2014-06-03 16:01:28 +02:00
|
|
|
/***************************************************************************
|
|
|
|
|
*
|
2017-04-20 11:24:55 -04:00
|
|
|
* Copyright (c) 2013-2017 PX4 Development Team. All rights reserved.
|
2014-06-03 16:01:28 +02:00
|
|
|
*
|
|
|
|
|
* Redistribution and use in source and binary forms, with or without
|
|
|
|
|
* modification, are permitted provided that the following conditions
|
|
|
|
|
* are met:
|
|
|
|
|
*
|
|
|
|
|
* 1. Redistributions of source code must retain the above copyright
|
|
|
|
|
* notice, this list of conditions and the following disclaimer.
|
|
|
|
|
* 2. Redistributions in binary form must reproduce the above copyright
|
|
|
|
|
* notice, this list of conditions and the following disclaimer in
|
|
|
|
|
* the documentation and/or other materials provided with the
|
|
|
|
|
* distribution.
|
|
|
|
|
* 3. Neither the name PX4 nor the names of its contributors may be
|
|
|
|
|
* used to endorse or promote products derived from this software
|
|
|
|
|
* without specific prior written permission.
|
|
|
|
|
*
|
|
|
|
|
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
|
|
|
|
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
|
|
|
|
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
|
|
|
|
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
|
|
|
|
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
|
|
|
|
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
|
|
|
|
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
|
|
|
|
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
|
|
|
|
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
|
|
|
|
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
|
|
|
|
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
|
|
|
|
* POSSIBILITY OF SUCH DAMAGE.
|
|
|
|
|
*
|
|
|
|
|
****************************************************************************/
|
|
|
|
|
/**
|
|
|
|
|
* @file navigator.h
|
|
|
|
|
* Helper class to access missions
|
|
|
|
|
* @author Julian Oes <julian@oes.ch>
|
|
|
|
|
* @author Anton Babushkin <anton.babushkin@me.com>
|
2014-07-19 20:03:37 +02:00
|
|
|
* @author Thomas Gubler <thomasgubler@gmail.com>
|
2014-06-03 16:01:28 +02:00
|
|
|
*/
|
|
|
|
|
|
|
|
|
|
#ifndef NAVIGATOR_H
|
|
|
|
|
#define NAVIGATOR_H
|
|
|
|
|
|
2017-04-20 11:24:55 -04:00
|
|
|
#include "datalinkloss.h"
|
|
|
|
|
#include "enginefailure.h"
|
|
|
|
|
#include "follow_target.h"
|
|
|
|
|
#include "geofence.h"
|
|
|
|
|
#include "gpsfailure.h"
|
|
|
|
|
#include "land.h"
|
|
|
|
|
#include "loiter.h"
|
|
|
|
|
#include "mission.h"
|
|
|
|
|
#include "navigator_mode.h"
|
|
|
|
|
#include "rcloss.h"
|
|
|
|
|
#include "rtl.h"
|
|
|
|
|
#include "takeoff.h"
|
2014-06-03 16:01:28 +02:00
|
|
|
|
2014-06-06 18:13:45 +02:00
|
|
|
#include <controllib/block/BlockParam.hpp>
|
2017-04-20 11:24:55 -04:00
|
|
|
#include <controllib/blocks.hpp>
|
2015-08-20 11:07:40 +02:00
|
|
|
#include <navigator/navigation.h>
|
2017-04-20 11:24:55 -04:00
|
|
|
#include <systemlib/perf_counter.h>
|
|
|
|
|
#include <uORB/topics/fw_pos_ctrl_status.h>
|
|
|
|
|
#include <uORB/topics/geofence_result.h>
|
2014-06-03 16:01:28 +02:00
|
|
|
#include <uORB/topics/mission.h>
|
2017-04-20 11:24:55 -04:00
|
|
|
#include <uORB/topics/mission_result.h>
|
|
|
|
|
#include <uORB/topics/parameter_update.h>
|
2014-06-03 16:01:28 +02:00
|
|
|
#include <uORB/topics/position_setpoint_triplet.h>
|
2017-04-20 11:24:55 -04:00
|
|
|
#include <uORB/topics/vehicle_attitude_setpoint.h>
|
2014-06-03 16:01:28 +02:00
|
|
|
#include <uORB/topics/vehicle_global_position.h>
|
2014-08-24 11:14:15 +02:00
|
|
|
#include <uORB/topics/vehicle_gps_position.h>
|
2016-02-25 17:00:39 +00:00
|
|
|
#include <uORB/topics/vehicle_land_detected.h>
|
2017-04-20 11:24:55 -04:00
|
|
|
#include <uORB/uORB.h>
|
2014-06-03 16:01:28 +02:00
|
|
|
|
2014-06-12 16:33:15 -07:00
|
|
|
/**
|
|
|
|
|
* Number of navigation modes that need on_active/on_inactive calls
|
|
|
|
|
*/
|
2016-03-09 15:31:50 -08:00
|
|
|
#define NAVIGATOR_MODE_ARRAY_SIZE 10
|
2014-06-12 16:22:04 -07:00
|
|
|
|
2014-06-06 18:13:45 +02:00
|
|
|
class Navigator : public control::SuperBlock
|
2014-06-03 16:01:28 +02:00
|
|
|
{
|
|
|
|
|
public:
|
|
|
|
|
Navigator();
|
|
|
|
|
~Navigator();
|
2017-04-20 11:24:55 -04:00
|
|
|
Navigator(const Navigator &) = delete;
|
|
|
|
|
Navigator operator=(const Navigator &) = delete;
|
2014-06-03 16:01:28 +02:00
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Start the navigator task.
|
|
|
|
|
*
|
|
|
|
|
* @return OK on success.
|
|
|
|
|
*/
|
2017-08-01 18:59:12 -04:00
|
|
|
int start();
|
2014-06-03 16:01:28 +02:00
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Display the navigator status.
|
|
|
|
|
*/
|
|
|
|
|
void status();
|
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Load fence from file
|
|
|
|
|
*/
|
|
|
|
|
void load_fence_from_file(const char *filename);
|
|
|
|
|
|
2014-12-19 22:26:31 +00:00
|
|
|
/**
|
|
|
|
|
* Publish the geofence result
|
|
|
|
|
*/
|
2016-07-29 20:24:21 -04:00
|
|
|
void publish_geofence_result();
|
2014-12-19 22:26:31 +00:00
|
|
|
|
2014-08-22 00:40:45 +02:00
|
|
|
/**
|
|
|
|
|
* Publish the attitude sp, only to be used in very special modes when position control is deactivated
|
|
|
|
|
* Example: mode that is triggered on gps failure
|
|
|
|
|
*/
|
2016-07-29 20:24:21 -04:00
|
|
|
void publish_att_sp();
|
2014-07-23 22:58:19 +02:00
|
|
|
|
2017-04-20 11:24:55 -04:00
|
|
|
void publish_vehicle_cmd(const struct vehicle_command_s &vcmd);
|
|
|
|
|
|
2014-06-06 00:55:18 +02:00
|
|
|
/**
|
|
|
|
|
* Setters
|
|
|
|
|
*/
|
2014-06-26 00:17:25 +02:00
|
|
|
void set_can_loiter_at_sp(bool can_loiter) { _can_loiter_at_sp = can_loiter; }
|
2014-06-29 14:09:22 +02:00
|
|
|
void set_position_setpoint_triplet_updated() { _pos_sp_triplet_updated = true; }
|
2014-12-19 23:36:32 +00:00
|
|
|
void set_mission_result_updated() { _mission_result_updated = true; }
|
2014-06-06 00:55:18 +02:00
|
|
|
|
2014-06-04 01:07:50 +02:00
|
|
|
/**
|
|
|
|
|
* Getters
|
|
|
|
|
*/
|
2017-04-20 11:24:55 -04:00
|
|
|
struct fw_pos_ctrl_status_s *get_fw_pos_ctrl_status() { return &_fw_pos_ctrl_status; }
|
2017-02-13 09:42:31 +01:00
|
|
|
struct home_position_s *get_home_position() { return &_home_pos; }
|
2017-04-20 11:24:55 -04:00
|
|
|
struct mission_result_s *get_mission_result() { return &_mission_result; }
|
2017-01-04 17:27:13 -05:00
|
|
|
struct position_setpoint_triplet_s *get_position_setpoint_triplet() { return &_pos_sp_triplet; }
|
|
|
|
|
struct position_setpoint_triplet_s *get_reposition_triplet() { return &_reposition_triplet; }
|
|
|
|
|
struct position_setpoint_triplet_s *get_takeoff_triplet() { return &_takeoff_triplet; }
|
|
|
|
|
struct vehicle_attitude_setpoint_s *get_att_sp() { return &_att_sp; }
|
2017-04-20 11:24:55 -04:00
|
|
|
struct vehicle_global_position_s *get_global_position() { return &_global_pos; }
|
|
|
|
|
struct vehicle_gps_position_s *get_gps_position() { return &_gps_pos; }
|
|
|
|
|
struct vehicle_land_detected_s *get_land_detected() { return &_land_detected; }
|
|
|
|
|
struct vehicle_local_position_s *get_local_position() { return &_local_pos; }
|
|
|
|
|
struct vehicle_status_s *get_vstatus() { return &_vstatus; }
|
|
|
|
|
|
|
|
|
|
bool home_position_valid() { return (_home_pos.timestamp > 0); }
|
2014-07-23 22:58:19 +02:00
|
|
|
|
2014-06-06 00:55:18 +02:00
|
|
|
int get_onboard_mission_sub() { return _onboard_mission_sub; }
|
|
|
|
|
int get_offboard_mission_sub() { return _offboard_mission_sub; }
|
2017-01-04 17:27:13 -05:00
|
|
|
Geofence &get_geofence() { return _geofence; }
|
2014-06-26 00:17:25 +02:00
|
|
|
bool get_can_loiter_at_sp() { return _can_loiter_at_sp; }
|
2014-06-06 20:02:38 +02:00
|
|
|
float get_loiter_radius() { return _param_loiter_radius.get(); }
|
2015-06-05 10:34:17 +02:00
|
|
|
|
2016-03-27 14:09:59 +02:00
|
|
|
/**
|
|
|
|
|
* Returns the default acceptance radius defined by the parameter
|
|
|
|
|
*/
|
2016-07-29 20:24:21 -04:00
|
|
|
float get_default_acceptance_radius();
|
2016-03-27 14:09:59 +02:00
|
|
|
|
2015-06-05 10:34:17 +02:00
|
|
|
/**
|
|
|
|
|
* Get the acceptance radius
|
|
|
|
|
*
|
|
|
|
|
* @return the distance at which the next waypoint should be used
|
|
|
|
|
*/
|
2015-06-05 10:16:51 +02:00
|
|
|
float get_acceptance_radius();
|
2015-06-05 10:34:17 +02:00
|
|
|
|
2016-07-28 22:29:18 +02:00
|
|
|
/**
|
|
|
|
|
* Get the altitude acceptance radius
|
|
|
|
|
*
|
|
|
|
|
* @return the distance from the target altitude before considering the waypoint reached
|
|
|
|
|
*/
|
|
|
|
|
float get_altitude_acceptance_radius();
|
2016-07-28 20:58:48 +02:00
|
|
|
|
2016-01-22 13:29:48 +01:00
|
|
|
/**
|
|
|
|
|
* Get the cruising speed
|
|
|
|
|
*
|
|
|
|
|
* @return the desired cruising speed for this mission
|
|
|
|
|
*/
|
|
|
|
|
float get_cruising_speed();
|
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Set the cruising speed
|
2016-09-19 21:48:10 +02:00
|
|
|
*
|
|
|
|
|
* Passing a negative value or leaving the parameter away will reset the cruising speed
|
|
|
|
|
* to its default value.
|
|
|
|
|
*
|
2017-04-20 11:24:55 -04:00
|
|
|
* For VTOL: sets cruising speed for current mode only (multirotor or fixed-wing).
|
2016-09-19 21:48:10 +02:00
|
|
|
*
|
|
|
|
|
*/
|
2017-01-04 17:27:13 -05:00
|
|
|
void set_cruising_speed(float speed = -1.0f);
|
2016-09-19 21:48:10 +02:00
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Reset cruising speed to default values
|
|
|
|
|
*
|
|
|
|
|
* For VTOL: resets both cruising speeds.
|
2016-01-22 13:29:48 +01:00
|
|
|
*/
|
2016-09-19 21:48:10 +02:00
|
|
|
void reset_cruising_speed();
|
2016-01-22 13:29:48 +01:00
|
|
|
|
2016-06-09 17:15:57 +02:00
|
|
|
/**
|
|
|
|
|
* Get the target throttle
|
|
|
|
|
*
|
|
|
|
|
* @return the desired throttle for this mission
|
|
|
|
|
*/
|
|
|
|
|
float get_cruising_throttle();
|
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Set the target throttle
|
|
|
|
|
*/
|
2017-01-04 17:27:13 -05:00
|
|
|
void set_cruising_throttle(float throttle = -1.0f) { _mission_throttle = throttle; }
|
2016-06-09 17:15:57 +02:00
|
|
|
|
2015-06-05 10:34:17 +02:00
|
|
|
/**
|
|
|
|
|
* Get the acceptance radius given the mission item preset radius
|
|
|
|
|
*
|
|
|
|
|
* @param mission_item_radius the radius to use in case the controller-derived radius is smaller
|
|
|
|
|
*
|
|
|
|
|
* @return the distance at which the next waypoint should be used
|
|
|
|
|
*/
|
|
|
|
|
float get_acceptance_radius(float mission_item_radius);
|
2016-03-15 18:25:02 +00:00
|
|
|
orb_advert_t *get_mavlink_log_pub() { return &_mavlink_log_pub; }
|
2014-06-06 17:17:41 +02:00
|
|
|
|
2015-06-13 17:31:58 +02:00
|
|
|
void increment_mission_instance_count() { _mission_instance_count++; }
|
|
|
|
|
|
2016-02-13 01:08:07 +01:00
|
|
|
void set_mission_failure(const char *reason);
|
2016-03-09 15:31:50 -08:00
|
|
|
|
2016-05-10 10:12:29 +02:00
|
|
|
bool is_planned_mission() { return _navigation_mode == &_mission; }
|
|
|
|
|
|
2016-07-29 20:24:21 -04:00
|
|
|
bool abort_landing();
|
|
|
|
|
|
2014-06-03 16:01:28 +02:00
|
|
|
private:
|
|
|
|
|
|
2017-04-20 11:24:55 -04:00
|
|
|
bool _task_should_exit{false}; /**< if true, sensor task should exit */
|
|
|
|
|
int _navigator_task{-1}; /**< task handle for sensor task */
|
|
|
|
|
|
|
|
|
|
orb_advert_t _mavlink_log_pub{nullptr}; /**< the uORB advert to send messages over mavlink */
|
|
|
|
|
|
|
|
|
|
int _fw_pos_ctrl_status_sub{-1}; /**< notification of vehicle capabilities updates */
|
|
|
|
|
int _global_pos_sub{-1}; /**< global position subscription */
|
|
|
|
|
int _gps_pos_sub{-1}; /**< gps position subscription */
|
|
|
|
|
int _home_pos_sub{-1}; /**< home position subscription */
|
|
|
|
|
int _land_detected_sub{-1}; /**< vehicle land detected subscription */
|
|
|
|
|
int _local_pos_sub{-1}; /**< local position subscription */
|
|
|
|
|
int _offboard_mission_sub{-1}; /**< offboard mission subscription */
|
|
|
|
|
int _onboard_mission_sub{-1}; /**< onboard mission subscription */
|
|
|
|
|
int _param_update_sub{-1}; /**< param update subscription */
|
|
|
|
|
int _sensor_combined_sub{-1}; /**< sensor combined subscription */
|
|
|
|
|
int _vehicle_command_sub{-1}; /**< vehicle commands (onboard and offboard) */
|
|
|
|
|
int _vstatus_sub{-1}; /**< vehicle status subscription */
|
|
|
|
|
|
|
|
|
|
orb_advert_t _att_sp_pub{nullptr};
|
|
|
|
|
orb_advert_t _geofence_result_pub{nullptr};
|
|
|
|
|
orb_advert_t _mission_result_pub{nullptr};
|
|
|
|
|
orb_advert_t _pos_sp_triplet_pub{nullptr};
|
|
|
|
|
orb_advert_t _vehicle_cmd_pub{nullptr};
|
|
|
|
|
|
|
|
|
|
fw_pos_ctrl_status_s _fw_pos_ctrl_status{}; /**< fixed wing navigation capabilities */
|
|
|
|
|
geofence_result_s _geofence_result{};
|
|
|
|
|
home_position_s _home_pos{}; /**< home position for RTL */
|
|
|
|
|
mission_result_s _mission_result{};
|
|
|
|
|
position_setpoint_triplet_s _pos_sp_triplet{}; /**< triplet of position setpoints */
|
|
|
|
|
position_setpoint_triplet_s _reposition_triplet{}; /**< triplet for non-mission direct position command */
|
|
|
|
|
position_setpoint_triplet_s _takeoff_triplet{}; /**< triplet for non-mission direct takeoff command */
|
|
|
|
|
sensor_combined_s _sensor_combined{}; /**< sensor values */
|
|
|
|
|
vehicle_attitude_setpoint_s _att_sp{};
|
|
|
|
|
vehicle_global_position_s _global_pos{}; /**< global vehicle position */
|
|
|
|
|
vehicle_gps_position_s _gps_pos{}; /**< gps position */
|
|
|
|
|
vehicle_land_detected_s _land_detected{}; /**< vehicle land_detected */
|
2017-02-06 16:48:37 +01:00
|
|
|
vehicle_local_position_s _local_pos; /**< local vehicle position */
|
2017-04-20 11:24:55 -04:00
|
|
|
vehicle_status_s _vstatus{}; /**< vehicle status */
|
|
|
|
|
|
|
|
|
|
int _mission_instance_count{-1}; /**< instance count for the current mission */
|
2014-06-03 16:01:28 +02:00
|
|
|
|
|
|
|
|
perf_counter_t _loop_perf; /**< loop performance counter */
|
|
|
|
|
|
|
|
|
|
Geofence _geofence; /**< class that handles the geofence */
|
2017-04-20 11:24:55 -04:00
|
|
|
bool _geofence_violation_warning_sent{false}; /**< prevents spaming to mavlink */
|
2014-06-03 16:01:28 +02:00
|
|
|
|
2017-04-20 11:24:55 -04:00
|
|
|
bool _can_loiter_at_sp{false}; /**< flags if current position SP can be used to loiter */
|
|
|
|
|
bool _pos_sp_triplet_updated{false}; /**< flags if position SP triplet needs to be published */
|
|
|
|
|
bool _pos_sp_triplet_published_invalid_once{false}; /**< flags if position SP triplet has been published once to UORB */
|
|
|
|
|
bool _mission_result_updated{false}; /**< flags if mission result has seen an update */
|
2014-06-03 16:01:28 +02:00
|
|
|
|
2017-04-20 11:24:55 -04:00
|
|
|
NavigatorMode *_navigation_mode{nullptr}; /**< abstract pointer to current navigation mode class */
|
2014-06-03 16:01:28 +02:00
|
|
|
Mission _mission; /**< class that handles the missions */
|
2014-06-06 00:55:18 +02:00
|
|
|
Loiter _loiter; /**< class that handles loiter */
|
2015-11-20 11:14:51 +01:00
|
|
|
Takeoff _takeoff; /**< class for handling takeoff commands */
|
2015-12-17 00:11:50 +01:00
|
|
|
Land _land; /**< class for handling land commands */
|
2014-06-03 16:01:28 +02:00
|
|
|
RTL _rtl; /**< class that handles RTL */
|
2017-04-20 11:24:55 -04:00
|
|
|
RCLoss _rcLoss; /**< class that handles RTL according to OBC rules (rc loss mode) */
|
2014-07-23 23:07:11 +02:00
|
|
|
DataLinkLoss _dataLinkLoss; /**< class that handles the OBC datalink loss mode */
|
2017-04-20 11:24:55 -04:00
|
|
|
EngineFailure _engineFailure; /**< class that handles the engine failure mode (FW only!) */
|
2014-08-20 07:45:01 +02:00
|
|
|
GpsFailure _gpsFailure; /**< class that handles the OBC gpsfailure loss mode */
|
2017-04-20 11:24:55 -04:00
|
|
|
FollowTarget _follow_target;
|
2016-02-18 06:57:01 -08:00
|
|
|
|
2014-06-12 16:22:04 -07:00
|
|
|
NavigatorMode *_navigation_mode_array[NAVIGATOR_MODE_ARRAY_SIZE]; /**< array of navigation modes */
|
2014-06-12 15:50:06 -07:00
|
|
|
|
2014-06-06 18:13:45 +02:00
|
|
|
control::BlockParamFloat _param_loiter_radius; /**< loiter radius for fixedwing */
|
2017-04-21 11:35:34 -04:00
|
|
|
|
2014-06-27 11:09:49 +02:00
|
|
|
control::BlockParamFloat _param_acceptance_radius; /**< acceptance for takeoff */
|
2016-07-28 22:29:18 +02:00
|
|
|
control::BlockParamFloat _param_fw_alt_acceptance_radius; /**< acceptance radius for fixedwing altitude */
|
|
|
|
|
control::BlockParamFloat _param_mc_alt_acceptance_radius; /**< acceptance radius for multicopter altitude */
|
2017-01-04 17:27:13 -05:00
|
|
|
|
2017-04-20 11:24:55 -04:00
|
|
|
float _mission_cruising_speed_mc{-1.0f};
|
|
|
|
|
float _mission_cruising_speed_fw{-1.0f};
|
|
|
|
|
float _mission_throttle{-1.0f};
|
2016-01-22 13:29:48 +01:00
|
|
|
|
2017-04-20 11:24:55 -04:00
|
|
|
// update subscriptions
|
2017-04-16 21:16:47 -04:00
|
|
|
void fw_pos_ctrl_status_update(bool force = false);
|
2014-06-03 16:01:28 +02:00
|
|
|
void global_position_update();
|
2014-08-24 11:14:15 +02:00
|
|
|
void gps_position_update();
|
2017-01-04 17:27:13 -05:00
|
|
|
void home_position_update(bool force = false);
|
2017-04-20 11:24:55 -04:00
|
|
|
void local_position_update();
|
2014-06-06 18:13:45 +02:00
|
|
|
void params_update();
|
2017-04-20 11:24:55 -04:00
|
|
|
void sensor_combined_update();
|
|
|
|
|
void vehicle_land_detected_update();
|
|
|
|
|
void vehicle_status_update();
|
2014-06-06 18:13:45 +02:00
|
|
|
|
2014-06-03 16:01:28 +02:00
|
|
|
/**
|
|
|
|
|
* Shim for calling task_main from task_create.
|
|
|
|
|
*/
|
|
|
|
|
static void task_main_trampoline(int argc, char *argv[]);
|
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Main task.
|
|
|
|
|
*/
|
|
|
|
|
void task_main();
|
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Translate mission item to a position setpoint.
|
|
|
|
|
*/
|
|
|
|
|
void mission_item_to_position_setpoint(const mission_item_s *item, position_setpoint_s *sp);
|
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Publish a new position setpoint triplet for position controllers
|
|
|
|
|
*/
|
|
|
|
|
void publish_position_setpoint_triplet();
|
2014-07-16 09:24:50 +02:00
|
|
|
|
2014-12-19 23:36:32 +00:00
|
|
|
/**
|
|
|
|
|
* Publish the mission result so commander and mavlink know what is going on
|
|
|
|
|
*/
|
|
|
|
|
void publish_mission_result();
|
2014-06-03 16:01:28 +02:00
|
|
|
};
|
|
|
|
|
#endif
|