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436 lines
14 KiB
C++
436 lines
14 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2014 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file mission_block.cpp
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*
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* Helper class to use mission items
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*
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* @author Julian Oes <julian@oes.ch>
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* @author Sander Smeets <sander@droneslab.com>
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*/
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#include <sys/types.h>
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#include <string.h>
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#include <stdlib.h>
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#include <unistd.h>
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#include <math.h>
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#include <float.h>
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#include <systemlib/err.h>
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#include <geo/geo.h>
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#include <mavlink/mavlink_log.h>
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#include <uORB/uORB.h>
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#include <uORB/topics/actuator_controls.h>
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#include <uORB/topics/vehicle_command.h>
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#include "navigator.h"
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#include "mission_block.h"
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actuator_controls_s actuators;
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orb_advert_t actuator_pub_fd;
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MissionBlock::MissionBlock(Navigator *navigator, const char *name) :
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NavigatorMode(navigator, name),
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_mission_item({0}),
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_waypoint_position_reached(false),
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_waypoint_yaw_reached(false),
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_time_first_inside_orbit(0),
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_actuators{},
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_actuator_pub(nullptr),
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_cmd_pub(nullptr)
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{
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}
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MissionBlock::~MissionBlock()
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{
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}
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bool
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MissionBlock::is_mission_item_reached()
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{
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/* handle non-navigation or indefinite waypoints */
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switch (_mission_item.nav_cmd) {
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case NAV_CMD_DO_SET_SERVO: {
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memset(&actuators, 0, sizeof(actuators));
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actuators.control[_mission_item.actuator_num] = 1.0f / 2000 * -_mission_item.actuator_value;
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actuators.timestamp = hrt_absolute_time();
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if (_actuator_pub != nullptr) {
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orb_publish(ORB_ID(actuator_controls_2), _actuator_pub, &actuators);
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} else {
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_actuator_pub = orb_advertise(ORB_ID(actuator_controls_2), &actuators);
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}
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return true;
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}
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case NAV_CMD_LAND:
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return _navigator->get_vstatus()->condition_landed;
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/* TODO: count turns */
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/*_mission_item.nav_cmd == NAV_CMD_LOITER_TURN_COUNT ||*/
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case NAV_CMD_IDLE: /* fall through */
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case NAV_CMD_LOITER_UNLIMITED:
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return false;
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case vehicle_command_s::VEHICLE_CMD_DO_DIGICAM_CONTROL: /* fallthrough */
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case vehicle_command_s::VEHICLE_CMD_DO_VTOL_TRANSITION:
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{
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/* forward the command to other processes */
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warnx("got instantaneous command, forwarding.\n");
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struct vehicle_command_s cmd = {};
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cmd.command = _mission_item.nav_cmd;
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mission_item_to_vehicle_command(&_mission_item, &cmd);
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if (_cmd_pub != nullptr) {
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orb_publish(ORB_ID(vehicle_command), _cmd_pub, &cmd);
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} else {
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_cmd_pub = orb_advertise(ORB_ID(vehicle_command), &cmd);
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}
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return true;
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}
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default:
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/* do nothing, this is a 3D waypoint */
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break;
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}
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hrt_abstime now = hrt_absolute_time();
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if (!_waypoint_position_reached) {
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float dist = -1.0f;
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float dist_xy = -1.0f;
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float dist_z = -1.0f;
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float altitude_amsl = _mission_item.altitude_is_relative
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? _mission_item.altitude + _navigator->get_home_position()->alt
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: _mission_item.altitude;
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dist = get_distance_to_point_global_wgs84(_mission_item.lat, _mission_item.lon, altitude_amsl,
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_navigator->get_global_position()->lat,
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_navigator->get_global_position()->lon,
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_navigator->get_global_position()->alt,
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&dist_xy, &dist_z);
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if (_mission_item.nav_cmd == NAV_CMD_TAKEOFF && _navigator->get_vstatus()->is_rotary_wing) {
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/* require only altitude for takeoff for multicopter, do not use waypoint acceptance radius */
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if (_navigator->get_global_position()->alt >
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altitude_amsl - _navigator->get_acceptance_radius()) {
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_waypoint_position_reached = true;
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}
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} else if (_mission_item.nav_cmd == NAV_CMD_TAKEOFF) {
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/* for takeoff mission items use the parameter for the takeoff acceptance radius */
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if (dist >= 0.0f && dist <= _navigator->get_acceptance_radius()) {
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_waypoint_position_reached = true;
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}
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} else if (!_navigator->get_vstatus()->is_rotary_wing &&
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(_mission_item.nav_cmd == NAV_CMD_LOITER_UNLIMITED ||
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_mission_item.nav_cmd == NAV_CMD_LOITER_TIME_LIMIT ||
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_mission_item.nav_cmd == NAV_CMD_LOITER_TURN_COUNT)) {
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/* Loiter mission item on a non rotary wing: the aircraft is going to circle the
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* coordinates with a radius equal to the loiter_radius field. It is not flying
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* through the waypoint center.
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* Therefore the item is marked as reached once the system reaches the loiter
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* radius (+ some margin). Time inside and turn count is handled elsewhere.
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*/
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if (dist >= 0.0f && dist <= _navigator->get_acceptance_radius(_mission_item.loiter_radius * 1.2f)) {
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_waypoint_position_reached = true;
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}
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} else {
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/* for normal mission items used their acceptance radius */
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float mission_acceptance_radius = _navigator->get_acceptance_radius(_mission_item.acceptance_radius);
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/* if set to zero use the default instead */
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if (mission_acceptance_radius < NAV_EPSILON_POSITION) {
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mission_acceptance_radius = _navigator->get_acceptance_radius();
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}
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if (dist >= 0.0f && dist <= mission_acceptance_radius) {
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_waypoint_position_reached = true;
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}
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}
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}
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/* Check if the waypoint and the requested yaw setpoint. */
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if (_waypoint_position_reached && !_waypoint_yaw_reached) {
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/* TODO: removed takeoff, why? */
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if (_navigator->get_vstatus()->is_rotary_wing && PX4_ISFINITE(_mission_item.yaw)) {
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/* check yaw if defined only for rotary wing except takeoff */
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float yaw_err = _wrap_pi(_mission_item.yaw - _navigator->get_global_position()->yaw);
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if (fabsf(yaw_err) < 0.2f) { /* TODO: get rid of magic number */
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_waypoint_yaw_reached = true;
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}
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} else {
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_waypoint_yaw_reached = true;
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}
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}
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/* Once the waypoint and yaw setpoint have been reached we can start the loiter time countdown */
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if (_waypoint_position_reached && _waypoint_yaw_reached) {
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if (_time_first_inside_orbit == 0) {
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_time_first_inside_orbit = now;
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// if (_mission_item.time_inside > 0.01f) {
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// mavlink_log_critical(_mavlink_fd, "waypoint reached, wait for %.1fs",
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// (double)_mission_item.time_inside);
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// }
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}
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/* check if the MAV was long enough inside the waypoint orbit */
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if (now - _time_first_inside_orbit >= (hrt_abstime)_mission_item.time_inside * 1e6f) {
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return true;
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}
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}
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return false;
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}
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void
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MissionBlock::reset_mission_item_reached()
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{
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_waypoint_position_reached = false;
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_waypoint_yaw_reached = false;
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_time_first_inside_orbit = 0;
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}
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void
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MissionBlock::mission_item_to_vehicle_command(const struct mission_item_s *item, struct vehicle_command_s *cmd)
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{
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// we're expecting a mission command item here so assign the "raw" inputs to the command
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// (MAV_FRAME_MISSION mission item)
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cmd->param1 = item->params[0];
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cmd->param2 = item->params[1];
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cmd->param3 = item->params[2];
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cmd->param4 = item->params[3];
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cmd->param5 = item->params[4];
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cmd->param6 = item->params[5];
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cmd->param7 = item->params[6];
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cmd->target_system = _navigator->get_vstatus()->system_id;
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cmd->target_component = _navigator->get_vstatus()->component_id;
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cmd->source_system = _navigator->get_vstatus()->system_id;
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cmd->source_component = _navigator->get_vstatus()->component_id;
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cmd->confirmation = false;
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}
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void
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MissionBlock::mission_item_to_position_setpoint(const struct mission_item_s *item, struct position_setpoint_s *sp)
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{
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sp->valid = true;
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sp->lat = item->lat;
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sp->lon = item->lon;
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sp->alt = item->altitude_is_relative ? item->altitude + _navigator->get_home_position()->alt : item->altitude;
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sp->yaw = item->yaw;
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sp->loiter_radius = (item->loiter_radius > NAV_EPSILON_POSITION) ? item->loiter_radius :
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_navigator->get_loiter_radius();
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sp->loiter_direction = item->loiter_direction;
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sp->pitch_min = item->pitch_min;
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sp->acceptance_radius = item->acceptance_radius;
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switch (item->nav_cmd) {
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case NAV_CMD_DO_SET_SERVO:
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/* Set current position for loitering set point*/
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sp->lat = _navigator->get_global_position()->lat;
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sp->lon = _navigator->get_global_position()->lon;
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sp->alt = _navigator->get_global_position()->alt;
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sp->type = position_setpoint_s::SETPOINT_TYPE_LOITER;
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break;
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case NAV_CMD_IDLE:
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sp->type = position_setpoint_s::SETPOINT_TYPE_IDLE;
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break;
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case NAV_CMD_TAKEOFF:
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sp->type = position_setpoint_s::SETPOINT_TYPE_TAKEOFF;
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break;
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case NAV_CMD_LAND:
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sp->type = position_setpoint_s::SETPOINT_TYPE_LAND;
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break;
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case NAV_CMD_LOITER_TIME_LIMIT:
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case NAV_CMD_LOITER_TURN_COUNT:
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case NAV_CMD_LOITER_UNLIMITED:
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sp->type = position_setpoint_s::SETPOINT_TYPE_LOITER;
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break;
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default:
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sp->type = position_setpoint_s::SETPOINT_TYPE_POSITION;
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break;
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}
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}
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void
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MissionBlock::set_previous_pos_setpoint()
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{
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struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
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if (pos_sp_triplet->current.valid) {
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memcpy(&pos_sp_triplet->previous, &pos_sp_triplet->current, sizeof(struct position_setpoint_s));
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}
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}
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void
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MissionBlock::set_loiter_item(struct mission_item_s *item, float min_clearance)
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{
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if (_navigator->get_vstatus()->condition_landed) {
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/* landed, don't takeoff, but switch to IDLE mode */
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item->nav_cmd = NAV_CMD_IDLE;
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} else {
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item->nav_cmd = NAV_CMD_LOITER_UNLIMITED;
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struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
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if (_navigator->get_can_loiter_at_sp() && pos_sp_triplet->current.valid) {
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/* use current position setpoint */
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item->lat = pos_sp_triplet->current.lat;
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item->lon = pos_sp_triplet->current.lon;
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item->altitude = pos_sp_triplet->current.alt;
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} else {
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/* use current position and use return altitude as clearance */
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item->lat = _navigator->get_global_position()->lat;
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item->lon = _navigator->get_global_position()->lon;
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item->altitude = _navigator->get_global_position()->alt;
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if (min_clearance > 0.0f && item->altitude < _navigator->get_home_position()->alt + min_clearance) {
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item->altitude = _navigator->get_home_position()->alt + min_clearance;
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}
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}
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item->altitude_is_relative = false;
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item->yaw = NAN;
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item->loiter_radius = _navigator->get_loiter_radius();
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item->loiter_direction = 1;
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item->acceptance_radius = _navigator->get_acceptance_radius();
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item->time_inside = 0.0f;
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item->pitch_min = 0.0f;
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item->autocontinue = false;
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item->origin = ORIGIN_ONBOARD;
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}
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}
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void
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MissionBlock::set_takeoff_item(struct mission_item_s *item, float min_clearance, float min_pitch)
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{
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item->nav_cmd = NAV_CMD_TAKEOFF;
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/* use current position and use return altitude as clearance */
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item->lat = _navigator->get_global_position()->lat;
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item->lon = _navigator->get_global_position()->lon;
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item->altitude = _navigator->get_global_position()->alt;
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if (min_clearance > 0.0f) {
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item->altitude += min_clearance;
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/* we must takeoff to a point further above ground than the acceptance radius */
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if (_navigator->get_acceptance_radius() > min_clearance) {
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item->altitude += _navigator->get_acceptance_radius();
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}
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}
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item->altitude_is_relative = false;
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item->yaw = NAN;
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item->loiter_radius = _navigator->get_loiter_radius();
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item->loiter_direction = 1;
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item->time_inside = 0.0f;
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item->pitch_min = min_pitch;
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item->autocontinue = false;
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item->origin = ORIGIN_ONBOARD;
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}
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void
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MissionBlock::set_land_item(struct mission_item_s *item, bool at_current_location)
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{
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/* VTOL transition to RW before landing */
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if(_navigator->get_vstatus()->is_vtol){
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struct vehicle_command_s cmd = {};
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cmd.command = NAV_CMD_DO_VTOL_TRANSITION;
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cmd.param1 = 3;
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if (_cmd_pub != nullptr) {
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orb_publish(ORB_ID(vehicle_command), _cmd_pub, &cmd);
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} else {
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_cmd_pub = orb_advertise(ORB_ID(vehicle_command), &cmd);
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}
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}
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/* set the land item */
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item->nav_cmd = NAV_CMD_LAND;
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/* use current position */
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if (at_current_location) {
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item->lat = _navigator->get_global_position()->lat;
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item->lon = _navigator->get_global_position()->lon;
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/* use home position */
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} else {
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item->lat = _navigator->get_home_position()->lat;
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item->lon = _navigator->get_home_position()->lon;
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}
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item->altitude = 0;
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item->altitude_is_relative = false;
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item->yaw = NAN;
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item->loiter_radius = _navigator->get_loiter_radius();
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item->loiter_direction = 1;
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item->acceptance_radius = _navigator->get_acceptance_radius();
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item->time_inside = 0.0f;
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item->pitch_min = 0.0f;
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item->autocontinue = true;
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item->origin = ORIGIN_ONBOARD;
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}
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void
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MissionBlock::set_idle_item(struct mission_item_s *item)
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{
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item->nav_cmd = NAV_CMD_IDLE;
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item->lat = _navigator->get_home_position()->lat;
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item->lon = _navigator->get_home_position()->lon;
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item->altitude_is_relative = false;
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item->altitude = _navigator->get_home_position()->alt;
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item->yaw = NAN;
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item->loiter_radius = _navigator->get_loiter_radius();
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item->loiter_direction = 1;
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item->acceptance_radius = _navigator->get_acceptance_radius();
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item->time_inside = 0.0f;
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item->pitch_min = 0.0f;
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item->autocontinue = true;
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item->origin = ORIGIN_ONBOARD;
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}
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