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OREKIT 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 2002-2024 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.time;

import org.hipparchus.CalculusFieldElement;
import org.hipparchus.util.FastMath;
import org.orekit.utils.Constants;

/** Greenwich Mean Sidereal Time.
 * 

The Greenwich Mean Sidereal Time is the hour angle between the meridian of Greenwich * and mean equinox of date at 0h UT1.

*

This is intended to be accessed thanks to {@link TimeScales}, * so there is no public constructor.

* @author Luc Maisonobe * @see AbsoluteDate * @since 5.1 */ public class GMSTScale implements TimeScale { /** Serializable UID. */ private static final long serialVersionUID = 20131209L; /** Duration of one julian day. */ private static final double FULL_DAY = Constants.JULIAN_DAY; /** Duration of an half julian day. */ private static final double HALF_DAY = Constants.JULIAN_DAY / 2.0; /** Coefficient for degree 0. */ private static final double C0 = 24110.54841; /** Coefficient for degree 1. */ private static final double C1 = 8640184.812866; /** Coefficient for degree 2. */ private static final double C2 = 0.093104; /** Coefficient for degree 3. */ private static final double C3 = -0.0000062; /** Universal Time 1 time scale. */ private final UT1Scale ut1; /** Reference date for GMST. */ private final AbsoluteDate referenceDate; // GST 1982: 24110.54841 + 8640184.812866 t + 0.093104 t2 - 6.2e-6 t3 // GST 2000: 24110.5493771 + 8639877.3173760 tu + 307.4771600 te + 0.0931118 te2 - 0.0000062 te3 + 0.0000013 te4 /** Package private constructor for the factory. * @param ut1 Universal Time 1 scale */ GMSTScale(final UT1Scale ut1) { this.ut1 = ut1; this.referenceDate = new AbsoluteDate(2000, 1, 1, 12, 0, 0.0, ut1); } /** {@inheritDoc} */ @Override public double offsetFromTAI(final AbsoluteDate date) { // julian seconds since reference date final double ts = date.durationFrom(referenceDate); // julian centuries since reference date final double tc = ts / Constants.JULIAN_CENTURY; // GMST at 0h00 UT1 in seconds = offset with respect to UT1 final double gmst0h = C0 + tc * (C1 + tc * (C2 + tc * C3)); // offset with respect to TAI final double offset = gmst0h + ut1.offsetFromTAI(date); // normalize offset between -43200 and +43200 seconds return offset - FULL_DAY * FastMath.floor((offset + HALF_DAY) / FULL_DAY); } /** {@inheritDoc} */ @Override public > T offsetFromTAI(final FieldAbsoluteDate date) { // julian seconds since reference date final T ts = date.durationFrom(referenceDate); // julian centuries since reference date final T tc = ts.divide(Constants.JULIAN_CENTURY); // GMST at 0h00 UT1 in seconds = offset with respect to UT1 final T gmst0h = tc.multiply(C3).add(C2).multiply(tc).add(C1).multiply(tc).add(C0); // offset with respect to TAI final T offset = gmst0h.add(ut1.offsetFromTAI(date)); // normalize offset between -43200 and +43200 seconds return offset.subtract(FULL_DAY * FastMath.floor((offset.getReal() + HALF_DAY) / FULL_DAY)); } /** {@inheritDoc} */ public String getName() { return "GMST"; } /** {@inheritDoc} */ public String toString() { return getName(); } }




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