KeplerianExtendedPositionProvider.java
/* Copyright 2022-2026 Romain Serra
* 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.orbits;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.Field;
import org.orekit.utils.AbstractExtendedPositionProvider;
import org.orekit.utils.PVCoordinates;
/**
* Position provider assuming pure Keplerian motion.
* Propagation is computed with the same orbital parameters used to define the reference.
*
* @author Romain Serra
* @see org.orekit.utils.ExtendedPositionProvider
* @see Orbit
* @see FieldOrbit
*
* @since 14.0
*/
public class KeplerianExtendedPositionProvider extends AbstractExtendedPositionProvider<Orbit> {
/**
* Constructor.
* @param referenceOrbit reference orbit (non-Keplerian terms will be ignored if any)
*/
public KeplerianExtendedPositionProvider(final Orbit referenceOrbit) {
// Remove non-Keplerian rates if any
super(referenceOrbit.getType().convertType(new CartesianOrbit(new PVCoordinates(referenceOrbit.getPosition(),
referenceOrbit.getVelocity()), referenceOrbit.getFrame(), referenceOrbit.getDate(), referenceOrbit.getMu())));
}
/** {@inheritDoc} */
@Override
protected <T extends CalculusFieldElement<T>> FieldOrbit<T> getFieldProvider(final Field<T> field) {
return getProvider().getType().convertToFieldOrbit(field, getProvider());
}
}