RelativisticClockOneWayGNSSRangeRateModifier.java

  1. /* Copyright 2002-2024 Thales Alenia Space
  2.  * Licensed to CS GROUP (CS) under one or more
  3.  * contributor license agreements.  See the NOTICE file distributed with
  4.  * this work for additional information regarding copyright ownership.
  5.  * CS licenses this file to You under the Apache License, Version 2.0
  6.  * (the "License"); you may not use this file except in compliance with
  7.  * the License.  You may obtain a copy of the License at
  8.  *
  9.  *   http://www.apache.org/licenses/LICENSE-2.0
  10.  *
  11.  * Unless required by applicable law or agreed to in writing, software
  12.  * distributed under the License is distributed on an "AS IS" BASIS,
  13.  * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
  14.  * See the License for the specific language governing permissions and
  15.  * limitations under the License.
  16.  */
  17. package org.orekit.estimation.measurements.modifiers;

  18. import org.orekit.estimation.measurements.EstimatedMeasurementBase;
  19. import org.orekit.estimation.measurements.gnss.OneWayGNSSRangeRate;
  20. import org.orekit.propagation.SpacecraftState;
  21. import org.orekit.utils.PVCoordinates;

  22. /** Class modifying theoretical range-rate measurement with relativistic frequency deviation.
  23.  * <p>
  24.  * Relativistic clock correction is caused by the motion of the satellite as well as
  25.  * the change in the gravitational potential
  26.  * </p>
  27.  * @author Luc Maisonobe
  28.  * @since 12.1
  29.  *
  30.  * @see "Teunissen, Peter, and Oliver Montenbruck, eds. Springer handbook of global navigation
  31.  * satellite systems. Chapter 19.2. Springer, 2017."
  32.  */
  33. public class RelativisticClockOneWayGNSSRangeRateModifier
  34.     extends AbstractRelativisticClockOnBoardRangeRateModifier<OneWayGNSSRangeRate> {

  35.     /** Simple constructor.
  36.      * @param gm gravitational constant for main body in signal path vicinity.
  37.      */
  38.     public RelativisticClockOneWayGNSSRangeRateModifier(final double gm) {
  39.         super(gm);
  40.     }

  41.     /** {@inheritDoc} */
  42.     @Override
  43.     public void modifyWithoutDerivatives(final EstimatedMeasurementBase<OneWayGNSSRangeRate> estimated) {

  44.         // local satellite
  45.         final SpacecraftState local = estimated.getStates()[0];

  46.         // compute semi major axis of remote (transmitter) satellite
  47.         final PVCoordinates remote  = estimated.getParticipants()[0];
  48.         final double        rRemote = remote.getPosition().getNorm();
  49.         final double        vRemote = remote.getVelocity().getNorm();
  50.         final double        aRemote = 1.0 / (2 / rRemote - vRemote * vRemote / getGm());

  51.         modifyWithoutDerivatives(estimated,
  52.                                  local.getA(), local.getPosition().getNorm(),
  53.                                  aRemote, rRemote);

  54.     }

  55. }