FlightTaskOrbit.hpp
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/****************************************************************************
*
* Copyright (c) 2017-2019 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 FlightTaskOrbit.hpp
*
* Flight task for orbiting in a circle around a target position
*
* @author Matthias Grob <maetugr@gmail.com>
*/
#pragma once
#include "FlightTaskManualAltitudeSmoothVel.hpp"
#include <uORB/Publication.hpp>
#include <uORB/topics/orbit_status.h>
#include "StraightLine.hpp"
#include <lib/slew_rate/SlewRateYaw.hpp>
class FlightTaskOrbit : public FlightTaskManualAltitudeSmoothVel
{
public:
FlightTaskOrbit();
virtual ~FlightTaskOrbit() = default;
bool applyCommandParameters(const vehicle_command_s &command) override;
bool activate(const vehicle_local_position_setpoint_s &last_setpoint) override;
bool update() override;
/**
* Check the feasibility of orbit parameters with respect to
* centripetal acceleration a = v^2 / r
* @param r desired radius
* @param v desired velocity
* @param a maximal allowed acceleration
* @return true on success, false if value not accepted
*/
bool checkAcceleration(float r, float v, float a);
protected:
/**
* Send out telemetry information for the log and MAVLink.
* @return true on success, false on error
*/
bool sendTelemetry();
/**
* Change the radius of the circle.
* @param r desired new radius
* @return true on success, false if value not accepted
*/
bool setRadius(const float r);
/**
* Change the velocity of the vehicle on the circle.
* @param v desired new velocity
* @return true on success, false if value not accepted
*/
bool setVelocity(const float v);
private:
/** generates setpoints to smoothly reach the closest point on the circle when starting from far away */
void generate_circle_approach_setpoints(const matrix::Vector2f ¢er_to_position);
/** generates xy setpoints to make the vehicle orbit */
void generate_circle_setpoints(const matrix::Vector2f ¢er_to_position);
/** generates yaw setpoints to control the vehicle's heading */
void generate_circle_yaw_setpoints(const matrix::Vector2f ¢er_to_position);
float _r = 0.f; /**< radius with which to orbit the target */
float _v = 0.f; /**< clockwise tangential velocity for orbiting in m/s */
matrix::Vector2f _center; /**< local frame coordinates of the center point */
bool _in_circle_approach = false;
StraightLine _circle_approach_line;
// TODO: create/use parameters for limits
const float _radius_min = 1.f;
const float _radius_max = 100.f;
const float _velocity_max = 10.f;
const float _acceleration_max = 2.f;
/** yaw behaviour during the orbit flight according to MAVLink's ORBIT_YAW_BEHAVIOUR enum */
int _yaw_behaviour = orbit_status_s::ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TO_CIRCLE_CENTER;
float _initial_heading = 0.f; /**< the heading of the drone when the orbit command was issued */
SlewRateYaw<float> _slew_rate_yaw;
uORB::Publication<orbit_status_s> _orbit_status_pub{ORB_ID(orbit_status)};
DEFINE_PARAMETERS(
(ParamFloat<px4::params::MPC_XY_CRUISE>) _param_mpc_xy_cruise, /**< cruise speed for circle approach */
(ParamFloat<px4::params::MPC_YAWRAUTO_MAX>) _param_mpc_yawrauto_max
)
};