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.orekit.bodies.CelestialBodies;
22 import org.orekit.propagation.SpacecraftState;
23 import org.orekit.propagation.events.handlers.EventHandler;
24 import org.orekit.propagation.events.handlers.StopOnDecreasing;
25 import org.orekit.utils.PVCoordinatesProvider;
26
27 /** Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.
28 * <p>The main use case for this detector is when the observer is in fact a ground
29 * station, modeled as a {@link org.orekit.frames.TopocentricFrame} and when the beacon
30 * is the {@link CelestialBodies#getSun() Sun}, for computing
31 * interferences for the telemetry link. Another similar case is when the beacon is
32 * another spacecraft, for interferences computation.</p>
33 * <p>The default handler behavior is to {@link Action#STOP stop}
34 * propagation when spacecraft enters the proximity zone. This can be changed by calling
35 * {@link #withHandler(EventHandler)} after construction.</p>
36 * @see org.orekit.propagation.Propagator#addEventDetector(EventDetector)
37 * @author Luc Maisonobe
38 * @since 8.0
39 */
40 public class AngularSeparationDetector extends AbstractDetector<AngularSeparationDetector> {
41
42 /** Default detection settings. */
43 public static final EventDetectionSettings DEFAULT_SETTINGS = new EventDetectionSettings(60., 1e-3, EventDetectionSettings.DEFAULT_MAX_ITER);
44
45 /** Beacon at the center of the proximity zone. */
46 private final PVCoordinatesProvider beacon;
47
48 /** Observer for the spacecraft, that may also see the beacon at the same time if they are too close. */
49 private final PVCoordinatesProvider observer;
50
51 /** Proximity angle (rad). */
52 private final double proximityAngle;
53
54 /** Build a new angular separation detector.
55 * @param beacon beacon at the center of the proximity zone
56 * @param observer observer for the spacecraft, that may also see
57 * the beacon at the same time if they are too close to each other
58 * @param proximityAngle proximity angle as seen from observer, at which events are triggered (rad)
59 */
60 public AngularSeparationDetector(final PVCoordinatesProvider beacon,
61 final PVCoordinatesProvider observer,
62 final double proximityAngle) {
63 this(DEFAULT_SETTINGS, new StopOnDecreasing(), beacon, observer, proximityAngle);
64 }
65
66 /** Protected constructor with full parameters.
67 * <p>
68 * This constructor is not public as users are expected to use the builder
69 * API with the various {@code withXxx()} methods to set up the instance
70 * in a readable manner without using a huge amount of parameters.
71 * </p>
72 * @param detectionSettings detection settings
73 * @param handler event handler to call at event occurrences
74 * @param beacon beacon at the center of the proximity zone
75 * @param observer observer for the spacecraft, that may also see
76 * the beacon at the same time if they are too close to each other
77 * @param proximityAngle proximity angle as seen from observer, at which events are triggered (rad)
78 * @since 13.0
79 */
80 protected AngularSeparationDetector(final EventDetectionSettings detectionSettings,
81 final EventHandler handler,
82 final PVCoordinatesProvider beacon,
83 final PVCoordinatesProvider observer,
84 final double proximityAngle) {
85 super(detectionSettings, handler);
86 this.beacon = beacon;
87 this.observer = observer;
88 this.proximityAngle = proximityAngle;
89 }
90
91 /** {@inheritDoc} */
92 @Override
93 protected AngularSeparationDetector create(final EventDetectionSettings detectionSettings, final EventHandler newHandler) {
94 return new AngularSeparationDetector(detectionSettings, newHandler,
95 beacon, observer, proximityAngle);
96 }
97
98 /** Get the beacon at the center of the proximity zone.
99 * @return beacon at the center of the proximity zone
100 */
101 public PVCoordinatesProvider getBeacon() {
102 return beacon;
103 }
104
105 /** Get the observer for the spacecraft.
106 * @return observer for the spacecraft
107 */
108 public PVCoordinatesProvider getObserver() {
109 return observer;
110 }
111
112 /** Get the proximity angle (rad).
113 * @return the proximity angle
114 */
115 public double getProximityAngle() {
116 return proximityAngle;
117 }
118
119 /** Compute the value of the switching function.
120 * <p>
121 * This function measures the angular separation between beacon and spacecraft
122 * as seen from the observer minus the proximity angle. It therefore triggers
123 * decreasing events when the spacecraft enters the proximity zone and increasing
124 * events when it leaves the proximity zone.
125 * </p>
126 * <p>
127 * No shadowing effect is taken into account, so this method is computed and
128 * may trigger events even when the spacecraft is below horizon for an observer
129 * which is a ground station. If such effects must be taken into account the
130 * detector must be associated with a {@link EventEnablingPredicateFilter predicate
131 * filter} where the {@link EnablingPredicate predicate function} is based on elevation.
132 * </p>
133 * @param s the current state information: date, kinematics, attitude
134 * @return value of the switching function
135 */
136 public double g(final SpacecraftState s) {
137 final Vector3D sPosition = s.getPosition();
138 final Vector3D bP = beacon.getPosition(s.getDate(), s.getFrame());
139 final Vector3D oP = observer.getPosition(s.getDate(), s.getFrame());
140 final double separation = Vector3D.angle(sPosition.subtract(oP), bP.subtract(oP));
141 return separation - proximityAngle;
142 }
143
144 }