GenericGNSS.java

  1. /* Copyright 2002-2025 CS GROUP
  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.gnss.attitude;

  18. import org.hipparchus.CalculusFieldElement;
  19. import org.orekit.frames.Frame;
  20. import org.orekit.time.AbsoluteDate;
  21. import org.orekit.utils.ExtendedPositionProvider;
  22. import org.orekit.utils.TimeStampedAngularCoordinates;
  23. import org.orekit.utils.TimeStampedFieldAngularCoordinates;

  24. /**
  25.  * Attitude providers for navigation satellites for which no specialized model is known.
  26.  *
  27.  * @author Luc Maisonobe
  28.  * @since 9.2
  29.  */
  30. public class GenericGNSS extends AbstractGNSSAttitudeProvider {

  31.     /** Simple constructor.
  32.      * @param validityStart start of validity for this provider
  33.      * @param validityEnd end of validity for this provider
  34.      * @param sun provider for Sun position
  35.      * @param inertialFrame inertial frame where velocity are computed
  36.      */
  37.     public GenericGNSS(final AbsoluteDate validityStart, final AbsoluteDate validityEnd,
  38.                        final ExtendedPositionProvider sun, final Frame inertialFrame) {
  39.         super(validityStart, validityEnd, sun, inertialFrame);
  40.     }

  41.     /** {@inheritDoc} */
  42.     @Override
  43.     protected TimeStampedAngularCoordinates correctedYaw(final GNSSAttitudeContext context) {
  44.         // no eclipse/noon turn mode for generic spacecraft
  45.         return context.nominalYaw(context.getDate());
  46.     }

  47.     /** {@inheritDoc} */
  48.     @Override
  49.     protected <T extends CalculusFieldElement<T>> TimeStampedFieldAngularCoordinates<T> correctedYaw(final GNSSFieldAttitudeContext<T> context) {
  50.         // no eclipse/noon turn mode for generic spacecraft
  51.         return context.nominalYaw(context.getDate());
  52.     }

  53. }