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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.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();

}