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.propagation.events;
18
19 import org.hipparchus.geometry.euclidean.threed.Vector3D;
20 import org.hipparchus.ode.events.Action;
21 import org.hipparchus.util.FastMath;
22 import org.hipparchus.util.SinCos;
23 import org.orekit.orbits.Orbit;
24 import org.orekit.propagation.SpacecraftState;
25 import org.orekit.propagation.events.handlers.EventHandler;
26 import org.orekit.propagation.events.handlers.StopOnIncreasing;
27 import org.orekit.utils.PVCoordinates;
28 import org.orekit.utils.PVCoordinatesProvider;
29
30 /** Finder for satellite/body alignment events in orbital plane.
31 * <p>This class finds alignment events.</p>
32 * <p>Alignment means the conjunction, with some threshold angle, between the satellite
33 * position and the projection in the orbital plane of some body position.</p>
34 * <p>The default handler behavior is to {@link Action#STOP stop}
35 * propagation when alignment is reached. This can be changed by calling
36 * {@link #withHandler(EventHandler)} after construction.</p>
37 * @see org.orekit.propagation.Propagator#addEventDetector(EventDetector)
38 * @author Pascal Parraud
39 */
40 public class AlignmentDetector extends AbstractDetector<AlignmentDetector> {
41
42 /** Body to align. */
43 private final PVCoordinatesProvider body;
44
45 /** Alignment angle (rad). */
46 private final double alignAngle;
47
48 /** Cosinus of alignment angle. */
49 private final double cosAlignAngle;
50
51 /** Sinus of alignment angle. */
52 private final double sinAlignAngle;
53
54 /** Build a new alignment detector.
55 * <p>The orbit is used only to set an upper bound for the max check interval
56 * to period/3 and to set the convergence threshold according to orbit size.</p>
57 * @param orbit initial orbit
58 * @param body the body to align
59 * @param alignAngle the alignment angle (rad)
60 */
61 public AlignmentDetector(final Orbit orbit,
62 final PVCoordinatesProvider body,
63 final double alignAngle) {
64 this(1.0e-13 * orbit.getKeplerianPeriod(), orbit, body, alignAngle);
65 }
66
67 /** Build a new alignment detector.
68 * @param maxCheck maximum checking interval (s)
69 * @param threshold convergence threshold (s)
70 * @param body the body to align
71 * @param alignAngle the alignment angle (rad)
72 */
73 public AlignmentDetector(final double maxCheck, final double threshold,
74 final PVCoordinatesProvider body,
75 final double alignAngle) {
76 this(new EventDetectionSettings(maxCheck, threshold, EventDetectionSettings.DEFAULT_MAX_ITER),
77 new StopOnIncreasing(), body, alignAngle);
78 }
79
80 /** Build a new alignment detector.
81 * @param detectionSettings detection settings
82 * @param body the body to align
83 * @param alignAngle the alignment angle (rad)
84 * @since 13.0
85 */
86 public AlignmentDetector(final EventDetectionSettings detectionSettings,
87 final PVCoordinatesProvider body,
88 final double alignAngle) {
89 this(detectionSettings, new StopOnIncreasing(), body, alignAngle);
90 }
91
92 /** Build a new alignment detector.
93 * <p>The orbit is used only to set an upper bound for the max check interval
94 * to period/3.</p>
95 * @param threshold convergence threshold (s)
96 * @param orbit initial orbit
97 * @param body the body to align
98 * @param alignAngle the alignment angle (rad)
99 */
100 public AlignmentDetector(final double threshold,
101 final Orbit orbit,
102 final PVCoordinatesProvider body,
103 final double alignAngle) {
104 this(orbit.getKeplerianPeriod() / 3, threshold, body, alignAngle);
105 }
106
107 /** Protected constructor with full parameters.
108 * <p>
109 * This constructor is not public as users are expected to use the builder
110 * API with the various {@code withXxx()} methods to set up the instance
111 * in a readable manner without using a huge amount of parameters.
112 * </p>
113 * @param detectionSettings detection settings
114 * @param handler event handler to call at event occurrences
115 * @param body the body to align
116 * @param alignAngle the alignment angle (rad)
117 * @since 13.0
118 */
119 protected AlignmentDetector(final EventDetectionSettings detectionSettings, final EventHandler handler,
120 final PVCoordinatesProvider body,
121 final double alignAngle) {
122 super(detectionSettings, handler);
123 final SinCos sc = FastMath.sinCos(alignAngle);
124 this.body = body;
125 this.alignAngle = alignAngle;
126 this.cosAlignAngle = sc.cos();
127 this.sinAlignAngle = sc.sin();
128 }
129
130 /** {@inheritDoc} */
131 @Override
132 protected AlignmentDetector create(final EventDetectionSettings detectionSettings, final EventHandler newHandler) {
133 return new AlignmentDetector(detectionSettings, newHandler, body, alignAngle);
134 }
135
136 /** Get the body to align.
137 * @return the body to align
138 */
139 public PVCoordinatesProvider getPVCoordinatesProvider() {
140 return body;
141 }
142
143 /** Get the alignment angle (rad).
144 * @return the alignment angle
145 */
146 public double getAlignAngle() {
147 return alignAngle;
148 }
149
150 /** Compute the value of the switching function.
151 * This function measures the difference between the alignment angle and the
152 * angle between the satellite position and the body position projection in the
153 * orbital plane.
154 * @param s the current state information: date, kinematics, attitude
155 * @return value of the switching function
156 */
157 public double g(final SpacecraftState s) {
158 final PVCoordinates pv = s.getPVCoordinates();
159 final Vector3D a = pv.getPosition().normalize();
160 final Vector3D b = Vector3D.crossProduct(pv.getMomentum(), a).normalize();
161 final Vector3D x = new Vector3D(cosAlignAngle, a, sinAlignAngle, b);
162 final Vector3D y = new Vector3D(sinAlignAngle, a, -cosAlignAngle, b);
163 final Vector3D pb = body.getPosition(s.getDate(), s.getFrame());
164 final double beta = FastMath.atan2(Vector3D.dotProduct(pb, y), Vector3D.dotProduct(pb, x));
165 final double betm = -FastMath.PI - beta;
166 final double betp = FastMath.PI - beta;
167 if (beta < betm) {
168 return betm;
169 } else if (beta < betp) {
170 return beta;
171 } else {
172 return betp;
173 }
174 }
175
176 }