Commit 4a8caa6c authored by Bryan Cazabonne's avatar Bryan Cazabonne
Browse files

Added Evan's tests.

parent 8fefd539
/*
* Licensed to the Hipparchus project under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* The ASF 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.events;
import org.hipparchus.ode.ODEIntegrator;
import org.hipparchus.ode.nonstiff.DormandPrince853Integrator;
import org.orekit.bodies.CelestialBodyFactory;
import org.orekit.propagation.PropagationType;
import org.orekit.propagation.Propagator;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.semianalytical.dsst.DSSTPropagator;
import org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody;
import org.orekit.utils.Constants;
/** Test events with the DSST Propagator.
*
* @author Evan Ward
*/
public class CloseEventsDsstOsculatingTest extends CloseEventsAbstractTest {
@Override
public Propagator getPropagator(double stepSize) {
double[][] tol = DSSTPropagator.tolerances(1, initialOrbit);
ODEIntegrator integrator = new DormandPrince853Integrator(stepSize, stepSize, tol[0], tol[1]);
DSSTPropagator propagator = new DSSTPropagator(integrator, PropagationType.OSCULATING);
propagator.setInitialState(new SpacecraftState(initialOrbit));
double gm = Constants.EIGEN5C_EARTH_MU;
propagator.addForceModel(new DSSTThirdBody(CelestialBodyFactory.getMoon(), gm));
return propagator;
}
}
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