/**************************************************************************** * * Copyright (c) 2023 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. * ****************************************************************************/ /** * Maximal tilt angle in Stabilized or Altitude mode * * @unit deg * @min 1 * @max 70 * @decimal 0 * @increment 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_MAN_TILT_MAX, 35.f); /** * Max manual yaw rate for Stabilized, Altitude, Position mode * * @unit deg/s * @min 0 * @max 400 * @decimal 0 * @increment 10 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_MAN_Y_MAX, 150.f); /** * Minimum collective thrust in Stabilized mode * * The value is mapped to the lowest throttle stick position in Stabilized mode. * * Too low collective thrust leads to loss of roll/pitch/yaw torque control authority. * Airmode is used to keep torque authority with zero thrust (see MC_AIRMODE). * * @unit norm * @min 0 * @max 1 * @decimal 2 * @increment 0.01 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_MANTHR_MIN, 0.08f); /** * Thrust curve mapping in Stabilized Mode * * This parameter defines how the throttle stick input is mapped to collective thrust * in Stabilized mode. * * In case the default is used ('Rescale to hover thrust'), the stick input is linearly * rescaled, such that a centered stick corresponds to the hover throttle (see MPC_THR_HOVER). * * Select 'No Rescale' to directly map the stick 1:1 to the output. This can be useful * in case the hover thrust is very low and the default would lead to too much distortion * (e.g. if hover thrust is set to 20%, then 80% of the upper thrust range is squeezed into the * upper half of the stick range). * * Note: In case MPC_THR_HOVER is set to 50%, the modes 0 and 1 are the same. * * @value 0 Rescale to hover thrust * @value 1 No Rescale * @group Multicopter Position Control */ PARAM_DEFINE_INT32(MPC_THR_CURVE, 0);