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flight_mode_manager: merge with flight_tasks
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committed by
Lorenz Meier
parent
b1e442b830
commit
4d7b875ee2
@@ -0,0 +1,123 @@
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/****************************************************************************
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*
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* Copyright (c) 2017-2019 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 FlightTaskOrbit.hpp
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*
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* Flight task for orbiting in a circle around a target position
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*
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* @author Matthias Grob <maetugr@gmail.com>
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*/
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#pragma once
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#include "FlightTaskManualAltitudeSmoothVel.hpp"
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#include <uORB/Publication.hpp>
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#include <uORB/topics/orbit_status.h>
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#include <StraightLine.hpp>
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#include <SlewRateYaw.hpp>
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class FlightTaskOrbit : public FlightTaskManualAltitudeSmoothVel
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{
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public:
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FlightTaskOrbit();
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virtual ~FlightTaskOrbit() = default;
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bool applyCommandParameters(const vehicle_command_s &command) override;
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bool activate(const vehicle_local_position_setpoint_s &last_setpoint) override;
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bool update() override;
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/**
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* Check the feasibility of orbit parameters with respect to
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* centripetal acceleration a = v^2 / r
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* @param r desired radius
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* @param v desired velocity
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* @param a maximal allowed acceleration
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* @return true on success, false if value not accepted
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*/
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bool checkAcceleration(float r, float v, float a);
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protected:
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/**
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* Send out telemetry information for the log and MAVLink.
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* @return true on success, false on error
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*/
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bool sendTelemetry();
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/**
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* Change the radius of the circle.
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* @param r desired new radius
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* @return true on success, false if value not accepted
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*/
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bool setRadius(const float r);
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/**
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* Change the velocity of the vehicle on the circle.
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* @param v desired new velocity
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* @return true on success, false if value not accepted
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*/
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bool setVelocity(const float v);
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private:
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/** generates setpoints to smoothly reach the closest point on the circle when starting from far away */
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void generate_circle_approach_setpoints(const matrix::Vector2f ¢er_to_position);
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/** generates xy setpoints to make the vehicle orbit */
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void generate_circle_setpoints(const matrix::Vector2f ¢er_to_position);
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/** generates yaw setpoints to control the vehicle's heading */
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void generate_circle_yaw_setpoints(const matrix::Vector2f ¢er_to_position);
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float _r = 0.f; /**< radius with which to orbit the target */
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float _v = 0.f; /**< clockwise tangential velocity for orbiting in m/s */
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matrix::Vector2f _center; /**< local frame coordinates of the center point */
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bool _in_circle_approach = false;
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StraightLine _circle_approach_line;
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// TODO: create/use parameters for limits
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const float _radius_min = 1.f;
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const float _radius_max = 100.f;
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const float _velocity_max = 10.f;
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const float _acceleration_max = 2.f;
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/** yaw behaviour during the orbit flight according to MAVLink's ORBIT_YAW_BEHAVIOUR enum */
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int _yaw_behaviour = orbit_status_s::ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TO_CIRCLE_CENTER;
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float _initial_heading = 0.f; /**< the heading of the drone when the orbit command was issued */
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SlewRateYaw<float> _slew_rate_yaw;
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uORB::Publication<orbit_status_s> _orbit_status_pub{ORB_ID(orbit_status)};
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DEFINE_PARAMETERS(
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(ParamFloat<px4::params::MPC_XY_CRUISE>) _param_mpc_xy_cruise, /**< cruise speed for circle approach */
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(ParamFloat<px4::params::MPC_YAWRAUTO_MAX>) _param_mpc_yawrauto_max
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)
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};
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