AbstractInterSatellitesMeasurement.java
- /* Copyright 2022-2025 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.estimation.measurements.gnss;
- import java.util.Arrays;
- import org.hipparchus.analysis.differentiation.Gradient;
- import org.orekit.estimation.measurements.ObservableSatellite;
- import org.orekit.estimation.measurements.ObservedMeasurement;
- import org.orekit.estimation.measurements.QuadraticClockModel;
- import org.orekit.propagation.SpacecraftState;
- import org.orekit.time.AbsoluteDate;
- import org.orekit.utils.FieldPVCoordinatesProvider;
- import org.orekit.utils.PVCoordinatesProvider;
- import org.orekit.utils.ShiftingPVCoordinatesProvider;
- import org.orekit.utils.TimeStampedFieldPVCoordinates;
- /** Base class for measurement between two satellites that are both estimated.
- * <p>
- * The measurement is considered to be a signal emitted from
- * a remote satellite and received by a local satellite.
- * Its value is the number of cycles between emission and reception.
- * The motion of both spacecraft during the signal flight time
- * are taken into account. The date of the measurement corresponds to the
- * reception on ground of the emitted signal.
- * </p>
- * @param <T> type of the measurement
- * @author Luc Maisonobe
- * @since 12.1
- */
- public abstract class AbstractInterSatellitesMeasurement<T extends ObservedMeasurement<T>> extends AbstractOnBoardMeasurement<T> {
- /** Constructor.
- * @param date date of the measurement
- * @param observed observed value
- * @param sigma theoretical standard deviation
- * @param baseWeight base weight
- * @param local satellite which receives the signal and performs the measurement
- * @param remote remote satellite which simply emits the signal
- */
- public AbstractInterSatellitesMeasurement(final AbsoluteDate date, final double observed,
- final double sigma, final double baseWeight,
- final ObservableSatellite local,
- final ObservableSatellite remote) {
- // Call to super constructor
- super(date, observed, sigma, baseWeight, Arrays.asList(local, remote));
- }
- /** {@inheritDoc} */
- @Override
- protected PVCoordinatesProvider getRemotePV(final SpacecraftState[] states) {
- return new ShiftingPVCoordinatesProvider(states[1].getPVCoordinates(), states[1].getFrame());
- }
- /** {@inheritDoc} */
- @Override
- protected QuadraticClockModel getRemoteClock() {
- return getSatellites().get(1).getQuadraticClockModel();
- }
- /** {@inheritDoc} */
- @Override
- protected FieldPVCoordinatesProvider<Gradient> getRemotePV(final SpacecraftState[] states,
- final int freeParameters) {
- // convert the SpacecraftState to a FieldPVCoordinatesProvider<Gradient>
- return (date, frame) -> {
- // set up the derivatives with respect to remote state at its date
- final TimeStampedFieldPVCoordinates<Gradient> pv0 = getCoordinates(states[1], 6, freeParameters);
- // shift to desired date
- final TimeStampedFieldPVCoordinates<Gradient> shifted = pv0.shiftedBy(date.durationFrom(states[1].getDate()));
- // transform to desired frame
- return states[1].getFrame().getTransformTo(frame, states[1].getDate()).transformPVCoordinates(shifted);
- };
- }
- }