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PX4-Autopilot/src/modules/navigator/rtl.h
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2022-09-15 13:17:36 -04:00

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/***************************************************************************
*
* Copyright (c) 2013-2020 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 rtl.h
*
* Helper class for RTL
*
* @author Julian Oes <julian@oes.ch>
* @author Anton Babushkin <anton.babushkin@me.com>
*/
#pragma once
#include <px4_platform_common/module_params.h>
#include "navigator_mode.h"
#include "mission_block.h"
#include <uORB/Subscription.hpp>
#include <uORB/topics/home_position.h>
#include <uORB/topics/rtl_time_estimate.h>
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/wind.h>
#include <matrix/math.hpp>
#include <lib/geo/geo.h>
class Navigator;
class RTL : public MissionBlock, public ModuleParams
{
public:
RTL(Navigator *navigator);
~RTL() = default;
enum RTLType {
RTL_TYPE_HOME_OR_RALLY = 0,
RTL_TYPE_MISSION_LANDING,
RTL_TYPE_MISSION_LANDING_REVERSED,
RTL_TYPE_CLOSEST,
};
enum RTLDestinationType {
RTL_DESTINATION_HOME = 0,
RTL_DESTINATION_MISSION_LANDING,
RTL_DESTINATION_SAFE_POINT,
};
enum RTLHeadingMode {
RTL_NAVIGATION_HEADING = 0,
RTL_DESTINATION_HEADING,
RTL_CURRENT_HEADING,
};
enum RTLState {
RTL_STATE_NONE = 0,
RTL_STATE_CLIMB,
RTL_STATE_RETURN,
RTL_STATE_DESCEND,
RTL_STATE_LOITER,
RTL_STATE_TRANSITION_TO_MC,
RTL_MOVE_TO_LAND_HOVER_VTOL,
RTL_STATE_LAND,
RTL_STATE_LANDED,
RTL_STATE_HEAD_TO_CENTER,
};
void on_inactivation() override;
void on_inactive() override;
void on_activation() override;
void on_active() override;
void find_RTL_destination();
void set_return_alt_min(bool min) { _rtl_alt_min = min; }
int get_rtl_type() const { return _param_rtl_type.get(); }
void get_rtl_xy_z_speed(float &xy, float &z);
matrix::Vector2f get_wind();
RTLState getRTLState() { return _rtl_state; }
bool getShouldEngageMissionForLanding() const { return _should_engange_mission_for_landing; }
private:
void set_rtl_item();
void advance_rtl();
float calculate_return_alt_from_cone_half_angle(float cone_half_angle_deg);
void calc_and_pub_rtl_time_estimate(const RTLState rtl_state);
float getCruiseGroundSpeed();
float getClimbRate();
float getDescendRate();
float getCruiseSpeed();
float getHoverLandSpeed();
RTLState _rtl_state{RTL_STATE_NONE};
struct RTLPosition {
double lat;
double lon;
float alt;
float yaw;
uint8_t safe_point_index; ///< 0 = home position, 1 = mission landing, >1 = safe landing points (rally points)
RTLDestinationType type{RTL_DESTINATION_HOME};
void set(const home_position_s &home_position)
{
lat = home_position.lat;
lon = home_position.lon;
alt = home_position.alt;
yaw = home_position.yaw;
safe_point_index = 0;
type = RTL_DESTINATION_HOME;
}
};
RTLPosition _destination{}; ///< the RTL position to fly to (typically the home position or a safe point)
hrt_abstime _destination_check_time{0};
float _rtl_alt{0.0f}; // AMSL altitude at which the vehicle should return to the home position
bool _rtl_alt_min{false};
bool _should_engange_mission_for_landing{false};
DEFINE_PARAMETERS(
(ParamFloat<px4::params::RTL_RETURN_ALT>) _param_rtl_return_alt,
(ParamFloat<px4::params::RTL_DESCEND_ALT>) _param_rtl_descend_alt,
(ParamFloat<px4::params::RTL_LAND_DELAY>) _param_rtl_land_delay,
(ParamFloat<px4::params::RTL_MIN_DIST>) _param_rtl_min_dist,
(ParamInt<px4::params::RTL_TYPE>) _param_rtl_type,
(ParamInt<px4::params::RTL_CONE_ANG>) _param_rtl_cone_half_angle_deg,
(ParamInt<px4::params::RTL_PLD_MD>) _param_rtl_pld_md,
(ParamFloat<px4::params::RTL_LOITER_RAD>) _param_rtl_loiter_rad,
(ParamInt<px4::params::RTL_HDG_MD>) _param_rtl_hdg_md,
(ParamFloat<px4::params::RTL_TIME_FACTOR>) _param_rtl_time_factor,
(ParamInt<px4::params::RTL_TIME_MARGIN>) _param_rtl_time_margin
)
param_t _param_mpc_z_v_auto_up{PARAM_INVALID};
param_t _param_mpc_z_v_auto_dn{PARAM_INVALID};
param_t _param_mpc_land_speed{PARAM_INVALID};
param_t _param_fw_climb_rate{PARAM_INVALID};
param_t _param_fw_sink_rate{PARAM_INVALID};
param_t _param_fw_airspeed_trim{PARAM_INVALID};
param_t _param_mpc_xy_cruise{PARAM_INVALID};
param_t _param_rover_cruise_speed{PARAM_INVALID};
uORB::SubscriptionData<wind_s> _wind_sub{ORB_ID(wind)};
uORB::Publication<rtl_time_estimate_s> _rtl_time_estimate_pub{ORB_ID(rtl_time_estimate)};
};
float time_to_home(const matrix::Vector3f &to_home_vec,
const matrix::Vector2f &wind_velocity, float vehicle_speed_m_s,
float vehicle_descent_speed_m_s);