mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-07-17 15:00:35 +08:00
7a760c8c6e
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
197 lines
6.0 KiB
C++
197 lines
6.0 KiB
C++
/***************************************************************************
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*
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* Copyright (c) 2013-2020 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 rtl.h
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*
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* Helper class for RTL
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*
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* @author Julian Oes <julian@oes.ch>
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* @author Anton Babushkin <anton.babushkin@me.com>
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*/
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#pragma once
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#include <px4_platform_common/module_params.h>
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#include "navigator_mode.h"
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#include "mission_block.h"
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#include <uORB/Subscription.hpp>
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#include <uORB/topics/home_position.h>
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#include <uORB/topics/rtl_time_estimate.h>
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#include <uORB/topics/vehicle_status.h>
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#include <uORB/topics/wind.h>
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#include <matrix/math.hpp>
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#include <lib/geo/geo.h>
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class Navigator;
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class RTL : public MissionBlock, public ModuleParams
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{
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public:
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RTL(Navigator *navigator);
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~RTL() = default;
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enum RTLType {
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RTL_TYPE_HOME_OR_RALLY = 0,
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RTL_TYPE_MISSION_LANDING,
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RTL_TYPE_MISSION_LANDING_REVERSED,
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RTL_TYPE_CLOSEST,
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};
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enum RTLDestinationType {
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RTL_DESTINATION_HOME = 0,
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RTL_DESTINATION_MISSION_LANDING,
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RTL_DESTINATION_SAFE_POINT,
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};
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enum RTLHeadingMode {
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RTL_NAVIGATION_HEADING = 0,
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RTL_DESTINATION_HEADING,
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RTL_CURRENT_HEADING,
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};
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enum RTLState {
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RTL_STATE_NONE = 0,
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RTL_STATE_CLIMB,
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RTL_STATE_RETURN,
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RTL_STATE_DESCEND,
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RTL_STATE_LOITER,
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RTL_STATE_TRANSITION_TO_MC,
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RTL_MOVE_TO_LAND_HOVER_VTOL,
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RTL_STATE_LAND,
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RTL_STATE_LANDED,
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RTL_STATE_HEAD_TO_CENTER,
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};
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void on_inactivation() override;
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void on_inactive() override;
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void on_activation() override;
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void on_active() override;
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void find_RTL_destination();
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void set_return_alt_min(bool min) { _rtl_alt_min = min; }
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int get_rtl_type() const { return _param_rtl_type.get(); }
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void get_rtl_xy_z_speed(float &xy, float &z);
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matrix::Vector2f get_wind();
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RTLState getRTLState() { return _rtl_state; }
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bool getShouldEngageMissionForLanding() const { return _should_engange_mission_for_landing; }
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private:
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void set_rtl_item();
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void advance_rtl();
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float calculate_return_alt_from_cone_half_angle(float cone_half_angle_deg);
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void calc_and_pub_rtl_time_estimate(const RTLState rtl_state);
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float getCruiseGroundSpeed();
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float getClimbRate();
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float getDescendRate();
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float getCruiseSpeed();
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float getHoverLandSpeed();
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RTLState _rtl_state{RTL_STATE_NONE};
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struct RTLPosition {
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double lat;
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double lon;
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float alt;
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float yaw;
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uint8_t safe_point_index; ///< 0 = home position, 1 = mission landing, >1 = safe landing points (rally points)
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RTLDestinationType type{RTL_DESTINATION_HOME};
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void set(const home_position_s &home_position)
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{
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lat = home_position.lat;
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lon = home_position.lon;
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alt = home_position.alt;
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yaw = home_position.yaw;
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safe_point_index = 0;
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type = RTL_DESTINATION_HOME;
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}
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};
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RTLPosition _destination{}; ///< the RTL position to fly to (typically the home position or a safe point)
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hrt_abstime _destination_check_time{0};
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float _rtl_alt{0.0f}; // AMSL altitude at which the vehicle should return to the home position
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bool _rtl_alt_min{false};
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bool _should_engange_mission_for_landing{false};
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DEFINE_PARAMETERS(
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(ParamFloat<px4::params::RTL_RETURN_ALT>) _param_rtl_return_alt,
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(ParamFloat<px4::params::RTL_DESCEND_ALT>) _param_rtl_descend_alt,
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(ParamFloat<px4::params::RTL_LAND_DELAY>) _param_rtl_land_delay,
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(ParamFloat<px4::params::RTL_MIN_DIST>) _param_rtl_min_dist,
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(ParamInt<px4::params::RTL_TYPE>) _param_rtl_type,
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(ParamInt<px4::params::RTL_CONE_ANG>) _param_rtl_cone_half_angle_deg,
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(ParamInt<px4::params::RTL_PLD_MD>) _param_rtl_pld_md,
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(ParamFloat<px4::params::RTL_LOITER_RAD>) _param_rtl_loiter_rad,
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(ParamInt<px4::params::RTL_HDG_MD>) _param_rtl_hdg_md,
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(ParamFloat<px4::params::RTL_TIME_FACTOR>) _param_rtl_time_factor,
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(ParamInt<px4::params::RTL_TIME_MARGIN>) _param_rtl_time_margin
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)
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param_t _param_mpc_z_v_auto_up{PARAM_INVALID};
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param_t _param_mpc_z_v_auto_dn{PARAM_INVALID};
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param_t _param_mpc_land_speed{PARAM_INVALID};
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param_t _param_fw_climb_rate{PARAM_INVALID};
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param_t _param_fw_sink_rate{PARAM_INVALID};
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param_t _param_fw_airspeed_trim{PARAM_INVALID};
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param_t _param_mpc_xy_cruise{PARAM_INVALID};
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param_t _param_rover_cruise_speed{PARAM_INVALID};
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uORB::SubscriptionData<wind_s> _wind_sub{ORB_ID(wind)};
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uORB::Publication<rtl_time_estimate_s> _rtl_time_estimate_pub{ORB_ID(rtl_time_estimate)};
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};
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float time_to_home(const matrix::Vector3f &to_home_vec,
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const matrix::Vector2f &wind_velocity, float vehicle_speed_m_s,
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float vehicle_descent_speed_m_s);
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