/// -*- 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 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 to hold at current heading (reset to point at waypoint in guided_set_destination) set_auto_yaw_mode(AUTO_YAW_HOLD); return true; }else{ return false; } } // guided_set_destination - sets guided mode's target destination static void guided_set_destination(const Vector3f& destination) { if (control_mode == GUIDED) { wp_nav.set_wp_destination(destination); if (!guided_pilot_yaw_override_yaw) { // get default yaw mode set_auto_yaw_mode(get_default_auto_yaw_mode(false)); // point nose at next waypoint if it is more than 10m away if (auto_yaw_mode == AUTO_YAW_LOOK_AT_NEXT_WP) { // get distance to new location wp_distance = wp_nav.get_wp_distance_to_destination(); // set original_wp_bearing to point at next waypoint if (wp_distance >= GUIDED_LOOK_AT_TARGET_MIN_DISTANCE_CM) { original_wp_bearing = wp_bearing; } } } } } // 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.init_targets(); attitude_control.set_throttle_out(0, false); // To-Do: handle take-offs - these may not only be immediately after auto_armed becomes 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); 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(),true); } // 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; }