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OREKIT (ORbits Extrapolation KIT) is a low level space dynamics library. It provides basic elements (orbits, dates, attitude, frames ...) and various algorithms to handle them (conversions, analytical and numerical propagation, pointing ...).

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/* Copyright 2002-2022 CS GROUP
 * Licensed to CS GROUP (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.
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package org.orekit.frames;

import java.io.Serializable;
import java.util.HashMap;
import java.util.Map;

import org.hipparchus.Field;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.geometry.euclidean.threed.FieldRotation;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.RotationConvention;
import org.hipparchus.geometry.euclidean.threed.RotationOrder;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.annotation.DefaultDataContext;
import org.orekit.data.DataContext;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitInternalError;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
import org.orekit.time.TimeScalarFunction;
import org.orekit.time.TimeScales;
import org.orekit.time.TimeVectorFunction;
import org.orekit.utils.IERSConventions;

/** Mean Equator, Mean Equinox Frame.
 * 

This frame handles precession effects according to to selected IERS conventions.

*

Its parent frame is the GCRF frame. *

It is sometimes called Mean of Date (MoD) frame. * @author Pascal Parraud */ class MODProvider implements TransformProvider { /** Serializable UID. */ private static final long serialVersionUID = 20130920L; /** Conventions. */ private final IERSConventions conventions; /** Function computing the precession angles. */ private final transient TimeVectorFunction precessionFunction; /** Constant rotation between ecliptic and equator poles at J2000.0. */ private final Rotation r4; /** Constant rotations between ecliptic and equator poles at J2000.0. */ private final transient Map>, FieldRotation>> fieldR4; /** Simple constructor. * @param conventions IERS conventions to apply * @param timeScales used to define this frame. */ MODProvider(final IERSConventions conventions, final TimeScales timeScales) { this.conventions = conventions; this.precessionFunction = conventions.getPrecessionFunction(timeScales); final TimeScalarFunction epsilonAFunction = conventions.getMeanObliquityFunction(timeScales); final AbsoluteDate date0 = conventions.getNutationReferenceEpoch(timeScales); final double epsilon0 = epsilonAFunction.value(date0); r4 = new Rotation(Vector3D.PLUS_I, epsilon0, RotationConvention.FRAME_TRANSFORM); fieldR4 = new HashMap<>(); } /** {@inheritDoc} */ @Override public Transform getTransform(final AbsoluteDate date) { // compute the precession angles phiA, omegaA, chiA final double[] angles = precessionFunction.value(date); // complete precession final Rotation precession = r4.compose(new Rotation(RotationOrder.ZXZ, RotationConvention.FRAME_TRANSFORM, -angles[0], -angles[1], angles[2]), RotationConvention.FRAME_TRANSFORM); // set up the transform from parent GCRF return new Transform(date, precession); } /** {@inheritDoc} */ @Override public > FieldTransform getTransform(final FieldAbsoluteDate date) { // compute the precession angles phiA, omegaA, chiA final T[] angles = precessionFunction.value(date); @SuppressWarnings("unchecked") FieldRotation fR4 = (FieldRotation) fieldR4.get(date.getField()); if (fR4 == null) { fR4 = new FieldRotation<>(date.getField(), r4); fieldR4.put(date.getField(), fR4); } // complete precession final FieldRotation precession = fR4.compose(new FieldRotation<>(RotationOrder.ZXZ, RotationConvention.FRAME_TRANSFORM, angles[0].negate(), angles[1].negate(), angles[2]), RotationConvention.FRAME_TRANSFORM); // set up the transform from parent GCRF return new FieldTransform<>(date, precession); } /** Replace the instance with a data transfer object for serialization. *

* This intermediate class serializes only the frame key. *

* @return data transfer object that will be serialized */ @DefaultDataContext private Object writeReplace() { return new DataTransferObject(conventions); } /** Internal class used only for serialization. */ @DefaultDataContext private static class DataTransferObject implements Serializable { /** Serializable UID. */ private static final long serialVersionUID = 20131209L; /** Conventions. */ private final IERSConventions conventions; /** Simple constructor. * @param conventions IERSConventions conventions */ DataTransferObject(final IERSConventions conventions) { this.conventions = conventions; } /** Replace the deserialized data transfer object with a {@link MODProvider}. * @return replacement {@link MODProvider} */ private Object readResolve() { try { // retrieve a managed frame return new MODProvider(conventions, DataContext.getDefault().getTimeScales()); } catch (OrekitException oe) { throw new OrekitInternalError(oe); } } } }




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