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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 2002-2019 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
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 * Unless required by applicable law or agreed to in writing, software
 * distributed under the License is distributed on an "AS IS" BASIS,
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 * See the License for the specific language governing permissions and
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package org.orekit.time;

import org.hipparchus.RealFieldElement;

/** International Atomic Time.
 * 

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

* @author Luc Maisonobe * @see AbsoluteDate */ public class TAIScale implements TimeScale { /** Serializable UID. */ private static final long serialVersionUID = 20131209L; /** Package private constructor for the factory. */ TAIScale() { } /** {@inheritDoc} */ @Override public double offsetFromTAI(final AbsoluteDate taiTime) { return 0; } /** {@inheritDoc} */ @Override public > T offsetFromTAI(final FieldAbsoluteDate date) { return date.getField().getZero(); } /** {@inheritDoc} */ @Override public double offsetToTAI(final DateComponents date, final TimeComponents time) { return 0; } /** {@inheritDoc} */ public String getName() { return "TAI"; } /** {@inheritDoc} */ public String toString() { return getName(); } }




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