1   /* Copyright 2013 Applied Defense Solutions, Inc.
2    * Licensed to CS Communication & Systèmes (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.handlers;
18  
19  import org.hipparchus.ode.events.Action;
20  import org.orekit.propagation.SpacecraftState;
21  import org.orekit.propagation.events.EventDetector;
22  import org.orekit.time.AbsoluteDate;
23  
24  
25  /**
26   * An interface defining how to override event handling behavior in the standard
27   * propagator eventing classes without requiring subclassing.  In cases where
28   * one wishes to use anonymous classes rather than explicit subclassing this
29   * allows for a more direct way to override the behavior.  Event classes have to
30   * specifically support this capability.
31   *
32   * @author Hank Grabowski
33   *
34   * @param <T> object type that the handler is called from
35   * @since 6.1
36   */
37  public interface EventHandler<T extends EventDetector> {
38  
39      /** Initialize event handler at the start of a propagation.
40       * <p>
41       * This method is called once at the start of the propagation. It
42       * may be used by the event handler to initialize some internal data
43       * if needed.
44       * </p>
45       * <p>
46       * The default implementation does nothing
47       * </p>
48       * @param initialState initial state
49       * @param target target date for the propagation
50       * @param detector event detector related to the event handler
51       *
52       */
53      default void init(SpacecraftState initialState, AbsoluteDate target, final T detector) {
54          // nothing by default
55      }
56  
57      /**
58       * eventOccurred method mirrors the same interface method as in {@link EventDetector}
59       * and its subclasses, but with an additional parameter that allows the calling
60       * method to pass in an object from the detector which would have potential
61       * additional data to allow the implementing class to determine the correct
62       * return state.
63       *
64       * @param s SpaceCraft state to be used in the evaluation
65       * @param detector object with appropriate type that can be used in determining correct return state
66       * @param increasing with the event occurred in an "increasing" or "decreasing" slope direction
67       * @return the Action that the calling detector should pass back to the evaluation system
68       *
69       */
70      Action eventOccurred(SpacecraftState s, T detector, boolean increasing);
71  
72      /** Reset the state prior to continue propagation.
73       * <p>This method is called after the step handler has returned and
74       * before the next step is started, but only when {@link
75       * #eventOccurred} has itself returned the {@link Action#RESET_STATE}
76       * indicator. It allows the user to reset the state for the next step,
77       * without perturbing the step handler of the finishing step. If the
78       * {@link #eventOccurred} never returns the {@link Action#RESET_STATE}
79       * indicator, this function will never be called, and it is safe to simply return null.</p>
80       * <p>
81       * The default implementation simply return its argument.
82       * </p>
83       * @param detector object with appropriate type that can be used in determining correct return state
84       * @param oldState old state
85       * @return new state
86       */
87      default SpacecraftState resetState(T detector, SpacecraftState oldState) {
88          return oldState;
89      }
90  
91  }