mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-24 15:40:31 +08:00
mc_pos_control: AUTO implemented, fixes
This commit is contained in:
@@ -319,11 +319,11 @@ private:
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/**
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* Control position.
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*/
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bool control_position(const math::Vector2f &global_pos, const math::Vector2f &ground_speed,
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bool control_position(const math::Vector<2> &global_pos, const math::Vector<2> &ground_speed,
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const struct mission_item_triplet_s &_mission_item_triplet);
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float calculate_target_airspeed(float airspeed_demand);
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void calculate_gndspeed_undershoot(const math::Vector2f ¤t_position, const math::Vector2f &ground_speed, const struct mission_item_triplet_s &mission_item_triplet);
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void calculate_gndspeed_undershoot(const math::Vector<2> ¤t_position, const math::Vector<2> &ground_speed, const struct mission_item_triplet_s &mission_item_triplet);
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/**
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* Shim for calling task_main from task_create.
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@@ -680,13 +680,13 @@ FixedwingPositionControl::calculate_target_airspeed(float airspeed_demand)
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}
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void
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FixedwingPositionControl::calculate_gndspeed_undershoot(const math::Vector2f ¤t_position, const math::Vector2f &ground_speed, const struct mission_item_triplet_s &mission_item_triplet)
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FixedwingPositionControl::calculate_gndspeed_undershoot(const math::Vector<2> ¤t_position, const math::Vector<2> &ground_speed, const struct mission_item_triplet_s &mission_item_triplet)
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{
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if (_global_pos_valid) {
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/* rotate ground speed vector with current attitude */
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math::Vector2f yaw_vector(_R_nb(0, 0), _R_nb(1, 0));
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math::Vector<2> yaw_vector(_R_nb(0, 0), _R_nb(1, 0));
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yaw_vector.normalize();
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float ground_speed_body = yaw_vector * ground_speed;
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@@ -697,7 +697,7 @@ FixedwingPositionControl::calculate_gndspeed_undershoot(const math::Vector2f &cu
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distance = get_distance_to_next_waypoint(mission_item_triplet.previous.lat, mission_item_triplet.previous.lon, mission_item_triplet.current.lat, mission_item_triplet.current.lon);
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delta_altitude = mission_item_triplet.current.altitude - mission_item_triplet.previous.altitude;
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} else {
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distance = get_distance_to_next_waypoint(current_position.getX(), current_position.getY(), mission_item_triplet.current.lat, mission_item_triplet.current.lon);
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distance = get_distance_to_next_waypoint(current_position(0), current_position(1), mission_item_triplet.current.lat, mission_item_triplet.current.lon);
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delta_altitude = mission_item_triplet.current.altitude - _global_pos.alt;
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}
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@@ -730,7 +730,7 @@ void FixedwingPositionControl::navigation_capabilities_publish()
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}
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bool
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FixedwingPositionControl::control_position(const math::Vector2f ¤t_position, const math::Vector2f &ground_speed,
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FixedwingPositionControl::control_position(const math::Vector<2> ¤t_position, const math::Vector<2> &ground_speed,
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const struct mission_item_triplet_s &mission_item_triplet)
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{
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bool setpoint = true;
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@@ -765,26 +765,26 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio
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_tecs.set_speed_weight(_parameters.speed_weight);
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/* current waypoint (the one currently heading for) */
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math::Vector2f next_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon);
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math::Vector<2> next_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon);
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/* current waypoint (the one currently heading for) */
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math::Vector2f curr_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon);
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math::Vector<2> curr_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon);
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/* previous waypoint */
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math::Vector2f prev_wp;
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math::Vector<2> prev_wp;
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if (mission_item_triplet.previous_valid) {
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prev_wp.setX(mission_item_triplet.previous.lat);
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prev_wp.setY(mission_item_triplet.previous.lon);
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prev_wp(0) = mission_item_triplet.previous.lat;
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prev_wp(1) = mission_item_triplet.previous.lon;
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} else {
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/*
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* No valid previous waypoint, go for the current wp.
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* This is automatically handled by the L1 library.
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*/
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prev_wp.setX(mission_item_triplet.current.lat);
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prev_wp.setY(mission_item_triplet.current.lon);
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prev_wp(0) = mission_item_triplet.current.lat;
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prev_wp(1) = mission_item_triplet.current.lon;
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}
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@@ -820,7 +820,7 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio
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/* Horizontal landing control */
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/* switch to heading hold for the last meters, continue heading hold after */
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float wp_distance = get_distance_to_next_waypoint(current_position.getX(), current_position.getY(), curr_wp.getX(), curr_wp.getY());
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float wp_distance = get_distance_to_next_waypoint(current_position(0), current_position(1), curr_wp(0), curr_wp(1));
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//warnx("wp dist: %d, alt err: %d, noret: %s", (int)wp_distance, (int)altitude_error, (land_noreturn) ? "YES" : "NO");
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const float heading_hold_distance = 15.0f;
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if (wp_distance < heading_hold_distance || land_noreturn_horizontal) {
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@@ -829,7 +829,7 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio
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// if (mission_item_triplet.previous_valid) {
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// target_bearing = get_bearing_to_next_waypoint(prev_wp.getX(), prev_wp.getY(), next_wp.getX(), next_wp.getY());
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// target_bearing = get_bearing_to_next_waypoint(prev_wp(0), prev_wp(1), next_wp(0), next_wp(1));
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// } else {
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if (!land_noreturn_horizontal) //set target_bearing in first occurrence
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@@ -870,7 +870,7 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio
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float airspeed_land = 1.3f * _parameters.airspeed_min;
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float airspeed_approach = 1.3f * _parameters.airspeed_min;
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float L_wp_distance = get_distance_to_next_waypoint(prev_wp.getX(), prev_wp.getY(), curr_wp.getX(), curr_wp.getY()) * _parameters.land_slope_length;
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float L_wp_distance = get_distance_to_next_waypoint(prev_wp(0), prev_wp(1), curr_wp(0), curr_wp(1)) * _parameters.land_slope_length;
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float L_altitude = landingslope.getLandingSlopeAbsoluteAltitude(L_wp_distance, _mission_item_triplet.current.altitude);//getLandingSlopeAbsoluteAltitude(L_wp_distance, _mission_item_triplet.current.altitude, landing_slope_angle_rad, horizontal_slope_displacement);
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float landing_slope_alt_desired = landingslope.getLandingSlopeAbsoluteAltitude(wp_distance, _mission_item_triplet.current.altitude);//getLandingSlopeAbsoluteAltitude(wp_distance, _mission_item_triplet.current.altitude, landing_slope_angle_rad, horizontal_slope_displacement);
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@@ -989,8 +989,8 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio
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// warnx("nav bearing: %8.4f bearing err: %8.4f target bearing: %8.4f", (double)_l1_control.nav_bearing(),
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// (double)_l1_control.bearing_error(), (double)_l1_control.target_bearing());
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// warnx("prev wp: %8.4f/%8.4f, next wp: %8.4f/%8.4f prev:%s", (double)prev_wp.getX(), (double)prev_wp.getY(),
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// (double)next_wp.getX(), (double)next_wp.getY(), (mission_item_triplet.previous_valid) ? "valid" : "invalid");
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// warnx("prev wp: %8.4f/%8.4f, next wp: %8.4f/%8.4f prev:%s", (double)prev_wp(0), (double)prev_wp(1),
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// (double)next_wp(0), (double)next_wp(1), (mission_item_triplet.previous_valid) ? "valid" : "invalid");
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// XXX at this point we always want no loiter hold if a
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// mission is active
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@@ -61,7 +61,7 @@
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#include <uORB/topics/parameter_update.h>
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#include <uORB/topics/vehicle_local_position.h>
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#include <uORB/topics/vehicle_local_position_setpoint.h>
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#include <uORB/topics/vehicle_global_position_setpoint.h>
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#include <uORB/topics/mission_item_triplet.h>
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#include <uORB/topics/vehicle_global_velocity_setpoint.h>
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#include <systemlib/param/param.h>
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#include <systemlib/err.h>
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@@ -113,7 +113,7 @@ private:
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int _manual_sub; /**< notification of manual control updates */
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int _arming_sub; /**< arming status of outputs */
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int _local_pos_sub; /**< vehicle local position */
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int _global_pos_sp_sub; /**< vehicle global position setpoint */
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int _mission_items_sub; /**< mission item triplet */
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orb_advert_t _local_pos_sp_pub; /**< local position setpoint publication */
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orb_advert_t _att_sp_pub; /**< attitude setpoint publication */
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@@ -126,7 +126,7 @@ private:
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struct actuator_armed_s _arming; /**< actuator arming status */
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struct vehicle_local_position_s _local_pos; /**< vehicle local position */
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struct vehicle_local_position_setpoint_s _local_pos_sp; /**< vehicle local position */
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struct vehicle_global_position_setpoint_s _global_pos_sp; /**< vehicle global position setpoint */
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struct mission_item_triplet_s _mission_items; /**< vehicle global position setpoint */
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struct vehicle_global_velocity_setpoint_s _global_vel_sp; /**< vehicle global velocity setpoint */
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struct {
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@@ -232,7 +232,7 @@ MulticopterPositionControl::MulticopterPositionControl() :
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_manual_sub(-1),
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_arming_sub(-1),
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_local_pos_sub(-1),
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_global_pos_sp_sub(-1),
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_mission_items_sub(-1),
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/* publications */
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_local_pos_sp_pub(-1),
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@@ -246,7 +246,7 @@ MulticopterPositionControl::MulticopterPositionControl() :
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memset(&_arming, 0, sizeof(_arming));
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memset(&_local_pos, 0, sizeof(_local_pos));
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memset(&_local_pos_sp, 0, sizeof(_local_pos_sp));
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memset(&_global_pos_sp, 0, sizeof(_global_pos_sp));
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memset(&_mission_items, 0, sizeof(_mission_items));
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memset(&_global_vel_sp, 0, sizeof(_global_vel_sp));
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_params.pos_p.zero();
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@@ -395,9 +395,9 @@ MulticopterPositionControl::poll_subscriptions()
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if (updated)
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orb_copy(ORB_ID(actuator_armed), _arming_sub, &_arming);
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orb_check(_global_pos_sp_sub, &updated);
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orb_check(_mission_items_sub, &updated);
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if (updated)
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orb_copy(ORB_ID(vehicle_global_position_setpoint), _global_pos_sp_sub, &_global_pos_sp);
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orb_copy(ORB_ID(mission_item_triplet), _mission_items_sub, &_mission_items);
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}
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float
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@@ -439,7 +439,7 @@ MulticopterPositionControl::task_main()
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_manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
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_arming_sub = orb_subscribe(ORB_ID(actuator_armed));
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_local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
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_global_pos_sp_sub = orb_subscribe(ORB_ID(vehicle_global_position_setpoint));
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_mission_items_sub = orb_subscribe(ORB_ID(mission_item_triplet));
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parameters_update(true);
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@@ -449,8 +449,6 @@ MulticopterPositionControl::task_main()
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/* get an initial update for all sensor and status data */
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poll_subscriptions();
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bool reset_mission_sp = false;
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bool global_pos_sp_valid = false;
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bool reset_man_sp_z = true;
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bool reset_man_sp_xy = true;
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bool reset_int_z = true;
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@@ -466,9 +464,10 @@ MulticopterPositionControl::task_main()
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const float alt_ctl_dz = 0.2f;
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const float pos_ctl_dz = 0.05f;
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hrt_abstime ref_timestamp = 0;
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int32_t ref_lat = 0.0f;
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int32_t ref_lon = 0.0f;
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float ref_alt = 0.0f;
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hrt_abstime ref_alt_t = 0;
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hrt_abstime local_ref_timestamp = 0;
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math::Vector<3> sp_move_rate;
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sp_move_rate.zero();
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@@ -533,22 +532,32 @@ MulticopterPositionControl::task_main()
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sp_move_rate.zero();
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if (_local_pos.ref_timestamp != ref_timestamp) {
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/* initialize local projection with new reference */
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double lat_home = _local_pos.ref_lat * 1e-7;
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double lon_home = _local_pos.ref_lon * 1e-7;
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map_projection_init(lat_home, lon_home);
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mavlink_log_info(mavlink_fd, "[mpc] local pos ref: %.7f, %.7f", (double)lat_home, (double)lon_home);
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if (_control_mode.flag_control_manual_enabled && ref_timestamp != 0) {
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/* correct setpoint in manual mode to stay in the same point */
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float ref_change_x = 0.0f;
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float ref_change_y = 0.0f;
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map_projection_project(ref_lat, ref_lon, &ref_change_x, &ref_change_y);
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_pos_sp(0) += ref_change_x;
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_pos_sp(1) += ref_change_y;
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_pos_sp(2) += _local_pos.ref_alt - ref_alt;
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}
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ref_timestamp = _local_pos.ref_timestamp;
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ref_lat = _local_pos.ref_lat;
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ref_lon = _local_pos.ref_lon;
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ref_alt = _local_pos.ref_alt;
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}
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if (_control_mode.flag_control_manual_enabled) {
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/* manual control */
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/* check for reference point updates and correct setpoint */
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if (_local_pos.ref_timestamp != ref_alt_t) {
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if (ref_alt_t != 0) {
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/* home alt changed, don't follow large ground level changes in manual flight */
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_pos_sp(2) += _local_pos.ref_alt - ref_alt;
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}
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ref_alt_t = _local_pos.ref_timestamp;
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ref_alt = _local_pos.ref_alt;
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// TODO also correct XY setpoint
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}
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/* reset setpoints to current position if needed */
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if (_control_mode.flag_control_altitude_enabled) {
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/* reset setpoint Z to current altitude if needed */
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if (reset_man_sp_z) {
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reset_man_sp_z = false;
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_pos_sp(2) = _pos(2);
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@@ -560,6 +569,7 @@ MulticopterPositionControl::task_main()
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}
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if (_control_mode.flag_control_position_enabled) {
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/* reset setpoint XY to current position if needed */
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if (reset_man_sp_xy) {
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reset_man_sp_xy = false;
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_pos_sp(0) = _pos(0);
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@@ -594,21 +604,39 @@ MulticopterPositionControl::task_main()
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_pos_sp = _pos + pos_sp_offs.emult(_params.vel_max);
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}
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/* copy yaw setpoint to vehicle_local_position_setpoint topic */
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_local_pos_sp.yaw = _att_sp.yaw_body;
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/* local position setpoint is valid and can be used for auto loiter after position controlled mode */
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reset_auto_sp_xy = !_control_mode.flag_control_position_enabled;
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reset_auto_sp_z = !_control_mode.flag_control_altitude_enabled;
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reset_takeoff_sp = true;
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/* force reprojection of global setpoint after manual mode */
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reset_mission_sp = true;
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} else {
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// TODO AUTO
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_pos_sp = _pos;
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/* AUTO */
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if (_mission_items.current_valid) {
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struct mission_item_s item = _mission_items.current;
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map_projection_project(item.lat, item.lon, &_pos_sp(0), &_pos_sp(1));
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// TODO home altitude can be != ref_alt, check home_position topic
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_pos_sp(2) = -(item.altitude_is_relative ? item.altitude : item.altitude - ref_alt);
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/* in case of interrupted mission don't go to waypoint but stop */
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reset_auto_sp_xy = true;
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reset_auto_sp_z = true;
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} else {
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/* no waypoint, loiter, reset position setpoint if needed */
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if (reset_auto_sp_xy) {
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reset_auto_sp_xy = false;
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_pos_sp(0) = _pos(0);
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_pos_sp(1) = _pos(1);
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}
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if (reset_auto_sp_z) {
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reset_auto_sp_z = false;
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_pos_sp(2) = _pos(2);
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}
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}
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}
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/* copy resulting setpoint to vehicle_local_position_setpoint topic for logging */
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_local_pos_sp.yaw = _att_sp.yaw_body;
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_local_pos_sp.x = _pos_sp(0);
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_local_pos_sp.y = _pos_sp(1);
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_local_pos_sp.z = _pos_sp(2);
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@@ -874,7 +902,6 @@ MulticopterPositionControl::task_main()
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reset_man_sp_xy = true;
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reset_int_z = true;
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reset_int_xy = true;
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reset_mission_sp = true;
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reset_auto_sp_xy = true;
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reset_auto_sp_z = true;
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}
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