mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-06-28 19:40:34 +08:00
230 lines
9.1 KiB
C++
230 lines
9.1 KiB
C++
/****************************************************************************
|
|
*
|
|
* Copyright (c) 2013 PX4 Development Team. All rights reserved.
|
|
* Author: @author Lorenz Meier <lm@inf.ethz.ch>
|
|
* @author Thomas Gubler <thomasgubler@student.ethz.ch>
|
|
*
|
|
* 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 mission_feasibility_checker.cpp
|
|
* Provides checks if mission is feasible given the navigation capabilities
|
|
*/
|
|
|
|
#include "mission_feasibility_checker.h"
|
|
|
|
#include <geo/geo.h>
|
|
#include <math.h>
|
|
#include <mathlib/mathlib.h>
|
|
#include <mavlink/mavlink_log.h>
|
|
#include <fw_pos_control_l1/landingslope.h>
|
|
#include <systemlib/err.h>
|
|
#include <stdio.h>
|
|
#include <fcntl.h>
|
|
#include <errno.h>
|
|
#include <uORB/topics/fence.h>
|
|
|
|
/* oddly, ERROR is not defined for c++ */
|
|
#ifdef ERROR
|
|
# undef ERROR
|
|
#endif
|
|
static const int ERROR = -1;
|
|
|
|
MissionFeasibilityChecker::MissionFeasibilityChecker() : _mavlink_fd(-1), _capabilities_sub(-1), _initDone(false)
|
|
{
|
|
_nav_caps = {0};
|
|
}
|
|
|
|
|
|
bool MissionFeasibilityChecker::checkMissionFeasible(bool isRotarywing, dm_item_t dm_current, size_t nMissionItems, Geofence &geofence, float home_alt)
|
|
{
|
|
/* Init if not done yet */
|
|
init();
|
|
|
|
/* Open mavlink fd */
|
|
if (_mavlink_fd < 0) {
|
|
/* try to open the mavlink log device every once in a while */
|
|
_mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
|
|
}
|
|
|
|
|
|
if (isRotarywing)
|
|
return checkMissionFeasibleRotarywing(dm_current, nMissionItems, geofence, home_alt);
|
|
else
|
|
return checkMissionFeasibleFixedwing(dm_current, nMissionItems, geofence, home_alt);
|
|
}
|
|
|
|
bool MissionFeasibilityChecker::checkMissionFeasibleRotarywing(dm_item_t dm_current, size_t nMissionItems, Geofence &geofence, float home_alt)
|
|
{
|
|
|
|
return (checkGeofence(dm_current, nMissionItems, geofence) && checkHomePositionAltitude(dm_current, nMissionItems, home_alt));
|
|
}
|
|
|
|
bool MissionFeasibilityChecker::checkMissionFeasibleFixedwing(dm_item_t dm_current, size_t nMissionItems, Geofence &geofence, float home_alt)
|
|
{
|
|
/* Update fixed wing navigation capabilites */
|
|
updateNavigationCapabilities();
|
|
// warnx("_nav_caps.landing_slope_angle_rad %.4f, _nav_caps.landing_horizontal_slope_displacement %.4f", _nav_caps.landing_slope_angle_rad, _nav_caps.landing_horizontal_slope_displacement);
|
|
|
|
return (checkFixedWingLanding(dm_current, nMissionItems) && checkGeofence(dm_current, nMissionItems, geofence) && checkHomePositionAltitude(dm_current, nMissionItems, home_alt));
|
|
}
|
|
|
|
bool MissionFeasibilityChecker::checkGeofence(dm_item_t dm_current, size_t nMissionItems, Geofence &geofence)
|
|
{
|
|
/* Check if all mission items are inside the geofence (if we have a valid geofence) */
|
|
if (geofence.valid()) {
|
|
for (size_t i = 0; i < nMissionItems; i++) {
|
|
static struct mission_item_s missionitem;
|
|
const ssize_t len = sizeof(struct mission_item_s);
|
|
|
|
if (dm_read(dm_current, i, &missionitem, len) != len) {
|
|
/* not supposed to happen unless the datamanager can't access the SD card, etc. */
|
|
return false;
|
|
}
|
|
|
|
if (!geofence.inside(missionitem.lat, missionitem.lon, missionitem.altitude)) {
|
|
mavlink_log_info(_mavlink_fd, "#audio: Geofence violation waypoint %d", i);
|
|
return false;
|
|
}
|
|
}
|
|
}
|
|
|
|
return true;
|
|
}
|
|
|
|
bool MissionFeasibilityChecker::checkHomePositionAltitude(dm_item_t dm_current, size_t nMissionItems, float home_alt, bool throw_error)
|
|
{
|
|
/* Check if all all waypoints are above the home altitude, only return false if bool throw_error = true */
|
|
for (size_t i = 0; i < nMissionItems; i++) {
|
|
static struct mission_item_s missionitem;
|
|
const ssize_t len = sizeof(struct mission_item_s);
|
|
|
|
if (dm_read(dm_current, i, &missionitem, len) != len) {
|
|
/* not supposed to happen unless the datamanager can't access the SD card, etc. */
|
|
if (throw_error) {
|
|
return false;
|
|
} else {
|
|
return true;
|
|
}
|
|
}
|
|
|
|
if (home_alt > missionitem.altitude) {
|
|
mavlink_log_info(_mavlink_fd, "#audio: warning waypoint %d below home", i);
|
|
if (throw_error) {
|
|
return false;
|
|
} else {
|
|
return true;
|
|
}
|
|
}
|
|
}
|
|
}
|
|
|
|
bool MissionFeasibilityChecker::checkFixedWingLanding(dm_item_t dm_current, size_t nMissionItems)
|
|
{
|
|
/* Go through all mission items and search for a landing waypoint
|
|
* if landing waypoint is found: the previous waypoint is checked to be at a feasible distance and altitude given the landing slope */
|
|
|
|
|
|
for (size_t i = 0; i < nMissionItems; i++) {
|
|
static struct mission_item_s missionitem;
|
|
const ssize_t len = sizeof(struct mission_item_s);
|
|
if (dm_read(dm_current, i, &missionitem, len) != len) {
|
|
/* not supposed to happen unless the datamanager can't access the SD card, etc. */
|
|
return false;
|
|
}
|
|
|
|
if (missionitem.nav_cmd == NAV_CMD_LAND) {
|
|
struct mission_item_s missionitem_previous;
|
|
if (i != 0) {
|
|
if (dm_read(dm_current, i-1, &missionitem_previous, len) != len) {
|
|
/* not supposed to happen unless the datamanager can't access the SD card, etc. */
|
|
return false;
|
|
}
|
|
|
|
float wp_distance = get_distance_to_next_waypoint(missionitem_previous.lat , missionitem_previous.lon, missionitem.lat, missionitem.lon);
|
|
float slope_alt_req = Landingslope::getLandingSlopeAbsoluteAltitude(wp_distance, missionitem.altitude, _nav_caps.landing_horizontal_slope_displacement, _nav_caps.landing_slope_angle_rad);
|
|
float wp_distance_req = Landingslope::getLandingSlopeWPDistance(missionitem_previous.altitude, missionitem.altitude, _nav_caps.landing_horizontal_slope_displacement, _nav_caps.landing_slope_angle_rad);
|
|
float delta_altitude = missionitem.altitude - missionitem_previous.altitude;
|
|
// warnx("wp_distance %.2f, delta_altitude %.2f, missionitem_previous.altitude %.2f, missionitem.altitude %.2f, slope_alt_req %.2f, wp_distance_req %.2f",
|
|
// wp_distance, delta_altitude, missionitem_previous.altitude, missionitem.altitude, slope_alt_req, wp_distance_req);
|
|
// warnx("_nav_caps.landing_horizontal_slope_displacement %.4f, _nav_caps.landing_slope_angle_rad %.4f, _nav_caps.landing_flare_length %.4f",
|
|
// _nav_caps.landing_horizontal_slope_displacement, _nav_caps.landing_slope_angle_rad, _nav_caps.landing_flare_length);
|
|
|
|
if (wp_distance > _nav_caps.landing_flare_length) {
|
|
/* Last wp is before flare region */
|
|
|
|
if (delta_altitude < 0) {
|
|
if (missionitem_previous.altitude <= slope_alt_req) {
|
|
/* Landing waypoint is at or below altitude of slope at the given waypoint distance: this is ok, aircraft will intersect the slope */
|
|
return true;
|
|
} else {
|
|
/* Landing waypoint is above altitude of slope at the given waypoint distance */
|
|
mavlink_log_info(_mavlink_fd, "#audio: Landing: last waypoint too high/too close");
|
|
mavlink_log_info(_mavlink_fd, "Move down to %.1fm or move further away by %.1fm",
|
|
(double)(slope_alt_req),
|
|
(double)(wp_distance_req - wp_distance));
|
|
return false;
|
|
}
|
|
} else {
|
|
/* Landing waypoint is above last waypoint */
|
|
mavlink_log_info(_mavlink_fd, "#audio: Landing waypoint above last nav waypoint");
|
|
return false;
|
|
}
|
|
} else {
|
|
/* Last wp is in flare region */
|
|
//xxx give recommendations
|
|
mavlink_log_info(_mavlink_fd, "#audio: Warning: Landing: last waypoint in flare region");
|
|
return false;
|
|
}
|
|
} else {
|
|
mavlink_log_info(_mavlink_fd, "#audio: Warning: starting with land waypoint");
|
|
return false;
|
|
}
|
|
}
|
|
}
|
|
|
|
|
|
// float slope_alt = wp_altitude + _H0 * expf(-math::max(0.0f, _flare_length - wp_distance)/_flare_constant) - _H1_virt;
|
|
}
|
|
|
|
void MissionFeasibilityChecker::updateNavigationCapabilities()
|
|
{
|
|
int res = orb_copy(ORB_ID(navigation_capabilities), _capabilities_sub, &_nav_caps);
|
|
}
|
|
|
|
void MissionFeasibilityChecker::init()
|
|
{
|
|
if (!_initDone) {
|
|
|
|
_capabilities_sub = orb_subscribe(ORB_ID(navigation_capabilities));
|
|
|
|
_initDone = true;
|
|
}
|
|
}
|