MulticopterLandDetector.h
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/****************************************************************************
*
* Copyright (c) 2013-2016 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 MulticopterLandDetector.h
* Land detection implementation for multicopters.
*
* @author Johan Jansen <jnsn.johan@gmail.com>
* @author Morten Lysgaard <morten@lysgaard.no>
* @author Julian Oes <julian@oes.ch>
*/
#pragma once
#include <uORB/topics/actuator_controls.h>
#include <uORB/topics/hover_thrust_estimate.h>
#include <uORB/topics/vehicle_angular_velocity.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/topics/vehicle_local_position_setpoint.h>
#include <uORB/topics/takeoff_status.h>
#include "LandDetector.h"
using namespace time_literals;
namespace land_detector
{
class MulticopterLandDetector : public LandDetector
{
public:
MulticopterLandDetector();
~MulticopterLandDetector() override = default;
protected:
void _update_params() override;
void _update_topics() override;
bool _get_landed_state() override;
bool _get_ground_contact_state() override;
bool _get_maybe_landed_state() override;
bool _get_freefall_state() override;
bool _get_ground_effect_state() override;
bool _get_in_descend() override { return _in_descend; }
bool _get_has_low_throttle() override { return _has_low_throttle; }
bool _get_horizontal_movement() override { return _horizontal_movement; }
bool _get_vertical_movement() override { return _vertical_movement; }
bool _get_close_to_ground_or_skipped_check() override { return _close_to_ground_or_skipped_check; }
float _get_max_altitude() override;
void _set_hysteresis_factor(const int factor) override;
private:
float _get_gnd_effect_altitude();
bool _is_close_to_ground();
/** Time in us that freefall has to hold before triggering freefall */
static constexpr hrt_abstime FREEFALL_TRIGGER_TIME_US = 300_ms;
/** Time interval in us in which wider acceptance thresholds are used after landed. */
static constexpr hrt_abstime LAND_DETECTOR_LAND_PHASE_TIME_US = 2_s;
/** Distance above ground below which entering ground contact state is possible when distance to ground is available. */
static constexpr float DIST_FROM_GROUND_THRESHOLD = 1.0f;
/** Handles for interesting parameters. **/
struct {
param_t minThrottle;
param_t hoverThrottle;
param_t minManThrottle;
param_t landSpeed;
param_t useHoverThrustEstimate;
} _paramHandle{};
struct {
float minThrottle;
float hoverThrottle;
float minManThrottle;
float landSpeed;
bool useHoverThrustEstimate;
} _params{};
uORB::Subscription _actuator_controls_sub{ORB_ID(actuator_controls_0)};
uORB::Subscription _hover_thrust_estimate_sub{ORB_ID(hover_thrust_estimate)};
uORB::Subscription _trajectory_setpoint_sub{ORB_ID(trajectory_setpoint)};
uORB::Subscription _vehicle_angular_velocity_sub{ORB_ID(vehicle_angular_velocity)};
uORB::Subscription _vehicle_control_mode_sub{ORB_ID(vehicle_control_mode)};
uORB::Subscription _takeoff_status_sub{ORB_ID(takeoff_status)};
hrt_abstime _hover_thrust_estimate_last_valid{0};
bool _hover_thrust_estimate_valid{false};
bool _flag_control_climb_rate_enabled{false};
bool _hover_thrust_initialized{false};
float _actuator_controls_throttle{0.f};
uint8_t _takeoff_state{takeoff_status_s::TAKEOFF_STATE_DISARMED};
hrt_abstime _min_thrust_start{0}; ///< timestamp when minimum trust was applied first
hrt_abstime _landed_time{0};
bool _in_descend{false}; ///< vehicle is desending
bool _horizontal_movement{false}; ///< vehicle is moving horizontally
bool _vertical_movement{false};
bool _has_low_throttle{false};
bool _close_to_ground_or_skipped_check{false};
bool _below_gnd_effect_hgt{false}; ///< vehicle height above ground is below height where ground effect occurs
DEFINE_PARAMETERS_CUSTOM_PARENT(
LandDetector,
(ParamFloat<px4::params::LNDMC_TRIG_TIME>) _param_lndmc_trig_time,
(ParamFloat<px4::params::LNDMC_ALT_MAX>) _param_lndmc_alt_max,
(ParamFloat<px4::params::LNDMC_ROT_MAX>) _param_lndmc_rot_max,
(ParamFloat<px4::params::LNDMC_XY_VEL_MAX>) _param_lndmc_xy_vel_max,
(ParamFloat<px4::params::LNDMC_Z_VEL_MAX>) _param_lndmc_z_vel_max,
(ParamFloat<px4::params::LNDMC_ALT_GND>) _param_lndmc_alt_gnd_effect
);
};
} // namespace land_detector