KeplerianPropagatorBuilder.java
/* Copyright 2002-2019 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
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*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
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package org.orekit.propagation.conversion;
import org.orekit.orbits.Orbit;
import org.orekit.orbits.PositionAngle;
import org.orekit.propagation.Propagator;
import org.orekit.propagation.analytical.KeplerianPropagator;
/** Builder for Keplerian propagator.
* @author Pascal Parraud
* @since 6.0
*/
public class KeplerianPropagatorBuilder extends AbstractPropagatorBuilder {
/** Build a new instance.
* <p>
* The template orbit is used as a model to {@link
* #createInitialOrbit() create initial orbit}. It defines the
* inertial frame, the central attraction coefficient, the orbit type, and is also
* used together with the {@code positionScale} to convert from the {@link
* org.orekit.utils.ParameterDriver#setNormalizedValue(double) normalized} parameters used by the
* callers of this builder to the real orbital parameters.
* </p>
* @param templateOrbit reference orbit from which real orbits will be built
* @param positionAngle position angle type to use
* @param positionScale scaling factor used for orbital parameters normalization
* (typically set to the expected standard deviation of the position)
* @since 8.0
*/
public KeplerianPropagatorBuilder(final Orbit templateOrbit, final PositionAngle positionAngle,
final double positionScale) {
super(templateOrbit, positionAngle, positionScale, true);
}
/** {@inheritDoc} */
public Propagator buildPropagator(final double[] normalizedParameters) {
setParameters(normalizedParameters);
return new KeplerianPropagator(createInitialOrbit());
}
}