/* 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.frames; import org.hipparchus.geometry.euclidean.threed.Rotation; import org.hipparchus.geometry.euclidean.threed.RotationConvention; import org.hipparchus.geometry.euclidean.threed.Vector3D; import org.hipparchus.util.FastMath; import org.orekit.time.AbsoluteDate; import org.orekit.utils.Constants; /** EME2000 frame : mean equator at J2000.0. * <p>This frame was the standard inertial reference prior to GCRF. It was defined * using Lieske precession-nutation model for Earth. This frame has been superseded * by GCRF which is implicitly defined from a few hundred quasars coordinates. * <p>The transformation between GCRF and EME2000 is a constant rotation bias.</p> * @author Luc Maisonobe */ class EME2000Provider extends FixedTransformProvider { /** Serializable UID. */ private static final long serialVersionUID = -6134137187835219727L; /** Obliquity of the ecliptic. */ private static final double EPSILON_0 = 84381.448 * Constants.ARC_SECONDS_TO_RADIANS; /** Bias in longitude. */ private static final double D_PSI_B = -0.041775 * Constants.ARC_SECONDS_TO_RADIANS; /** Bias in obliquity. */ private static final double D_EPSILON_B = -0.0068192 * Constants.ARC_SECONDS_TO_RADIANS; /** Right Ascension of the 2000 equinox in ICRS frame. */ private static final double ALPHA_0 = -0.0146 * Constants.ARC_SECONDS_TO_RADIANS; /** Simple constructor. */ protected EME2000Provider() { // build the bias transform super(new Transform(AbsoluteDate.J2000_EPOCH, new Rotation(Vector3D.PLUS_I, D_EPSILON_B, RotationConvention.VECTOR_OPERATOR). compose(new Rotation(Vector3D.PLUS_J, -D_PSI_B * FastMath.sin(EPSILON_0), RotationConvention.VECTOR_OPERATOR). compose(new Rotation(Vector3D.PLUS_K, -ALPHA_0, RotationConvention.VECTOR_OPERATOR), RotationConvention.VECTOR_OPERATOR), RotationConvention.VECTOR_OPERATOR))); } }