ObserverSatellite.java
/* Copyright 2002-2026 Brianna Aubin
* Licensed to Hawkeye 360 (HE360) 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 java.util.Map;
import org.hipparchus.analysis.differentiation.Gradient;
import org.hipparchus.analysis.differentiation.GradientField;
import org.hipparchus.Field;
import org.orekit.frames.FieldTransform;
import org.orekit.frames.Frame;
import org.orekit.frames.Transform;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
import org.orekit.time.clocks.QuadraticClockModel;
import org.orekit.utils.ExtendedPositionProvider;
import org.orekit.utils.FieldPVCoordinatesProvider;
import org.orekit.utils.PVCoordinates;
import org.orekit.utils.PVCoordinatesProvider;
import org.orekit.utils.TimeStampedFieldPVCoordinates;
import org.orekit.utils.TimeStampedPVCoordinates;
/** Class that accepts a PVCoordinatesProvider for a space-
* based measurement receiver.
*
* @author Brianna Aubin
* @since 14.0
*/
public class ObserverSatellite extends MeasurementObject implements Observer {
/** Provides satellite trajectory. */
private final PVCoordinatesProvider pvCoordsProvider;
/** Simple constructor.
* @param name name of receiver
* @param pvCoordsProvider position/velocity coordinates provider for receiver
* @since 14.0
*/
public ObserverSatellite(final String name, final PVCoordinatesProvider pvCoordsProvider) {
this(name, pvCoordsProvider, createEmptyQuadraticClock(name));
}
/** Simple constructor.
* @param name name of receiver
* @param pvCoordsProvider position/velocity coordinates provider for receiver
* @param quadraticClock clock model for receiver
* @since 14.0
*/
public ObserverSatellite(final String name, final PVCoordinatesProvider pvCoordsProvider, final QuadraticClockModel quadraticClock) {
super(name, quadraticClock);
this.pvCoordsProvider = pvCoordsProvider;
}
/** {@inheritDoc} */
@Override
public final ObserverType getObserverType() {
return ObserverType.SATELLITE;
}
/** {@inheritDoc} */
@Override
public final PVCoordinatesProvider getPVCoordinatesProvider() {
return pvCoordsProvider;
}
/** {@inheritDoc} */
@Override
public FieldPVCoordinatesProvider<Gradient> getFieldPVCoordinatesProvider(final int freeParameters,
final Map<String, Integer> parameterIndices) {
// If a FieldPVCoordinatesProvider<Gradient> already exists, use it
if (pvCoordsProvider instanceof ExtendedPositionProvider) {
final Field<Gradient> check = GradientField.getField(freeParameters);
return ((ExtendedPositionProvider) pvCoordsProvider).toFieldPVCoordinatesProvider(check);
}
// Otherwise, convert the PVCoordinatesProvider to a FieldPVCoordinatesProvider<Gradient>
else {
return (date, frame) -> {
// apply the raw (no derivatives) remote provider
final AbsoluteDate dateBase = date.toAbsoluteDate();
final TimeStampedPVCoordinates pvBase = pvCoordsProvider.getPVCoordinates(dateBase, frame);
final TimeStampedFieldPVCoordinates<Gradient> pvWithoutDerivatives =
new TimeStampedFieldPVCoordinates<>(date.getField(), pvBase);
// add derivatives, using a trick: we shift the date by 0, with derivatives
final Gradient zeroWithDerivatives = date.durationFrom(dateBase);
return pvWithoutDerivatives.shiftedBy(zeroWithDerivatives);
};
}
}
/** {@inheritDoc} */
@Override
public Transform getOffsetToInertial(final Frame inertial,
final AbsoluteDate date,
final boolean clockOffsetAlreadyApplied) {
// take clock offset into account
final AbsoluteDate offsetCompensatedDate = clockOffsetAlreadyApplied ?
date :
new AbsoluteDate(date, -getClockOffsetDriver().getValue());
// Return transform that will give PV coords of emitter when pos = 0, vel = 0 is entered
final PVCoordinates coords = getPVCoordinates(offsetCompensatedDate, inertial);
return new Transform(offsetCompensatedDate, coords.getPosition(), coords.getVelocity(), coords.getAcceleration());
}
/** {@inheritDoc} */
@Override
public FieldTransform<Gradient> getOffsetToInertial(final Frame inertial,
final FieldAbsoluteDate<Gradient> offsetCompensatedDate,
final int freeParameters,
final Map<String, Integer> indices) {
final AbsoluteDate clockDate = offsetCompensatedDate.toAbsoluteDate();
final Field<Gradient> field = offsetCompensatedDate.getField();
final Transform transform = getOffsetToInertial(inertial, clockDate, true);
return new FieldTransform<>(field, transform);
}
}