/* Copyright 2002-2017 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (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.estimation;
import org.orekit.errors.OrekitException;
import org.orekit.propagation.SpacecraftState;
/** Interface representing the Jacobian of a vector function depending on {@link SpacecraftState}.
* @see EstimationUtils#differentiate(StateFunction, int, org.orekit.orbits.OrbitType, org.orekit.orbits.PositionAngle, double, int)
* @see StateFunction
* @author Luc Maisonobe
* @since 8.0
*/
public interface StateJacobian {
/** Evaluate the Jacobian of the function.
* @param state spacecraft state as the sole free parameter of the function.
* @return Jacobian matric
* @throws OrekitException if evaluation cannot be performed
*/
double[][] value(SpacecraftState state) throws OrekitException;
}