BeidouGeo.java
- /* Copyright 2002-2025 CS GROUP
- * 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.gnss.attitude;
- import org.hipparchus.CalculusFieldElement;
- import org.orekit.frames.Frame;
- import org.orekit.time.AbsoluteDate;
- import org.orekit.utils.ExtendedPositionProvider;
- import org.orekit.utils.TimeStampedAngularCoordinates;
- import org.orekit.utils.TimeStampedFieldAngularCoordinates;
- /**
- * Attitude providers for Beidou geostationary orbit navigation satellites.
- * @author Luc Maisonobe Java translation
- * @since 9.2
- */
- public class BeidouGeo extends AbstractGNSSAttitudeProvider {
- /** Simple constructor.
- * @param validityStart start of validity for this provider
- * @param validityEnd end of validity for this provider
- * @param sun provider for Sun position
- * @param inertialFrame inertial frame where velocity are computed
- */
- public BeidouGeo(final AbsoluteDate validityStart, final AbsoluteDate validityEnd,
- final ExtendedPositionProvider sun, final Frame inertialFrame) {
- super(validityStart, validityEnd, sun, inertialFrame);
- }
- /** {@inheritDoc} */
- @Override
- protected TimeStampedAngularCoordinates correctedYaw(final GNSSAttitudeContext context) {
- // geostationary Beidou spacecraft are always in Orbit Normal (ON) yaw
- return context.orbitNormalYaw();
- }
- /** {@inheritDoc} */
- @Override
- protected <T extends CalculusFieldElement<T>> TimeStampedFieldAngularCoordinates<T> correctedYaw(final GNSSFieldAttitudeContext<T> context) {
- // geostationary Beidou spacecraft are always in Orbit Normal (ON) yaw
- return context.orbitNormalYaw();
- }
- }