GroundReceiverCommonParametersWithDerivatives.java

  1. /* Copyright 2022-2025 Luc Maisonobe
  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;

  18. import java.util.Map;

  19. import org.hipparchus.analysis.differentiation.Gradient;
  20. import org.orekit.frames.FieldTransform;
  21. import org.orekit.propagation.SpacecraftState;
  22. import org.orekit.utils.TimeStampedFieldPVCoordinates;

  23. /** Common intermediate parameters used to estimate measurements where receiver is a ground station.
  24.  * @author Luc Maisonobe
  25.  * @since 12.0
  26.  */
  27. public class GroundReceiverCommonParametersWithDerivatives extends CommonParametersWithDerivatives {

  28.     /** Transform between station and inertial frame. */
  29.     private final FieldTransform<Gradient> offsetToInertialDownlink;

  30.     /** Station position in inertial frame at end of the downlink leg. */
  31.     private final TimeStampedFieldPVCoordinates<Gradient> stationDownlink;

  32.     /** Simple constructor.
  33.     * @param state spacecraft state
  34.     * @param indices derivatives indices map
  35.     * @param offsetToInertialDownlink transform between station and inertial frame
  36.     * @param stationDownlink station position in inertial frame at end of the downlink leg
  37.     * @param tauD downlink delay
  38.     * @param transitState transit state
  39.     * @param transitPV transit position/velocity as a gradient
  40.     */
  41.     public GroundReceiverCommonParametersWithDerivatives(final SpacecraftState state,
  42.                                                          final Map<String, Integer> indices,
  43.                                                          final FieldTransform<Gradient> offsetToInertialDownlink,
  44.                                                          final TimeStampedFieldPVCoordinates<Gradient> stationDownlink,
  45.                                                          final Gradient tauD,
  46.                                                          final SpacecraftState transitState,
  47.                                                          final TimeStampedFieldPVCoordinates<Gradient> transitPV) {
  48.         super(state, indices, tauD, transitState, transitPV);
  49.         this.offsetToInertialDownlink = offsetToInertialDownlink;
  50.         this.stationDownlink          = stationDownlink;
  51.     }

  52.     /** Get transform between station and inertial frame.
  53.      * @return transform between station and inertial frame
  54.      */
  55.     public FieldTransform<Gradient> getOffsetToInertialDownlink() {
  56.         return offsetToInertialDownlink;
  57.     }

  58.     /** Get station position in inertial frame at end of the downlink leg.
  59.      * @return station position in inertial frame at end of the downlink leg
  60.      */
  61.     public TimeStampedFieldPVCoordinates<Gradient> getStationDownlink() {
  62.         return stationDownlink;
  63.     }

  64. }