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.files.ccsds.ndm.adm.apm;
18  
19  import java.io.IOException;
20  
21  import org.orekit.data.DataContext;
22  import org.orekit.files.ccsds.definitions.TimeSystem;
23  import org.orekit.files.ccsds.ndm.ParsedUnitsBehavior;
24  import org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataWriter;
25  import org.orekit.files.ccsds.ndm.adm.AdmHeader;
26  import org.orekit.files.ccsds.ndm.adm.AdmMetadata;
27  import org.orekit.files.ccsds.section.Segment;
28  import org.orekit.files.ccsds.section.XmlStructureKey;
29  import org.orekit.files.ccsds.utils.ContextBinding;
30  import org.orekit.files.ccsds.utils.FileFormat;
31  import org.orekit.files.ccsds.utils.generation.AbstractMessageWriter;
32  import org.orekit.files.ccsds.utils.generation.Generator;
33  import org.orekit.time.AbsoluteDate;
34  import org.orekit.utils.IERSConventions;
35  
36  
37  /**
38   * Writer for CCSDS Orbit Parameter Message.
39   *
40   * @author Luc Maisonobe
41   * @since 11.0
42   */
43  public class ApmWriter extends AbstractMessageWriter<AdmHeader, Segment<AdmMetadata, ApmData>, Apm> {
44  
45      /** Version number implemented. **/
46      public static final double CCSDS_APM_VERS = 1.0;
47  
48      /** Padding width for aligning the '=' sign. */
49      public static final int KVN_PADDING_WIDTH = 17;
50  
51      /** Complete constructor.
52       * <p>
53       * Calling this constructor directly is not recommended. Users should rather use
54       * {@link org.orekit.files.ccsds.ndm.WriterBuilder#buildApmWriter()
55       * writerBuilder.buildOpmWriter()}.
56       * </p>
57       * @param conventions IERS Conventions
58       * @param dataContext used to retrieve frames, time scales, etc.
59       * @param missionReferenceDate reference date for Mission Elapsed Time or Mission Relative Time time systems
60       */
61      public ApmWriter(final IERSConventions conventions, final DataContext dataContext,
62                       final AbsoluteDate missionReferenceDate) {
63          super(Apm.ROOT, Apm.FORMAT_VERSION_KEY, CCSDS_APM_VERS,
64                new ContextBinding(
65                    () -> conventions,
66                    () -> false, () -> dataContext, () -> ParsedUnitsBehavior.STRICT_COMPLIANCE,
67                    () -> missionReferenceDate, () -> TimeSystem.UTC,
68                    () -> 0.0, () -> 1.0));
69      }
70  
71      /** {@inheritDoc} */
72      @Override
73      protected void writeSegmentContent(final Generator generator, final double formatVersion,
74                                         final Segment<AdmMetadata, ApmData> segment)
75          throws IOException {
76  
77          // write the metadata
78          final ContextBinding oldContext = getContext();
79          final AdmMetadata    metadata   = segment.getMetadata();
80          setContext(new ContextBinding(oldContext::getConventions,
81                                        oldContext::isSimpleEOP,
82                                        oldContext::getDataContext,
83                                        oldContext::getParsedUnitsBehavior,
84                                        oldContext::getReferenceDate,
85                                        metadata::getTimeSystem,
86                                        oldContext::getClockCount,
87                                        oldContext::getClockRate));
88          new AdmCommonMetadataWriter(metadata).write(generator);
89  
90          // start data block
91          if (generator.getFormat() == FileFormat.XML) {
92              generator.enterSection(XmlStructureKey.data.name());
93          }
94  
95          generator.writeComments(segment.getData().getComments());
96          if (formatVersion >= 2.0) {
97              // starting with version 2, epoch is outside of other blocks
98              generator.writeEntry("EPOCH", getTimeConverter(), segment.getData().getEpoch(), false, true);
99          }
100 
101         if (segment.getData().getQuaternionBlock() != null) {
102             // write quaternion block
103             final String xmlTag = ApmDataSubStructureKey.quaternionState.name();
104             final String kvnTag = formatVersion < 2.0 ? null : ApmDataSubStructureKey.QUAT.name();
105             new ApmQuaternionWriter(formatVersion, xmlTag, kvnTag,
106                                     segment.getData().getQuaternionBlock(),
107                                     formatVersion >= 2.0 ? null : segment.getData().getEpoch(),
108                                                          getTimeConverter()).
109             write(generator);
110         }
111 
112         if (segment.getData().getEulerBlock() != null) {
113             // write optional Euler block for three axis stabilized satellites
114             final String xmlTag = formatVersion < 2.0 ?
115                                   ApmDataSubStructureKey.eulerElementsThree.name() :
116                                   ApmDataSubStructureKey.eulerAngleState.name();
117             final String kvnTag = formatVersion < 2.0 ? null : ApmDataSubStructureKey.EULER.name();
118             new EulerWriter(formatVersion, xmlTag, kvnTag,
119                             segment.getData().getEulerBlock()).
120             write(generator);
121         }
122 
123         if (segment.getData().getAngularVelocityBlock() != null) {
124             // write optional angular velocity block
125             final String xmlTag = ApmDataSubStructureKey.angularVelocity.name();
126             final String kvnTag = ApmDataSubStructureKey.ANGVEL.name();
127             new AngularVelocityWriter(xmlTag, kvnTag,
128                                       segment.getData().getAngularVelocityBlock()).
129             write(generator);
130         }
131 
132         if (segment.getData().getSpinStabilizedBlock() != null) {
133             // write optional block for spin stabilized satellites
134             final String xmlTag;
135             final String kvnTag;
136             if (formatVersion < 2.0) {
137                 xmlTag = ApmDataSubStructureKey.eulerElementsSpin.name();
138                 kvnTag = null;
139             } else {
140                 xmlTag = ApmDataSubStructureKey.spin.name();
141                 kvnTag = ApmDataSubStructureKey.SPIN.name();
142             }
143             new SpinStabilizedWriter(formatVersion, xmlTag, kvnTag,
144                                      segment.getData().getSpinStabilizedBlock()).
145             write(generator);
146         }
147 
148         if (segment.getData().getInertiaBlock() != null) {
149             // write optional spacecraft parameters block
150             final String xmlTag = formatVersion < 2.0 ?
151                                   ApmDataSubStructureKey.spacecraftParameters.name() :
152                                   ApmDataSubStructureKey.inertia.name();
153             final String kvnTag = formatVersion < 2.0 ? null : ApmDataSubStructureKey.INERTIA.name();
154             new InertiaWriter(formatVersion, xmlTag, kvnTag,
155                               segment.getData().getInertiaBlock()).
156             write(generator);
157         }
158 
159         if (!segment.getData().getManeuvers().isEmpty()) {
160             for (final Maneuver maneuver : segment.getData().getManeuvers()) {
161                 // write optional maneuver block
162                 final String xmlTag = ApmDataSubStructureKey.maneuverParameters.name();
163                 final String kvnTag = formatVersion < 2.0 ? null : ApmDataSubStructureKey.MAN.name();
164                 new ManeuverWriter(formatVersion, xmlTag, kvnTag,
165                                    maneuver, getTimeConverter()).write(generator);
166             }
167         }
168 
169         // stop data block
170         if (generator.getFormat() == FileFormat.XML) {
171             generator.exitSection();
172         }
173 
174     }
175 
176 }