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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 2002-2021 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,
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 * See the License for the specific language governing permissions and
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package org.orekit.attitudes;

import org.orekit.time.AbsoluteDate;

/** This interface is intended for attitude ephemerides valid only during a time range.
*
* 

This interface provides a mean to retrieve an attitude at * any time within a given range. It should be implemented by attitude readers * based on external data files.

* * @author Bryan Cazabonne * @since 10.3 */ public interface BoundedAttitudeProvider extends AttitudeProvider { /** Get the first date of the range. * @return the first date of the range */ AbsoluteDate getMinDate(); /** Get the last date of the range. * @return the last date of the range */ AbsoluteDate getMaxDate(); }




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