/* Copyright 2002-2017 CS Systèmes d'Information * Licensed to CS Systèmes d'Information (CS) under one or more * contributor license agreements. See the NOTICE file distributed with * this work for additional information regarding copyright ownership. * CS licenses this file to You under the Apache License, Version 2.0 * (the "License"); you may not use this file except in compliance with * the License. You may obtain a copy of the License at * * http://www.apache.org/licenses/LICENSE-2.0 * * Unless required by applicable law or agreed to in writing, software * distributed under the License is distributed on an "AS IS" BASIS, * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied. * See the License for the specific language governing permissions and * limitations under the License. */ package org.orekit.propagation.events; import org.orekit.bodies.OneAxisEllipsoid; import org.orekit.bodies.GeodeticPoint; import org.orekit.errors.OrekitException; import org.orekit.propagation.SpacecraftState; import org.orekit.propagation.events.handlers.EventHandler; import org.orekit.propagation.events.handlers.StopOnIncreasing; /** Detector for geographic latitude crossing. * <p>This detector identifies when a spacecraft crosses a fixed * latitude with respect to a central body.</p> * @author Luc Maisonobe * @since 7.1 */ public class LatitudeCrossingDetector extends AbstractDetector<LatitudeCrossingDetector> { /** Serializable UID. */ private static final long serialVersionUID = 20150824L; /** Body on which the latitude is defined. */ private OneAxisEllipsoid body; /** Fixed latitude to be crossed. */ private final double latitude; /** Build a new detector. * <p>The new instance uses default values for maximal checking interval * ({@link #DEFAULT_MAXCHECK}) and convergence threshold ({@link * #DEFAULT_THRESHOLD}).</p> * @param body body on which the latitude is defined * @param latitude latitude to be crossed */ public LatitudeCrossingDetector(final OneAxisEllipsoid body, final double latitude) { this(DEFAULT_MAXCHECK, DEFAULT_THRESHOLD, body, latitude); } /** Build a detector. * @param maxCheck maximal checking interval (s) * @param threshold convergence threshold (s) * @param body body on which the latitude is defined * @param latitude latitude to be crossed */ public LatitudeCrossingDetector(final double maxCheck, final double threshold, final OneAxisEllipsoid body, final double latitude) { this(maxCheck, threshold, DEFAULT_MAX_ITER, new StopOnIncreasing<LatitudeCrossingDetector>(), body, latitude); } /** Private constructor with full parameters. * <p> * This constructor is private as users are expected to use the builder * API with the various {@code withXxx()} methods to set up the instance * in a readable manner without using a huge amount of parameters. * </p> * @param maxCheck maximum checking interval (s) * @param threshold convergence threshold (s) * @param maxIter maximum number of iterations in the event time search * @param handler event handler to call at event occurrences * @param body body on which the latitude is defined * @param latitude latitude to be crossed */ private LatitudeCrossingDetector(final double maxCheck, final double threshold, final int maxIter, final EventHandler<? super LatitudeCrossingDetector> handler, final OneAxisEllipsoid body, final double latitude) { super(maxCheck, threshold, maxIter, handler); this.body = body; this.latitude = latitude; } /** {@inheritDoc} */ @Override protected LatitudeCrossingDetector create(final double newMaxCheck, final double newThreshold, final int newMaxIter, final EventHandler<? super LatitudeCrossingDetector> newHandler) { return new LatitudeCrossingDetector(newMaxCheck, newThreshold, newMaxIter, newHandler, body, latitude); } /** Get the body on which the geographic zone is defined. * @return body on which the geographic zone is defined */ public OneAxisEllipsoid getBody() { return body; } /** Get the fixed latitude to be crossed (radians). * @return fixed latitude to be crossed (radians) */ public double getLatitude() { return latitude; } /** Compute the value of the detection function. * <p> * The value is the spacecraft latitude minus the fixed latitude to be crossed. * It is positive if the spacecraft is northward and negative if it is southward * with respect to the fixed latitude. * </p> * @param s the current state information: date, kinematics, attitude * @return spacecraft latitude minus the fixed latitude to be crossed * @exception OrekitException if some specific error occurs */ public double g(final SpacecraftState s) throws OrekitException { // convert state to geodetic coordinates final GeodeticPoint gp = body.transform(s.getPVCoordinates().getPosition(), s.getFrame(), s.getDate()); // latitude difference return gp.getLatitude() - latitude; } }