1 /* Copyright 2002-2018 CS Systèmes d'Information
2 * Licensed to CS Systèmes d'Information (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.sampling;
18
19 import org.orekit.errors.OrekitException;
20 import org.orekit.propagation.SpacecraftState;
21 import org.orekit.time.AbsoluteDate;
22
23 /** This interface is a space-dynamics aware fixed size step handler.
24 *
25 * <p>It mirrors the <code>FixedStepHandler</code> interface from <a
26 * href="https://hipparchus.org/">Hipparchus</a> but provides
27 * a space-dynamics interface to the methods.</p>
28 * @author Luc Maisonobe
29 */
30 @FunctionalInterface
31 public interface OrekitFixedStepHandler {
32
33 /** Initialize step handler at the start of a propagation.
34 * <p>
35 * This method is called once at the start of the propagation. It
36 * may be used by the step handler to initialize some internal data
37 * if needed.
38 * </p>
39 * <p>
40 * The default implementation does nothing
41 * </p>
42 * @param s0 initial state
43 * @param t target time for the integration
44 * @exception OrekitException if step handler cannot be initialized
45 * @deprecated as of 9.0, replaced by {@link #init(SpacecraftState, AbsoluteDate, double)}
46 */
47 @Deprecated
48 default void init(SpacecraftState s0, AbsoluteDate t)
49 throws OrekitException {
50 // nothing by default
51 }
52
53 /** Initialize step handler at the start of a propagation.
54 * <p>
55 * This method is called once at the start of the propagation. It
56 * may be used by the step handler to initialize some internal data
57 * if needed.
58 * </p>
59 * <p>
60 * The default implementation currently calls the deprecated
61 * {@link #init(SpacecraftState, AbsoluteDate)} which does nothing by
62 * default. When that method is removed the default implementation will do
63 * nothing.
64 * </p>
65 * @param s0 initial state
66 * @param t target time for the integration
67 * @param step the duration in seconds of the fixed step. This value is
68 * positive even if propagation is backwards.
69 * @exception OrekitException if step handler cannot be initialized
70 * @since 9.0
71 */
72 default void init(SpacecraftState s0, AbsoluteDate t, double step)
73 throws OrekitException {
74 // as of 9.0, the default implementation calls the DEPRECATED version
75 // without a step size, which does nothing by default but may have
76 // been overridden by users
77 // When the deprecated version is removed, the default implementation
78 // will do nothing
79 init(s0, t);
80 }
81
82 /** Handle the current step.
83 * @param currentState current state at step time
84 * @param isLast if true, this is the last integration step
85 * @exception OrekitException if step cannot be handled
86 */
87 void handleStep(SpacecraftState currentState, boolean isLast)
88 throws OrekitException;
89
90 }