/* 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; }