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.CalculusFieldElement;
20 import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
21 import org.hipparchus.ode.events.Action;
22 import org.orekit.bodies.CelestialBodies;
23 import org.orekit.propagation.FieldSpacecraftState;
24 import org.orekit.propagation.events.handlers.FieldEventHandler;
25 import org.orekit.propagation.events.handlers.FieldStopOnEvent;
26 import org.orekit.utils.ExtendedPositionProvider;
27
28 /** Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.
29 * <p>The main use case for this detector is when the observer is in fact a ground
30 * station, modeled as a {@link org.orekit.frames.TopocentricFrame} and when the beacon
31 * is the {@link CelestialBodies#getSun() Sun}, for computing
32 * interferences for the telemetry link. Another similar case is when the beacon is
33 * another spacecraft, for interferences computation.</p>
34 * <p>The default handler behavior is to {@link Action#STOP stop}
35 * propagation when spacecraft enters the proximity zone. This can be changed by calling
36 * {@code #withHandler(EventHandler)} after construction.</p>
37 * @see org.orekit.propagation.Propagator#addEventDetector(EventDetector)
38 * @author Luc Maisonobe
39 * @author Romain Serra
40 * @see AngularSeparationDetector
41 * @since 13.1
42 */
43 public class FieldAngularSeparationDetector<T extends CalculusFieldElement<T>>
44 extends FieldAbstractDetector<FieldAngularSeparationDetector<T>, T> {
45
46 /** Beacon at the center of the proximity zone. */
47 private final ExtendedPositionProvider beacon;
48
49 /** Observer for the spacecraft, that may also see the beacon at the same time if they are too close. */
50 private final ExtendedPositionProvider observer;
51
52 /** Proximity angle (rad). */
53 private final T proximityAngle;
54
55 /** Build a new angular separation detector.
56 * @param beacon beacon at the center of the proximity zone
57 * @param observer observer for the spacecraft, that may also see
58 * the beacon at the same time if they are too close to each other
59 * @param proximityAngle proximity angle as seen from observer, at which events are triggered (rad)
60 */
61 public FieldAngularSeparationDetector(final ExtendedPositionProvider beacon,
62 final ExtendedPositionProvider observer,
63 final T proximityAngle) {
64 this(new FieldEventDetectionSettings<>(proximityAngle.getField(), AngularSeparationDetector.DEFAULT_SETTINGS),
65 new FieldStopOnEvent<>(), beacon, observer, proximityAngle);
66 }
67
68 /** Protected constructor with full parameters.
69 * <p>
70 * This constructor is not public as users are expected to use the builder
71 * API with the various {@code withXxx()} methods to set up the instance
72 * in a readable manner without using a huge amount of parameters.
73 * </p>
74 * @param detectionSettings detection settings
75 * @param handler event handler to call at event occurrences
76 * @param beacon beacon at the center of the proximity zone
77 * @param observer observer for the spacecraft, that may also see
78 * the beacon at the same time if they are too close to each other
79 * @param proximityAngle proximity angle as seen from observer, at which events are triggered (rad)
80 * @since 13.0
81 */
82 protected FieldAngularSeparationDetector(final FieldEventDetectionSettings<T> detectionSettings,
83 final FieldEventHandler<T> handler,
84 final ExtendedPositionProvider beacon,
85 final ExtendedPositionProvider observer,
86 final T proximityAngle) {
87 super(detectionSettings, handler);
88 this.beacon = beacon;
89 this.observer = observer;
90 this.proximityAngle = proximityAngle;
91 }
92
93 /** {@inheritDoc} */
94 @Override
95 protected FieldAngularSeparationDetector<T> create(final FieldEventDetectionSettings<T> detectionSettings,
96 final FieldEventHandler<T> newHandler) {
97 return new FieldAngularSeparationDetector<>(detectionSettings, newHandler, beacon, observer, proximityAngle);
98 }
99
100 /** Get the beacon at the center of the proximity zone.
101 * @return beacon at the center of the proximity zone
102 */
103 public ExtendedPositionProvider getBeacon() {
104 return beacon;
105 }
106
107 /** Get the observer for the spacecraft.
108 * @return observer for the spacecraft
109 */
110 public ExtendedPositionProvider getObserver() {
111 return observer;
112 }
113
114 /** Get the proximity angle (rad).
115 * @return the proximity angle
116 */
117 public T getProximityAngle() {
118 return proximityAngle;
119 }
120
121 /** Compute the value of the switching function.
122 * <p>
123 * This function measures the angular separation between beacon and spacecraft
124 * as seen from the observer minus the proximity angle. It therefore triggers
125 * decreasing events when the spacecraft enters the proximity zone and increasing
126 * events when it leaves the proximity zone.
127 * </p>
128 * <p>
129 * No shadowing effect is taken into account, so this method is computed and
130 * may trigger events even when the spacecraft is below horizon for an observer
131 * which is a ground station. If such effects must be taken into account the
132 * detector must be associated with a {@link EventEnablingPredicateFilter predicate
133 * filter} where the {@link EnablingPredicate predicate function} is based on elevation.
134 * </p>
135 * @param s the current state information: date, kinematics, attitude
136 * @return value of the switching function
137 */
138 public T g(final FieldSpacecraftState<T> s) {
139 final FieldVector3D<T> sPos = s.getPosition();
140 final FieldVector3D<T> bP = beacon.getPosition(s.getDate(), s.getFrame());
141 final FieldVector3D<T> oP = observer.getPosition(s.getDate(), s.getFrame());
142 final T separation = FieldVector3D.angle(sPos.subtract(oP), bP.subtract(oP));
143 return separation.subtract(proximityAngle);
144 }
145
146 }