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
19 import org.hipparchus.CalculusFieldElement;
20 import org.orekit.frames.Frame;
21 import org.orekit.time.AbsoluteDate;
22 import org.orekit.utils.ExtendedPositionProvider;
23 import org.orekit.utils.TimeStampedAngularCoordinates;
24 import org.orekit.utils.TimeStampedFieldAngularCoordinates;
25
26 /**
27 * Attitude providers for Beidou geostationary orbit navigation satellites.
28 * @author Luc Maisonobe Java translation
29 * @since 9.2
30 */
31 public class BeidouGeo extends AbstractGNSSAttitudeProvider {
32
33 /** Simple constructor.
34 * @param validityStart start of validity for this provider
35 * @param validityEnd end of validity for this provider
36 * @param sun provider for Sun position
37 * @param inertialFrame inertial frame where velocity are computed
38 */
39 public BeidouGeo(final AbsoluteDate validityStart, final AbsoluteDate validityEnd,
40 final ExtendedPositionProvider sun, final Frame inertialFrame) {
41 super(validityStart, validityEnd, sun, inertialFrame);
42 }
43
44 /** {@inheritDoc} */
45 @Override
46 protected TimeStampedAngularCoordinates correctedYaw(final GNSSAttitudeContext context) {
47
48 // geostationary Beidou spacecraft are always in Orbit Normal (ON) yaw
49 return context.orbitNormalYaw();
50
51 }
52
53 /** {@inheritDoc} */
54 @Override
55 protected <T extends CalculusFieldElement<T>> TimeStampedFieldAngularCoordinates<T> correctedYaw(final GNSSFieldAttitudeContext<T> context) {
56
57 // geostationary Beidou spacecraft are always in Orbit Normal (ON) yaw
58 return context.orbitNormalYaw();
59
60 }
61
62 }