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PX4-Autopilot/src/modules/navigator/navigation.h
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2017-01-17 03:14:26 -08:00

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/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
*
* 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 navigation.h
* Definition of a mission consisting of mission items.
* @author Thomas Gubler <thomasgubler@student.ethz.ch>
* @author Julian Oes <joes@student.ethz.ch>
* @author Lorenz Meier <lm@inf.ethz.ch>
*/
#ifndef NAVIGATION_H_
#define NAVIGATION_H_
#include <stdint.h>
#include <stdbool.h>
#if defined(MEMORY_CONSTRAINED_SYSTEM)
# define NUM_MISSIONS_SUPPORTED 50
#else
# define NUM_MISSIONS_SUPPORTED 256
#endif
#define NAV_EPSILON_POSITION 0.001f /**< Anything smaller than this is considered zero */
/* compatible to mavlink MAV_CMD */
enum NAV_CMD {
NAV_CMD_IDLE = 0,
NAV_CMD_WAYPOINT = 16,
NAV_CMD_LOITER_UNLIMITED = 17,
NAV_CMD_LOITER_TIME_LIMIT = 19,
NAV_CMD_RETURN_TO_LAUNCH = 20,
NAV_CMD_LAND = 21,
NAV_CMD_TAKEOFF = 22,
NAV_CMD_LOITER_TO_ALT = 31,
NAV_CMD_DO_FOLLOW_REPOSITION = 33,
NAV_CMD_ROI = 80,
NAV_CMD_VTOL_TAKEOFF = 84,
NAV_CMD_VTOL_LAND = 85,
NAV_CMD_DO_JUMP = 177,
NAV_CMD_DO_CHANGE_SPEED = 178,
NAV_CMD_DO_SET_SERVO = 183,
NAV_CMD_DO_LAND_START = 189,
NAV_CMD_DO_SET_ROI = 201,
NAV_CMD_DO_DIGICAM_CONTROL = 203,
NAV_CMD_DO_MOUNT_CONFIGURE = 204,
NAV_CMD_DO_MOUNT_CONTROL = 205,
NAV_CMD_DO_SET_CAM_TRIGG_DIST = 206,
NAV_CMD_IMAGE_START_CAPTURE = 2000,
NAV_CMD_IMAGE_STOP_CAPTURE = 2001,
NAV_CMD_VIDEO_START_CAPTURE = 2500,
NAV_CMD_VIDEO_STOP_CAPTURE = 2501,
NAV_CMD_DO_VTOL_TRANSITION = 3000,
NAV_CMD_INVALID = UINT16_MAX /* ensure that casting a large number results in a specific error */
};
enum ORIGIN {
ORIGIN_MAVLINK = 0,
ORIGIN_ONBOARD
};
/**
* @addtogroup topics
* @{
*/
/**
* Global position setpoint in WGS84 coordinates.
*
* This is the position the MAV is heading towards. If it of type loiter,
* the MAV is circling around it with the given loiter radius in meters.
*/
#pragma pack(push, 1)
struct mission_item_s {
double lat; /**< latitude in degrees */
double lon; /**< longitude in degrees */
union {
struct {
union {
float time_inside; /**< time that the MAV should stay inside the radius before advancing in seconds */
float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */
};
float acceptance_radius; /**< default radius in which the mission is accepted as reached in meters */
float loiter_radius; /**< loiter radius in meters, 0 for a VTOL to hover, negative for counter-clockwise */
float yaw; /**< in radians NED -PI..+PI, NAN means don't change yaw */
float ___lat_float; /**< padding */
float ___lon_float; /**< padding */
float altitude; /**< altitude in meters (AMSL) */
};
float params[7]; /**< array to store mission command values for MAV_FRAME_MISSION ***/
};
uint16_t nav_cmd; /**< navigation command */
int16_t do_jump_mission_index; /**< index where the do jump will go to */
uint16_t do_jump_repeat_count; /**< how many times do jump needs to be done */
uint16_t do_jump_current_count; /**< count how many times the jump has been done */
struct {
uint16_t frame : 4, /**< mission frame ***/
origin : 3, /**< how the mission item was generated */
loiter_exit_xtrack : 1, /**< exit xtrack location: 0 for center of loiter wp, 1 for exit location */
force_heading : 1, /**< heading needs to be reached ***/
altitude_is_relative : 1, /**< true if altitude is relative from start point */
autocontinue : 1, /**< true if next waypoint should follow after this one */
disable_mc_yaw : 1, /**< weathervane mode */
vtol_back_transition : 1; /**< part of the vtol back transition sequence */
};
};
#pragma pack(pop)
#include <uORB/topics/mission.h>
/**
* @}
*/
#endif