HalfTrackSampler.java
/* Copyright 2002-2023 CS GROUP
* Licensed to CS GROUP (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.models.earth.tessellation;
import java.util.ArrayList;
import java.util.List;
import org.hipparchus.util.Pair;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.bodies.OneAxisEllipsoid;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.sampling.OrekitFixedStepHandler;
import org.orekit.utils.TimeStampedPVCoordinates;
/** Sampler for half track span.
* @since 7.1
* @see AlongTrackAiming
* @author Luc Maisonobe
*/
class HalfTrackSampler implements OrekitFixedStepHandler {
/** Ellipsoid over which track is sampled. */
private final OneAxisEllipsoid ellipsoid;
/** Half track sample. */
private final List<Pair<GeodeticPoint, TimeStampedPVCoordinates>> halfTrack;
/** Simple constructor.
* @param ellipsoid ellipsoid over which track is sampled
*/
HalfTrackSampler(final OneAxisEllipsoid ellipsoid) {
this.ellipsoid = ellipsoid;
this.halfTrack = new ArrayList<Pair<GeodeticPoint, TimeStampedPVCoordinates>>();
}
/** Get half track sample.
* @return half track sample
*/
public List<Pair<GeodeticPoint, TimeStampedPVCoordinates>> getHalfTrack() {
return halfTrack;
}
/** {@inheritDoc} */
@Override
public void handleStep(final SpacecraftState currentState) {
// find the sliding ground point below spacecraft
final TimeStampedPVCoordinates pv = currentState.getPVCoordinates(ellipsoid.getBodyFrame());
final TimeStampedPVCoordinates groundPV = ellipsoid.projectToGround(pv, ellipsoid.getBodyFrame());
// geodetic coordinates
final GeodeticPoint gp =
ellipsoid.transform(groundPV.getPosition(), ellipsoid.getBodyFrame(), currentState.getDate());
halfTrack.add(new Pair<GeodeticPoint, TimeStampedPVCoordinates>(gp, groundPV));
}
}