/**************************************************************************** * * 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 CatapultLaunchMethod.cpp * Catapult Launch detection * * @author Thomas Gubler * */ #include "CatapultLaunchMethod.h" #include namespace launchdetection { CatapultLaunchMethod::CatapultLaunchMethod(SuperBlock *parent) : SuperBlock(parent, "CAT"), last_timestamp(hrt_absolute_time()), integrator(0.0f), state(LAUNCHDETECTION_RES_NONE), thresholdAccel(this, "A"), thresholdTime(this, "T"), motorDelay(this, "MDEL"), pitchMaxPreThrottle(this, "PMAX") { } CatapultLaunchMethod::~CatapultLaunchMethod() { } void CatapultLaunchMethod::update(float accel_x) { float dt = (float)hrt_elapsed_time(&last_timestamp) * 1e-6f; last_timestamp = hrt_absolute_time(); switch (state) { case LAUNCHDETECTION_RES_NONE: /* Detect a acceleration that is longer and stronger as the minimum given by the params */ if (accel_x > thresholdAccel.get()) { integrator += dt; if (integrator > thresholdTime.get()) { if (motorDelay.get() > 0.0f) { state = LAUNCHDETECTION_RES_DETECTED_ENABLECONTROL; warnx("Launch detected: state: enablecontrol, waiting %.2fs until using full" " throttle", (double)motorDelay.get()); } else { /* No motor delay set: go directly to enablemotors state */ state = LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS; warnx("Launch detected: state: enablemotors (delay not activated)"); } } } else { /* reset */ reset(); } break; case LAUNCHDETECTION_RES_DETECTED_ENABLECONTROL: /* Vehicle is currently controlling attitude but not with full throttle. Waiting undtil delay is * over to allow full throttle */ motorDelayCounter += dt; if (motorDelayCounter > motorDelay.get()) { warnx("Launch detected: state enablemotors"); state = LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS; } break; default: break; } } LaunchDetectionResult CatapultLaunchMethod::getLaunchDetected() const { return state; } void CatapultLaunchMethod::reset() { integrator = 0.0f; motorDelayCounter = 0.0f; state = LAUNCHDETECTION_RES_NONE; } float CatapultLaunchMethod::getPitchMax(float pitchMaxDefault) { /* If motor is turned on do not impose the extra limit on maximum pitch */ if (state == LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS) { return pitchMaxDefault; } else { return pitchMaxPreThrottle.get(); } } }