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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.
 */
package org.orekit.frames;

import java.io.Serializable;

import org.hipparchus.CalculusFieldElement;
import org.hipparchus.geometry.euclidean.threed.FieldRotation;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
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.MathUtils;
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.TimeScale;
import org.orekit.utils.Constants;

/** Terrestrial Intermediate Reference Frame.
 * 

The pole motion is not considered : Pseudo Earth Fixed Frame. It handles * the earth rotation angle, its parent frame is the {@link CIRFProvider}

*/ class TIRFProvider implements EOPBasedTransformProvider { /** Serializable UID. */ private static final long serialVersionUID = 20130919L; /** Angular velocity of the Earth, in rad/s. */ private static final double AVE = 7.292115146706979e-5; /** EOP history. */ private final EOPHistory eopHistory; /** UT1 time scale. */ private final transient TimeScale ut1; /** ERA function. */ private final transient TimeScalarFunction era; /** Simple constructor. * @param eopHistory EOP history * @param ut1 the UT1 time scale. */ protected TIRFProvider(final EOPHistory eopHistory, final TimeScale ut1) { this.ut1 = ut1; this.eopHistory = eopHistory; this.era = eopHistory.getConventions().getEarthOrientationAngleFunction( ut1, eopHistory.getTimeScales().getTAI()); } /** {@inheritDoc} */ @Override public EOPHistory getEOPHistory() { return eopHistory; } /** {@inheritDoc} */ @Override public TIRFProvider getNonInterpolatingProvider() { return new TIRFProvider(eopHistory.getNonInterpolatingEOPHistory(), ut1); } /** {@inheritDoc} */ @Override public Transform getTransform(final AbsoluteDate date) { // compute proper rotation final double correctedERA = era.value(date); // compute true angular rotation of Earth, in rad/s final double lod = (eopHistory == null) ? 0.0 : eopHistory.getLOD(date); final double omp = AVE * (1 - lod / Constants.JULIAN_DAY); final Vector3D rotationRate = new Vector3D(omp, Vector3D.PLUS_K); // set up the transform from parent CIRF final Rotation rotation = new Rotation(Vector3D.PLUS_K, correctedERA, RotationConvention.FRAME_TRANSFORM); return new Transform(date, rotation, rotationRate); } /** {@inheritDoc} */ @Override public StaticTransform getStaticTransform(final AbsoluteDate date) { // compute proper rotation final double correctedERA = era.value(date); // set up the transform from parent CIRF final Rotation rotation = new Rotation( Vector3D.PLUS_K, correctedERA, RotationConvention.FRAME_TRANSFORM); return StaticTransform.of(date, rotation); } /** {@inheritDoc} */ @Override public > FieldTransform getTransform(final FieldAbsoluteDate date) { // compute proper rotation final T correctedERA = era.value(date); // compute true angular rotation of Earth, in rad/s final T lod = (eopHistory == null) ? date.getField().getZero() : eopHistory.getLOD(date); final T omp = lod.divide(Constants.JULIAN_DAY).subtract(1).multiply(-AVE); final FieldVector3D rotationRate = new FieldVector3D<>(omp, Vector3D.PLUS_K); // set up the transform from parent CIRF final FieldRotation rotation = new FieldRotation<>(FieldVector3D.getPlusK(date.getField()), correctedERA, RotationConvention.FRAME_TRANSFORM); return new FieldTransform<>(date, rotation, rotationRate); } /** Get the Earth Rotation Angle at the current date. * @param date the date * @return Earth Rotation Angle at the current date in radians */ public double getEarthRotationAngle(final AbsoluteDate date) { return MathUtils.normalizeAngle(era.value(date), 0); } /** 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(eopHistory); } /** Internal class used only for serialization. */ @DefaultDataContext 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 TIRFProvider}. * @return replacement {@link TIRFProvider} */ private Object readResolve() { try { // retrieve a managed frame return new TIRFProvider(eopHistory, DataContext.getDefault().getTimeScales().getUT1(eopHistory)); } catch (OrekitException oe) { throw new OrekitInternalError(oe); } } } }




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