J2SquaredModel.java
/* Copyright 2022 Bryan Cazabonne
* 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.
* Bryan Cazabonne 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.propagation.semianalytical.dsst.forces;
import org.hipparchus.CalculusFieldElement;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.PropagationType;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements;
import org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements;
import java.util.Collections;
import java.util.List;
/**
* Semi-analytical J2-squared model.
* <p>
* This interface is implemented by models providing J2-squared
* second-order terms in equinoctial elements. These terms are
* used in the computation of the closed-form J2-squared perturbation
* in semi-analytical satellite theory.
* </p>
* @see ZeisModel
* @author Bryan Cazabonne
* @since 12.0
*/
public interface J2SquaredModel {
/**
* Compute the J2-squared second-order terms in equinoctial elements.
* @param context model context
* @return the J2-squared second-order terms in equinoctial elements.
* Order must follow: [A, K, H, Q, P, M]
*/
double[] computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext context);
/**
* Compute the J2-squared second-order terms in equinoctial elements.
* @param context model context
* @param <T> type of the elements
* @return the J2-squared second-order terms in equinoctial elements.
* Order must follow: [A, K, H, Q, P, M]
*/
<T extends CalculusFieldElement<T>> T[] computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T> context);
/**
* Performs initialization of J2-squared short period terms prior to propagation.
* @param auxiliaryElements auxiliary elements
* @param type type of the elements used (MEAN or OSCULATING)
* @param parameters force model parameters
* @return a list containing the initialized short period terms
* @since 12.2
*/
default List<ShortPeriodTerms> initializeShortPeriodTerms(final AuxiliaryElements auxiliaryElements,
final PropagationType type,
final double[] parameters) {
return Collections.emptyList();
}
/**
* Performs initialization of J2-squared short period terms prior to propagation.
* @param auxiliaryElements auxiliary elements
* @param type type of the orbital elements used (MEAN or OSCULATING)
* @param parameters force model parameters
* @param <T> type of the field elements
* @return a list containing the initialized short period terms
* @since 12.2
*/
default <T extends CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>> initializeShortPeriodTerms(final FieldAuxiliaryElements<T> auxiliaryElements,
final PropagationType type,
final T[] parameters) {
return Collections.emptyList();
}
/** Update the J2-squared short period terms.
* <p>
* The {@link ShortPeriodTerms short period terms} that will be updated
* are the ones that were returned during the call to {@link
* #initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[])}.
* </p>
* @param parameters force model parameters
* @param meanStates mean states information: date, kinematics, attitude
* @since 12.2
*/
default void updateShortPeriodTerms(final double[] parameters, final SpacecraftState... meanStates) {
// Does nothing by default
}
/** Update the J2-squared short period terms.
* <p>
* The {@link ShortPeriodTerms short period terms} that will be updated
* are the ones that were returned during the call to {@link
* #initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[])}.
* </p>
* @param parameters force model parameters
* @param meanStates mean states information: date, kinematics, attitude
* @param <T> type of the field elements
* @since 12.2
*/
@SuppressWarnings("unchecked")
default <T extends CalculusFieldElement<T>> void updateShortPeriodTerms(final T[] parameters, final FieldSpacecraftState<T>... meanStates) {
// Does nothing by default
}
}