TODProvider.java
/* Copyright 2002-2013 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.orekit.errors.OrekitException;
import org.orekit.errors.TimeStampedCacheException;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeFunction;
import org.orekit.utils.IERSConventions;
/** Provider for True of Date (ToD) frame.
* <p>This frame handles nutation effects according to selected IERS conventions.</p>
* <p>Transform is computed with reference to the {@link MODProvider Mean of Date} frame.</p>
* @author Pascal Parraud
*/
class TODProvider implements TransformProvider {
/** Serializable UID. */
private static final long serialVersionUID = 20131209L;
/** Conventions. */
private final IERSConventions conventions;
/** EOP history. */
private final EOPHistory eopHistory;
/** Function computing the mean obliquity. */
private final transient TimeFunction<Double> obliquityFunction;
/** Function computing the nutation angles. */
private final transient TimeFunction<double[]> nutationFunction;
/** Simple constructor.
* @param conventions IERS conventions to apply
* @param eopHistory EOP history
* @exception OrekitException if IERS conventions tables cannot be read
*/
public TODProvider(final IERSConventions conventions, final EOPHistory eopHistory)
throws OrekitException {
this.conventions = conventions;
this.eopHistory = eopHistory;
this.obliquityFunction = conventions.getMeanObliquityFunction();
this.nutationFunction = conventions.getNutationFunction();
}
/** Get the EOP history.
* @return EOP history
*/
EOPHistory getEOPHistory() {
return eopHistory;
}
/** Get the LoD (Length of Day) value.
* <p>The data provided comes from the IERS files. It is smoothed data.</p>
* @param date date at which the value is desired
* @return LoD in seconds (0 if date is outside covered range)
* @exception TimeStampedCacheException if EOP data cannot be retrieved
*/
double getLOD(final AbsoluteDate date) throws TimeStampedCacheException {
return (eopHistory == null) ? 0.0 : eopHistory.getLOD(date);
}
/** Get the pole IERS Reference Pole correction.
* <p>The data provided comes from the IERS files. It is smoothed data.</p>
* @param date date at which the correction is desired
* @return pole correction ({@link PoleCorrection#NULL_CORRECTION
* PoleCorrection.NULL_CORRECTION} if date is outside covered range)
*/
public PoleCorrection getPoleCorrection(final AbsoluteDate date) {
return (eopHistory == null) ? PoleCorrection.NULL_CORRECTION : eopHistory.getPoleCorrection(date);
}
/** Get the transform from Mean Of Date at specified date.
* <p>The update considers the nutation 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 {
// compute nutation angles
final double[] angles = nutationFunction.value(date);
// compute the mean obliquity of the ecliptic
final double moe = obliquityFunction.value(date);
double dpsi = angles[0];
double deps = angles[1];
if (eopHistory != null) {
// apply the corrections for the nutation parameters
final double[] correction = eopHistory.getEquinoxNutationCorrection(date);
dpsi += correction[0];
deps += correction[1];
}
// compute the true obliquity of the ecliptic
final double toe = moe + deps;
// set up the elementary rotations for nutation
final Rotation r1 = new Rotation(Vector3D.PLUS_I, toe);
final Rotation r2 = new Rotation(Vector3D.PLUS_K, dpsi);
final Rotation r3 = new Rotation(Vector3D.PLUS_I, -moe);
// complete nutation
final Rotation nutation = r1.applyTo(r2.applyTo(r3));
// set up the transform from parent MOD
return new Transform(date, nutation);
}
/** 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(conventions, eopHistory);
}
/** Internal class used only for serialization. */
private static class DataTransferObject implements Serializable {
/** Serializable UID. */
private static final long serialVersionUID = 20131209L;
/** Conventions. */
private final IERSConventions conventions;
/** EOP history. */
private final EOPHistory eopHistory;
/** Simple constructor.
* @param conventions IERS conventions to apply
* @param eopHistory EOP history
*/
public DataTransferObject(final IERSConventions conventions, final EOPHistory eopHistory) {
this.conventions = conventions;
this.eopHistory = eopHistory;
}
/** Replace the deserialized data transfer object with a {@link TODProvider}.
* @return replacement {@link TODProvider}
*/
private Object readResolve() {
try {
// retrieve a managed frame
return new TODProvider(conventions, eopHistory);
} catch (OrekitException oe) {
throw OrekitException.createInternalError(oe);
}
}
}
}