AttitudeProvider.java
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* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
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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.attitudes;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.Field;
import org.hipparchus.geometry.euclidean.threed.FieldRotation;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.orekit.frames.Frame;
import org.orekit.propagation.events.EventDetector;
import org.orekit.propagation.events.EventDetectorsProvider;
import org.orekit.propagation.events.FieldEventDetector;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
import org.orekit.utils.FieldPVCoordinatesProvider;
import org.orekit.utils.PVCoordinatesProvider;
import org.orekit.utils.ParameterDriver;
import org.orekit.utils.ParameterDriversProvider;
import java.util.ArrayList;
import java.util.List;
import java.util.stream.Stream;
/** This interface represents an attitude provider model set.
* <p>An attitude provider provides a way to compute an {@link Attitude Attitude}
* from an date and position-velocity local provider.</p>
* @author Véronique Pommier-Maurussane
*/
public interface AttitudeProvider extends EventDetectorsProvider, ParameterDriversProvider {
/** Compute the attitude corresponding to an orbital state.
* @param pvProv local position-velocity provider around current date
* @param date current date
* @param frame reference frame from which attitude is computed
* @return attitude on the specified date and position-velocity state
*/
Attitude getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame);
/** Compute the attitude corresponding to an orbital state.
* @param pvProv local position-velocity provider around current date
* @param date current date
* @param frame reference frame from which attitude is computed
* @param <T> type of the field elements
* @return attitude on the specified date and position-velocity state
* @since 9.0
*/
<T extends CalculusFieldElement<T>> FieldAttitude<T> getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame);
/** Compute the attitude-related rotation corresponding to an orbital state.
* @param pvProv local position-velocity provider around current date
* @param date current date
* @param frame reference frame from which attitude is computed
* @return attitude-related rotation on the specified date and position-velocity state
* @since 12.0
*/
default Rotation getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) {
return getAttitude(pvProv, date, frame).getRotation();
}
/** Compute the attitude-related rotation corresponding to an orbital state.
* @param pvProv local position-velocity provider around current date
* @param date current date
* @param frame reference frame from which attitude is computed
* @param <T> type of the field elements
* @return rotation on the specified date and position-velocity state
* @since 12.0
*/
default <T extends CalculusFieldElement<T>> FieldRotation<T> getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) {
return getAttitude(pvProv, date, frame).getRotation();
}
/** {@inheritDoc}
* @since 13.0
*/
@Override
default Stream<EventDetector> getEventDetectors() {
return getEventDetectors(getParametersDrivers());
}
/** {@inheritDoc}
* @since 13.0
*/
@Override
default <T extends CalculusFieldElement<T>> Stream<FieldEventDetector<T>> getFieldEventDetectors(final Field<T> field) {
return getFieldEventDetectors(field, getParametersDrivers());
}
/** {@inheritDoc}
* @since 13.0
*/
@Override
default List<ParameterDriver> getParametersDrivers() {
return new ArrayList<>();
}
}