FieldManeuverTriggersResetter.java
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*
* http://www.apache.org/licenses/LICENSE-2.0
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* Unless required by applicable law or agreed to in writing, software
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package org.orekit.forces.maneuvers.trigger;
import org.hipparchus.CalculusFieldElement;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.time.FieldAbsoluteDate;
/** Resetter for maneuver triggers.
* @param <T> type of the field elements
* @see AbstractManeuverTriggers
* @author Luc Maisonobe
* @since 11.1
*/
public interface FieldManeuverTriggersResetter<T extends CalculusFieldElement<T>> {
/** Initialization method called at propagation start.
* <p>
* The default implementation does nothing.
* </p>
* @param initialState initial spacecraft state (at the start of propagation).
* @param target date of propagation. Not equal to {@code initialState.getDate()}.
*/
default void init(FieldSpacecraftState<T> initialState, FieldAbsoluteDate<T> target) {
// nothing by default
}
/** Observe a maneuver trigger.
* <p>
* The {@code start} parameter corresponds to physical flow of time
* from past to future, not to propagation direction which can be backward.
* This means that during forward propagations, the first call will have
* {@code start} set to {@code true} and the second call will have
* {@code start} set to {@code false}, whereas in backward propagation,
* the first call will have {@code start} set to {@code false} and the second
* call will have {@code start} set to {@code true}.
* </p>
* @param state spacecraft state at trigger date (before applying the maneuver)
* @param start if true, the trigger is the start of the maneuver
*/
void maneuverTriggered(FieldSpacecraftState<T> state, boolean start);
/** Reset state as a maneuver triggers.
* @param state spacecraft state at trigger date
* @return reset state taking into account maneuver start/stop
*/
FieldSpacecraftState<T> resetState(FieldSpacecraftState<T> state);
}