ardupilot/ArduCopter/control_guided.pde

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

/*
 * control_guided.pde - init and run calls for guided flight mode
 */

#ifndef GUIDED_LOOK_AT_TARGET_MIN_DISTANCE_CM
 # define GUIDED_LOOK_AT_TARGET_MIN_DISTANCE_CM     500     // point nose at target if it is more than 5m away
#endif

static bool guided_pilot_yaw_override_yaw = false;

// guided_init - initialise guided controller
static bool guided_init(bool ignore_checks)
{
    if (GPS_ok() || ignore_checks) {
        // initialise yaw
        set_auto_yaw_mode(get_default_auto_yaw_mode(false));
        // start in position control mode
        guided_pos_control_start();
        return true;
    }else{
        return false;
    }
}


// guided_takeoff_start - initialises waypoint controller to implement take-off
static void guided_takeoff_start(float final_alt)
{
    guided_mode = Guided_TakeOff;
    
    // initialise wpnav destination
    Vector3f target_pos = inertial_nav.get_position();
    target_pos.z = final_alt;
    wp_nav.set_wp_destination(target_pos);

    // initialise yaw
    set_auto_yaw_mode(AUTO_YAW_HOLD);

    // tell motors to do a slow start
    motors.slow_start(true);
}

// initialise guided mode's position controller
void guided_pos_control_start()
{
    // set to position control mode
    guided_mode = Guided_WP;

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

    // initialise wpnav to stopping point at current altitude
    // To-Do: set to current location if disarmed?
    // To-Do: set to stopping point altitude?
    Vector3f stopping_point;
    stopping_point.z = inertial_nav.get_altitude();
    wp_nav.get_wp_stopping_point_xy(stopping_point);
    wp_nav.set_wp_destination(stopping_point);
    guided_pilot_yaw_override_yaw = false;

    // initialise yaw
    set_auto_yaw_mode(get_default_auto_yaw_mode(false));
}

// initialise guided mode's velocity controller
void guided_vel_control_start()
{
    // set guided_mode to velocity controller
    guided_mode = Guided_Velocity;

    // initialize vertical speeds and leash lengths
    pos_control.set_speed_z(-g.pilot_velocity_z_max, g.pilot_velocity_z_max);
    pos_control.set_accel_z(g.pilot_accel_z);

    // initialise velocity controller
    pos_control.init_vel_controller_xyz();
}

// guided_set_destination - sets guided mode's target destination
static void guided_set_destination(const Vector3f& destination)
{
    // ensure we are in position control mode
    if (guided_mode != Guided_WP) {
        guided_pos_control_start();
    }

    wp_nav.set_wp_destination(destination);
}

// guided_set_velocity - sets guided mode's target velocity
static void guided_set_velocity(const Vector3f& velocity)
{
    // check we are in velocity control mode
    if (guided_mode != Guided_Velocity) {
        guided_vel_control_start();
    }

    // set position controller velocity target
    pos_control.set_desired_velocity(velocity);
}

// guided_run - runs the guided controller
// should be called at 100hz or more
static void guided_run()
{
    // if not auto armed set throttle to zero and exit immediately
    if(!ap.auto_armed) {
        // To-Do: reset waypoint controller?
        attitude_control.relax_bf_rate_controller();
        attitude_control.set_yaw_target_to_current_heading();
        attitude_control.set_throttle_out(0, false);
        // To-Do: handle take-offs - these may not only be immediately after auto_armed becomes true
        return;
    }

    // call the correct auto controller
    switch (guided_mode) {

    case Guided_TakeOff:
        // run takeoff controller
        guided_takeoff_run();
        break;

    case Guided_WP:
        // run position controller
        guided_pos_control_run();
        break;

    case Guided_Velocity:
        // run velocity controller
        guided_vel_control_run();
    }
 }

// guided_takeoff_run - takeoff in guided mode
//      called by guided_run at 100hz or more
static void guided_takeoff_run()
{
    // if not auto armed set throttle to zero and exit immediately
    if(!ap.auto_armed) {
        // reset attitude control targets
        attitude_control.relax_bf_rate_controller();
        attitude_control.set_yaw_target_to_current_heading();
        attitude_control.set_throttle_out(0, false);
        // tell motors to do a slow start
        motors.slow_start(true);
        // 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);
    }

    // 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();

    // 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);
}

// guided_pos_control_run - runs the guided position controller
// called from guided_run
static void guided_pos_control_run()
{
    // 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);
    }
}

// guided_vel_control_run - runs the guided velocity controller
// called from guided_run
static void guided_vel_control_run()
{
    // 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);
        }
    }

    // call velocity controller which includes z axis controller
    pos_control.update_vel_controller_xyz();

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