/**************************************************************************** * * Copyright (c) 2013, 2014 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 bottle_drop_params.c * Bottle drop parameters * * @author Dominik Juchli */ #include #include /** * Ground drag property * * This parameter encodes the ground drag coefficient and the corresponding * decrease in wind speed from the plane altitude to ground altitude. * * @unit unknown * @min 0.001 * @max 0.1 * @group Payload drop */ PARAM_DEFINE_FLOAT(BD_GPROPERTIES, 0.03f); /** * Plane turn radius * * The planes known minimal turn radius - use a higher value * to make the plane maneuver more distant from the actual drop * position. This is to ensure the wings are level during the drop. * * @unit meter * @min 30.0 * @max 500.0 * @group Payload drop */ PARAM_DEFINE_FLOAT(BD_TURNRADIUS, 120.0f); /** * Drop precision * * If the system is closer than this distance on passing over the * drop position, it will release the payload. This is a safeguard * to prevent a drop out of the required accuracy. * * @unit meter * @min 1.0 * @max 80.0 * @group Payload drop */ PARAM_DEFINE_FLOAT(BD_PRECISION, 30.0f); /** * Payload drag coefficient of the dropped object * * The drag coefficient (cd) is the typical drag * constant for air. It is in general object specific, * but the closest primitive shape to the actual object * should give good results: * http://en.wikipedia.org/wiki/Drag_coefficient * * @unit meter * @min 0.08 * @max 1.5 * @group Payload drop */ PARAM_DEFINE_FLOAT(BD_OBJ_CD, 0.1f); /** * Payload mass * * A typical small toy ball: * 0.025 kg * * OBC water bottle: * 0.6 kg * * @unit kilogram * @min 0.001 * @max 5.0 * @group Payload drop */ PARAM_DEFINE_FLOAT(BD_OBJ_MASS, 0.6f); /** * Payload front surface area * * A typical small toy ball: * (0.045 * 0.045) / 4.0 * pi = 0.001590 m^2 * * OBC water bottle: * (0.063 * 0.063) / 4.0 * pi = 0.003117 m^2 * * @unit m^2 * @min 0.001 * @max 0.5 * @group Payload drop */ PARAM_DEFINE_FLOAT(BD_OBJ_SURFACE, 0.00311724531f);