/**************************************************************************** * * Copyright (c) 2017 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.cpp */ #include "FlightTaskOrbit.hpp" #include using namespace matrix; FlightTaskOrbit::FlightTaskOrbit(control::SuperBlock *parent, const char *name) : FlightTaskManual(parent, name) { _sticks_data_required = false; } bool FlightTaskOrbit::applyCommandParameters(const vehicle_command_s &command) { const float &r = command.param3; /**< commanded radius */ const float &v = command.param4; /**< commanded velocity */ if (math::isInRange(r, 5.f, 50.f) && fabs(v) < 10.f) { _r = r; _v = v; return FlightTaskManual::applyCommandParameters(command); } return false; } bool FlightTaskOrbit::activate() { bool ret = FlightTaskManual::activate(); _r = 1.f; _v = 0.5f; _z = _position(2); _center = Vector2f(_position.data()); _center(0) -= _r; return ret; } bool FlightTaskOrbit::update() { _r += _sticks_expo(0) * _deltatime; _r = math::constrain(_r, 1.f, 20.f); _v -= _sticks_expo(1) * _deltatime; _v = math::constrain(_v, -7.f, 7.f); _z += _sticks_expo(2) * _deltatime; Vector2f center_to_position = Vector2f(_position.data()) - _center; /* xy velocity to go around in a circle */ Vector2f velocity_xy = Vector2f(center_to_position(1), -center_to_position(0)); velocity_xy = velocity_xy.unit_or_zero(); velocity_xy *= _v; /* xy velocity adjustment to stay on the radius distance */ velocity_xy += (_r - center_to_position.norm()) * center_to_position.unit_or_zero(); float yaw = atan2f(center_to_position(1), center_to_position(0)) + M_PI_F; _setPositionSetpoint(Vector3f(NAN, NAN, _z)); _setVelocitySetpoint(Vector3f(velocity_xy(0), velocity_xy(1), 0.f)); _setYawSetpoint(yaw); return true; }