Java tutorial
/* Copyright 2002-2008 CS Communication & Systmes * Licensed to CS Communication & Systmes (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.frames; import org.apache.commons.math.geometry.Rotation; import org.apache.commons.math.geometry.Vector3D; import org.orekit.errors.OrekitException; import org.orekit.time.AbsoluteDate; import org.orekit.time.DateComponents; import org.orekit.time.TimeScalesFactory; import org.orekit.utils.Constants; /** Veis 1950 Frame. * <p>Its parent frame is the {@link PEFFrame} without EOP correction application.<p> * <p>This frame is mainly provided for consistency with legacy softwares.</p> * @author Pascal Parraud * @version $Revision$ $Date$ */ class VEISFrame extends Frame { /** Serializable UID. */ private static final long serialVersionUID = -8200570473557338686L; /** 2π. */ private static final double TWO_PI = 2.0 * Math.PI; /** Reference date. */ private static AbsoluteDate VST_REFERENCE = new AbsoluteDate(DateComponents.FIFTIES_EPOCH, TimeScalesFactory.getTAI()); /** 1st coef for Veis sidereal time computation in radians (100.075542 deg). */ private static final double VST0 = 1.746647708617871; /** 2nd coef for Veis sidereal time computation in rad/s (0.985612288 deg/s). */ private static final double VST1 = 0.17202179573714597e-1; /** Veis sidereal time derivative in rad/s. */ private static final double VSTD = 7.292115146705209e-5; /** Cached date to avoid useless calculus. */ private AbsoluteDate cachedDate; /** EOP history. */ private final EOP1980History eopHistory; /** Constructor for the singleton. * @param date the date. * @param name name of the frame * @exception OrekitException if data embedded in the library cannot be read */ public VEISFrame(final AbsoluteDate date, final String name) throws OrekitException { super(FramesFactory.getPEF(false), null, name, true); eopHistory = FramesFactory.getEOP1980History(); // frame synchronization updateFrame(date); } /** Update the frame to the given date. * @param date new value of the date * @exception OrekitException if data embedded in the library cannot be read */ protected void updateFrame(final AbsoluteDate date) throws OrekitException { if ((cachedDate == null) || !cachedDate.equals(date)) { // offset from FIFTIES epoch (UT1 scale) final double dtai = date.durationFrom(VST_REFERENCE); final double dutc = TimeScalesFactory.getUTC().offsetFromTAI(date); final double dut1 = eopHistory.getUT1MinusUTC(date); final double tut1 = dtai + dutc + dut1; final double ttd = tut1 / Constants.JULIAN_DAY; final double rdtt = ttd - (int) ttd; // compute Veis sidereal time, in radians final double vst = (VST0 + VST1 * ttd + TWO_PI * rdtt) % TWO_PI; // compute angular rotation of Earth, in rad/s final Vector3D rotationRate = new Vector3D(-VSTD, Vector3D.PLUS_K); // set up the transform from parent PEF setTransform(new Transform(new Rotation(Vector3D.PLUS_K, vst), rotationRate)); cachedDate = date; } } }