/* 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.measurements;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.junit.Assert;
import org.orekit.propagation.SpacecraftState;
public class PVMeasurementCreator extends MeasurementCreator {
public void handleStep(final SpacecraftState currentState, final boolean isLast) {
final Vector3D p = currentState.getPVCoordinates().getPosition();
final Vector3D v = currentState.getPVCoordinates().getVelocity();
final PV measurement = new PV(currentState.getDate(), p, v, 1.0, 0.001, 1.0);
Assert.assertEquals(0.0, Vector3D.distance(p, measurement.getPosition()), 1.0e-10);
Assert.assertEquals(0.0, Vector3D.distance(v, measurement.getVelocity()), 1.0e-10);
addMeasurement(measurement);
}
}