ODEIntegratorBuilder.java

  1. /* Copyright 2002-2024 CS GROUP
  2.  * Licensed to CS GROUP (CS) under one or more
  3.  * contributor license agreements.  See the NOTICE file distributed with
  4.  * this work for additional information regarding copyright ownership.
  5.  * CS licenses this file to You under the Apache License, Version 2.0
  6.  * (the "License"); you may not use this file except in compliance with
  7.  * the License.  You may obtain a copy of the License at
  8.  *
  9.  *   http://www.apache.org/licenses/LICENSE-2.0
  10.  *
  11.  * Unless required by applicable law or agreed to in writing, software
  12.  * distributed under the License is distributed on an "AS IS" BASIS,
  13.  * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
  14.  * See the License for the specific language governing permissions and
  15.  * limitations under the License.
  16.  */
  17. package org.orekit.propagation.conversion;

  18. import org.hipparchus.ode.AbstractIntegrator;
  19. import org.orekit.orbits.CartesianOrbit;
  20. import org.orekit.orbits.Orbit;
  21. import org.orekit.orbits.OrbitType;
  22. import org.orekit.utils.AbsolutePVCoordinates;

  23. /** This interface is the top-level abstraction to build first order integrators for propagators conversion.
  24.  * @author Pascal Parraud
  25.  * @since 6.0
  26.  */
  27. public interface ODEIntegratorBuilder {

  28.     /** Build a first order integrator.
  29.      * @param orbit reference orbit
  30.      * @param orbitType orbit type to use
  31.      * @return a first order integrator ready to use
  32.      */
  33.     AbstractIntegrator buildIntegrator(Orbit orbit, OrbitType orbitType);

  34.     /**
  35.      * Build a first order integrator. Non-orbit version.
  36.      * @param absolutePVCoordinates absolute position-velocity vector
  37.      * @return a first order integrator ready to use
  38.      */
  39.     default AbstractIntegrator buildIntegrator(final AbsolutePVCoordinates absolutePVCoordinates) {
  40.         final double arbitraryMu = 1.;
  41.         final CartesianOrbit cartesianOrbit = new CartesianOrbit(absolutePVCoordinates.getPVCoordinates(),
  42.             absolutePVCoordinates.getFrame(), arbitraryMu);
  43.         return buildIntegrator(cartesianOrbit, OrbitType.CARTESIAN);
  44.     }
  45. }