/**************************************************************************** * * Copyright (c) 2018 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 FlightTaskManualPosition.cpp */ #include "FlightTaskManualPosition.hpp" #include #include using namespace matrix; void FlightTaskManualPosition::_scaleSticks() { /* Use same scaling as for FlightTaskManualAltitude */ FlightTaskManualAltitude::_scaleSticks(); /* Constrain length of stick inputs to 1 for xy*/ Vector2f stick_xy(_sticks_expo(0), _sticks_expo(1)); float mag = math::constrain(stick_xy.length(), 0.0f, 1.0f); if (mag > FLT_EPSILON) { stick_xy = stick_xy.normalized() * mag; } // scale velocity to its maximum lmits Vector2f vel_sp_xy = stick_xy * _limits.speed_NE_max; /* Rotate setpoint into local frame. */ _rotateIntoHeadingFrame(vel_sp_xy); _velocity_setpoint(0) = vel_sp_xy(0); _velocity_setpoint(1) = vel_sp_xy(1); } void FlightTaskManualPosition::_updateXYlock() { /* If position lock is not active, position setpoint is set to NAN.*/ const float vel_xy_norm = Vector2f(&_velocity(0)).length(); const bool apply_brake = Vector2f(&_velocity_setpoint(0)).length() < FLT_EPSILON; const bool stopped = (MPC_HOLD_MAX_XY.get() < FLT_EPSILON || vel_xy_norm < MPC_HOLD_MAX_XY.get()); if (apply_brake && stopped && !PX4_ISFINITE(_position_setpoint(0))) { _position_setpoint(0) = _position(0); _position_setpoint(1) = _position(1); } else if (!apply_brake) { /* don't lock*/ _position_setpoint(0) = NAN; _position_setpoint(1) = NAN; } } void FlightTaskManualPosition::_updateSetpoints() { FlightTaskManualAltitude::_updateSetpoints(); // needed to get yaw and setpoints in z-direction _thrust_setpoint *= NAN; // don't require any thrust setpoints _updateXYlock(); // check for position lock } void FlightTaskManualPosition::_updateSetpointLimits() { FlightTaskManualAltitude::_updateSetpointLimits(); if (_limits.speed_NE_max >= MPC_VEL_MANUAL.get()) { _limits.speed_NE_max = MPC_VEL_MANUAL.get(); } }