
#else
    // disarm when the landing detector says we've landed
    if (ap.land_complete) {
        init_disarm_motors();
    }
#endif
}

// get_RTL_alt - return altitude which vehicle should return home at
//      altitude is in cm above home
static float get_RTL_alt()
{
    // maximum of current altitude and rtl altitude
    float rtl_alt = max(current_loc.alt, g.rtl_altitude);

#if AC_FENCE == ENABLED
    // ensure not above fence altitude if alt fence is enabled
    if ((fence.get_enabled_fences() & AC_FENCE_TYPE_ALT_MAX) != 0) {
        rtl_alt = min(rtl_alt, fence.get_safe_alt()*100.0f);
    }
#endif

    return rtl_alt;
}