SP3Ephemeris.java
/* Copyright 2002-2024 Luc Maisonobe
* 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.files.sp3;
import java.util.ArrayList;
import java.util.Collections;
import java.util.List;
import org.orekit.files.general.EphemerisFile;
import org.orekit.frames.Frame;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.CartesianDerivativesFilter;
/** Single satellite ephemeris from an {@link SP3 SP3} file.
* @author Luc Maisonobe
* @since 12.0
*/
public class SP3Ephemeris implements EphemerisFile.SatelliteEphemeris<SP3Coordinate, SP3Segment> {
/** Satellite ID. */
private final String id;
/** Standard gravitational parameter in m³ / s². */
private final double mu;
/** Reference frame. */
private final Frame frame;
/** Number of points to use for interpolation. */
private final int interpolationSamples;
/** Available derivatives. */
private final CartesianDerivativesFilter filter;
/** Segments. */
private final List<SP3Segment> segments;
/** Create an ephemeris for a single satellite.
* @param id of the satellite.
* @param mu standard gravitational parameter to use for creating
* {@link org.orekit.orbits.Orbit Orbits} from the ephemeris data.
* @param frame reference frame
* @param interpolationSamples number of points to use for interpolation
* @param filter available derivatives
*/
public SP3Ephemeris(final String id, final double mu, final Frame frame,
final int interpolationSamples, final CartesianDerivativesFilter filter) {
this.id = id;
this.mu = mu;
this.frame = frame;
this.interpolationSamples = interpolationSamples;
this.filter = filter;
this.segments = new ArrayList<>();
}
/** {@inheritDoc} */
@Override
public String getId() {
return this.id;
}
/** {@inheritDoc} */
@Override
public double getMu() {
return mu;
}
/** {@inheritDoc} */
@Override
public List<SP3Segment> getSegments() {
return Collections.unmodifiableList(segments);
}
/** {@inheritDoc} */
@Override
public AbsoluteDate getStart() {
return segments.isEmpty() ? null : segments.get(0).getStart();
}
/** {@inheritDoc} */
@Override
public AbsoluteDate getStop() {
return segments.isEmpty() ? null : segments.get(segments.size() - 1).getStop();
}
/** Get the reference frame.
* @return reference frame
*/
public Frame getFrame() {
return frame;
}
/** Get the number of points to use for interpolation.
* @return number of points to use for interpolation
*/
public int getInterpolationSamples() {
return interpolationSamples;
}
/** Get the available derivatives.
* @return available derivatives
*/
public CartesianDerivativesFilter getAvailableDerivatives() {
return filter;
}
/** Adds a new P/V coordinate.
* @param coord the P/V coordinate of the satellite
* @param maxGap maximum gap between segments
*/
public void addCoordinate(final SP3Coordinate coord, final double maxGap) {
final AbsoluteDate lastDate = getStop();
final SP3Segment segment;
if (lastDate == null || coord.getDate().durationFrom(lastDate) > maxGap) {
// we need to create a new segment
segment = new SP3Segment(mu, frame, interpolationSamples, filter);
segments.add(segment);
} else {
segment = segments.get(segments.size() - 1);
}
segment.addCoordinate(coord);
}
}