/**************************************************************************** * * 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 FlightManualStabilized.cpp */ #include "FlightTaskManualStabilized.hpp" #include #include using namespace matrix; bool FlightTaskManualStabilized::activate() { bool ret = FlightTaskManual::activate(); _thrust_setpoint = matrix::Vector3f(0.0f, 0.0f, -_throttle_hover.get()); _yaw_setpoint = _yaw; _yawspeed_setpoint = 0.0f; _constraints.tilt = math::radians(_tilt_max_man.get()); return ret; } bool FlightTaskManualStabilized::updateInitialize() { bool ret = FlightTaskManual::updateInitialize(); // need a valid yaw-state return ret && PX4_ISFINITE(_yaw); } void FlightTaskManualStabilized::_scaleSticks() { /* Scale sticks to yaw and thrust using * linear scale for yaw and piecewise linear map for thrust. */ _yawspeed_setpoint = _sticks_expo(3) * math::radians(_yaw_rate_scaling.get()); _throttle = _throttleCurve(); } void FlightTaskManualStabilized::_updateHeadingSetpoints() { /* Yaw-lock depends on stick input. If not locked, * yaw_sp is set to NAN. * TODO: add yawspeed to get threshold.*/ if (fabsf(_yawspeed_setpoint) > FLT_EPSILON) { // no fixed heading when rotating around yaw by stick _yaw_setpoint = NAN; } else { // hold the current heading when no more rotation commanded if (!PX4_ISFINITE(_yaw_setpoint)) { _yaw_setpoint = _yaw; } else { // check reset counter and update yaw setpoint if necessary if (_sub_attitude->get().quat_reset_counter != _heading_reset_counter) { _yaw_setpoint += matrix::Eulerf(matrix::Quatf(_sub_attitude->get().delta_q_reset)).psi(); _heading_reset_counter = _sub_attitude->get().quat_reset_counter; } } } // check if an external yaw handler is active and if yes, let it compute the yaw setpoints if (_ext_yaw_handler != nullptr && _ext_yaw_handler->is_active()) { _yaw_setpoint = NAN; _yawspeed_setpoint += _ext_yaw_handler->get_weathervane_yawrate(); } } void FlightTaskManualStabilized::_updateThrustSetpoints() { /* Rotate setpoint into local frame. */ Vector2f sp(&_sticks(0)); _rotateIntoHeadingFrame(sp); /* Ensure that maximum tilt is in [0.001, Pi] */ float tilt_max = math::constrain(_constraints.tilt, 0.001f, M_PI_F); const float x = sp(0) * tilt_max; const float y = sp(1) * tilt_max; /* The norm of the xy stick input provides the pointing * direction of the horizontal desired thrust setpoint. The magnitude of the * xy stick inputs represents the desired tilt. Both tilt and magnitude can * be captured through Axis-Angle. */ /* The Axis-Angle is the perpendicular vector to xy-stick input */ Vector2f v = Vector2f(y, -x); float v_norm = v.norm(); // the norm of v defines the tilt angle if (v_norm > tilt_max) { // limit to the configured maximum tilt angle v *= tilt_max / v_norm; } /* The final thrust setpoint is found by rotating the scaled unit vector pointing * upward by the Axis-Angle. * Make sure that the attitude can be controlled even at 0 throttle. */ Quatf q_sp = AxisAnglef(v(0), v(1), 0.0f); _thrust_setpoint = q_sp.conjugate(Vector3f(0.0f, 0.0f, -1.0f)) * math::max(_throttle, 0.0001f); } void FlightTaskManualStabilized::_rotateIntoHeadingFrame(Vector2f &v) { float yaw_rotate = PX4_ISFINITE(_yaw_setpoint) ? _yaw_setpoint : _yaw; Vector3f v_r = Vector3f(Dcmf(Eulerf(0.0f, 0.0f, yaw_rotate)) * Vector3f(v(0), v(1), 0.0f)); v(0) = v_r(0); v(1) = v_r(1); } void FlightTaskManualStabilized::_updateSetpoints() { _updateHeadingSetpoints(); _updateThrustSetpoints(); } float FlightTaskManualStabilized::_throttleCurve() { // Scale stick z from [-1,1] to [min thrust, max thrust] float throttle = -((_sticks(2) - 1.0f) * 0.5f); switch (_throttle_curve.get()) { case 1: // no rescaling return throttle; default: // 0 or other: rescale to hover throttle at 0.5 stick if (throttle < 0.5f) { return (_throttle_hover.get() - _throttle_min_stabilized.get()) / 0.5f * throttle + _throttle_min_stabilized.get(); } else { return (_throttle_max.get() - _throttle_hover.get()) / 0.5f * (throttle - 1.0f) + _throttle_max.get(); } } } bool FlightTaskManualStabilized::update() { _scaleSticks(); _updateSetpoints(); return true; }