/// -*- 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) { // initialise wpnav targets wp_nav.shift_wp_origin_to_current_pos(); // 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); 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); } }