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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 ...).
/* Copyright 2002-2020 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.RealFieldElement;
/** International Atomic Time.
* This is intended to be accessed thanks to {@link TimeScales},
* 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();
}
}