GNSSExtendedPositionProvider.java
/* Copyright 2022-2026 Romain Serra
* 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.propagation.analytical.gnss;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.Field;
import org.orekit.attitudes.AttitudeProvider;
import org.orekit.frames.Frame;
import org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements;
import org.orekit.utils.AbstractExtendedPositionProvider;
import org.orekit.utils.ExtendedPositionProvider;
/**
* Class for GNSS extended position provider.
* @see ExtendedPositionProvider
* @author Romain Serra
* @since 14.0
*/
public class GNSSExtendedPositionProvider extends AbstractExtendedPositionProvider<GNSSPropagator> {
/**
* Build a new instance.
* @param orbitalElements GNSS orbital elements
* @param eci Earth Centered Inertial frame
* @param ecef Earth Centered Earth Fixed frame
* @param provider attitude provider
* @param mass satellite mass (kg)
*/
public GNSSExtendedPositionProvider(final GNSSOrbitalElements<?> orbitalElements, final Frame eci,
final Frame ecef, final AttitudeProvider provider, final double mass) {
super(new GNSSPropagator(orbitalElements, eci, ecef, provider, mass));
}
/** {@inheritDoc} */
@Override
protected <T extends CalculusFieldElement<T>> FieldGnssPropagator<T> getFieldProvider(final Field<T> field) {
return new FieldGnssPropagator<>(getProvider().getOrbitalElements().toField(field),
getProvider().getECI(), getProvider().getECEF(), getProvider().getAttitudeProvider(),
field.getZero().newInstance(getProvider().getInitialState().getMass()));
}
}