CIRFProvider.java
/* Copyright 2002-2016 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 java.io.Serializable;
import org.apache.commons.math3.geometry.euclidean.threed.Rotation;
import org.apache.commons.math3.geometry.euclidean.threed.Vector3D;
import org.apache.commons.math3.util.FastMath;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitInternalError;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeFunction;
/** Celestial Intermediate Reference Frame 2000.
* <p>This provider includes precession effects according to either the IAU 2006 precession
* (also known as Nicole Capitaines's P03 precession theory) and IAU 2000A_R06 nutation
* for IERS 2010 conventions or the IAU 2000A precession-nutation model for IERS 2003
* conventions. These models replaced the older IAU-76 precession (Lieske) and IAU-80
* theory of nutation (Wahr) which were used in the classical equinox-based paradigm.
* It <strong>must</strong> be used with the Earth Rotation Angle (REA) defined by
* Capitaine's model and <strong>not</strong> IAU-82 sidereal
* time which is consistent with the older models only.</p>
* <p>Its parent frame is the GCRF frame.<p>
*/
class CIRFProvider implements EOPBasedTransformProvider {
/** Serializable UID. */
private static final long serialVersionUID = 20130806L;
/** Function computing CIP/CIO components. */
private final transient TimeFunction<double[]> xysPxy2Function;
/** EOP history. */
private final EOPHistory eopHistory;
/** Simple constructor.
* @param eopHistory EOP history
* @exception OrekitException if the nutation model data embedded in the
* library cannot be read.
* @see Frame
*/
CIRFProvider(final EOPHistory eopHistory)
throws OrekitException {
// load the nutation model
xysPxy2Function = eopHistory.getConventions().getXYSpXY2Function();
// store correction to the model
this.eopHistory = eopHistory;
}
/** {@inheritDoc} */
@Override
public EOPHistory getEOPHistory() {
return eopHistory;
}
/** {@inheritDoc} */
@Override
public CIRFProvider getNonInterpolatingProvider()
throws OrekitException {
return new CIRFProvider(eopHistory.getNonInterpolatingEOPHistory());
}
/** Get the transform from GCRF to CIRF2000 at the specified date.
* <p>The transform considers the nutation and precession effects from IERS data.</p>
* @param date new value of the date
* @return transform at the specified date
* @exception OrekitException if the nutation model data embedded in the
* library cannot be read
*/
public Transform getTransform(final AbsoluteDate date) throws OrekitException {
final double[] xys = xysPxy2Function.value(date);
final double[] dxdy = eopHistory.getNonRotatinOriginNutationCorrection(date);
// position of the Celestial Intermediate Pole (CIP)
final double xCurrent = xys[0] + dxdy[0];
final double yCurrent = xys[1] + dxdy[1];
// position of the Celestial Intermediate Origin (CIO)
final double sCurrent = xys[2] - xCurrent * yCurrent / 2;
// set up the bias, precession and nutation rotation
final double x2Py2 = xCurrent * xCurrent + yCurrent * yCurrent;
final double zP1 = 1 + FastMath.sqrt(1 - x2Py2);
final double r = FastMath.sqrt(x2Py2);
final double sPe2 = 0.5 * (sCurrent + FastMath.atan2(yCurrent, xCurrent));
final double cos = FastMath.cos(sPe2);
final double sin = FastMath.sin(sPe2);
final double xPr = xCurrent + r;
final double xPrCos = xPr * cos;
final double xPrSin = xPr * sin;
final double yCos = yCurrent * cos;
final double ySin = yCurrent * sin;
final Rotation bpn = new Rotation(zP1 * (xPrCos + ySin), -r * (yCos + xPrSin),
r * (xPrCos - ySin), zP1 * (yCos - xPrSin),
true);
return new Transform(date, bpn, Vector3D.ZERO);
}
/** Replace the instance with a data transfer object for serialization.
* <p>
* This intermediate class serializes only the frame key.
* </p>
* @return data transfer object that will be serialized
*/
private Object writeReplace() {
return new DataTransferObject(eopHistory);
}
/** Internal class used only for serialization. */
private static class DataTransferObject implements Serializable {
/** Serializable UID. */
private static final long serialVersionUID = 20131209L;
/** EOP history. */
private final EOPHistory eopHistory;
/** Simple constructor.
* @param eopHistory EOP history
*/
DataTransferObject(final EOPHistory eopHistory) {
this.eopHistory = eopHistory;
}
/** Replace the deserialized data transfer object with a {@link CIRFProvider}.
* @return replacement {@link CIRFProvider}
*/
private Object readResolve() {
try {
// retrieve a managed frame
return new CIRFProvider(eopHistory);
} catch (OrekitException oe) {
throw new OrekitInternalError(oe);
}
}
}
}