FieldLongitudeCrossingDetector.java
- /* Copyright 2023-2024 Alberto Ferrero
- * Licensed to CS GROUP (CS) under one or more
- * contributor license agreements. See the NOTICE file distributed with
- * this work for additional information regarding copyright ownership.
- * Alberto Ferrero licenses this file to You under the Apache License, Version 2.0
- * (the "License"); you may not use this file except in compliance with
- * the License. You may obtain a copy of the License at
- *
- * http://www.apache.org/licenses/LICENSE-2.0
- *
- * Unless required by applicable law or agreed to in writing, software
- * distributed under the License is distributed on an "AS IS" BASIS,
- * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
- * See the License for the specific language governing permissions and
- * limitations under the License.
- */
- package org.orekit.propagation.events;
- import org.hipparchus.CalculusFieldElement;
- import org.hipparchus.Field;
- import org.hipparchus.util.FastMath;
- import org.hipparchus.util.MathUtils;
- import org.orekit.bodies.FieldGeodeticPoint;
- import org.orekit.bodies.OneAxisEllipsoid;
- import org.orekit.propagation.FieldSpacecraftState;
- import org.orekit.propagation.events.handlers.FieldContinueOnEvent;
- import org.orekit.propagation.events.handlers.FieldEventHandler;
- import org.orekit.propagation.events.handlers.FieldStopOnIncreasing;
- import org.orekit.time.FieldAbsoluteDate;
- /** Detector for geographic longitude crossing.
- * <p>This detector identifies when a spacecraft crosses a fixed
- * longitude with respect to a central body.</p>
- * @author Alberto Ferrero
- * @since 12.0
- * @param <T> type of the field elements
- */
- public class FieldLongitudeCrossingDetector <T extends CalculusFieldElement<T>>
- extends FieldAbstractDetector<FieldLongitudeCrossingDetector<T>, T> {
- /**
- * Body on which the longitude is defined.
- */
- private OneAxisEllipsoid body;
- /**
- * Fixed longitude to be crossed.
- */
- private final double longitude;
- /**
- * Filtering detector.
- */
- private final FieldEventEnablingPredicateFilter<T> filtering;
- /**
- * Build a new detector.
- * <p>The new instance uses default values for maximal checking interval
- * ({@link #DEFAULT_MAXCHECK}) and convergence threshold ({@link
- * #DEFAULT_THRESHOLD}).</p>
- *
- * @param field the type of numbers to use.
- * @param body body on which the longitude is defined
- * @param longitude longitude to be crossed
- */
- public FieldLongitudeCrossingDetector(final Field<T> field, final OneAxisEllipsoid body, final double longitude) {
- this(FieldAdaptableInterval.of(DEFAULT_MAXCHECK),
- field.getZero().newInstance(DEFAULT_THRESHOLD), DEFAULT_MAX_ITER, new FieldStopOnIncreasing<>(), body, longitude);
- }
- /**
- * Build a detector.
- *
- * @param maxCheck maximal checking interval (s)
- * @param threshold convergence threshold (s)
- * @param body body on which the longitude is defined
- * @param longitude longitude to be crossed
- */
- public FieldLongitudeCrossingDetector(final T maxCheck,
- final T threshold,
- final OneAxisEllipsoid body,
- final double longitude) {
- this(FieldAdaptableInterval.of(maxCheck.getReal()), threshold, DEFAULT_MAX_ITER, new FieldStopOnIncreasing<>(), body, longitude);
- }
- /**
- * Protected constructor with full parameters.
- * <p>
- * This constructor is not public as users are expected to use the builder
- * API with the various {@code withXxx()} methods to set up the instance
- * in a readable manner without using a huge amount of parameters.
- * </p>
- *
- * @param maxCheck maximum checking interval
- * @param threshold convergence threshold (s)
- * @param maxIter maximum number of iterations in the event time search
- * @param handler event handler to call at event occurrences
- * @param body body on which the longitude is defined
- * @param longitude longitude to be crossed
- */
- protected FieldLongitudeCrossingDetector(
- final FieldAdaptableInterval<T> maxCheck,
- final T threshold,
- final int maxIter,
- final FieldEventHandler<T> handler,
- final OneAxisEllipsoid body,
- final double longitude) {
- super(maxCheck, threshold, maxIter, handler);
- this.body = body;
- this.longitude = longitude;
- // we filter out spurious longitude crossings occurring at the antimeridian
- final FieldRawLongitudeCrossingDetector<T> raw = new FieldRawLongitudeCrossingDetector<>(maxCheck, threshold, maxIter,
- new FieldContinueOnEvent<>());
- final FieldEnablingPredicate<T> predicate =
- (state, detector, g) -> FastMath.abs(g).getReal() < 0.5 * FastMath.PI;
- this.filtering = new FieldEventEnablingPredicateFilter<T>(raw, predicate);
- }
- /**
- * {@inheritDoc}
- */
- @Override
- protected FieldLongitudeCrossingDetector<T> create(
- final FieldAdaptableInterval<T> newMaxCheck,
- final T newThreshold,
- final int newMaxIter,
- final FieldEventHandler<T> newHandler) {
- return new FieldLongitudeCrossingDetector<>(newMaxCheck, newThreshold, newMaxIter, newHandler,
- body, longitude);
- }
- /**
- * Get the body on which the geographic zone is defined.
- *
- * @return body on which the geographic zone is defined
- */
- public OneAxisEllipsoid getBody() {
- return body;
- }
- /**
- * Get the fixed longitude to be crossed (radians).
- *
- * @return fixed longitude to be crossed (radians)
- */
- public double getLongitude() {
- return longitude;
- }
- /**
- * {@inheritDoc}
- */
- public void init(final FieldSpacecraftState<T> s0, final FieldAbsoluteDate<T> t) {
- filtering.init(s0, t);
- }
- /**
- * Compute the value of the detection function.
- * <p>
- * The value is the longitude difference between the spacecraft and the fixed
- * longitude to be crossed, with some sign tweaks to ensure continuity.
- * These tweaks imply the {@code increasing} flag in events detection becomes
- * irrelevant here! As an example, the longitude of a prograde spacecraft
- * will always increase, but this g function will increase and decrease so it
- * will cross the zero value once per orbit, in increasing and decreasing
- * directions on alternate orbits. If eastwards and westwards crossing have to
- * be distinguished, the velocity direction has to be checked instead of looking
- * at the {@code increasing} flag.
- * </p>
- *
- * @param s the current state information: date, kinematics, attitude
- * @return longitude difference between the spacecraft and the fixed
- * longitude, with some sign tweaks to ensure continuity
- */
- public T g(final FieldSpacecraftState<T> s) {
- return filtering.g(s);
- }
- private class FieldRawLongitudeCrossingDetector <TT extends CalculusFieldElement<TT>>
- extends FieldAbstractDetector<FieldRawLongitudeCrossingDetector<TT>, TT> {
- /**
- * Protected constructor with full parameters.
- * <p>
- * This constructor is not public as users are expected to use the builder
- * API with the various {@code withXxx()} methods to set up the instance
- * in a readable manner without using a huge amount of parameters.
- * </p>
- *
- * @param maxCheck maximum checking interval
- * @param threshold convergence threshold (s)
- * @param maxIter maximum number of iterations in the event time search
- * @param handler event handler to call at event occurrences
- */
- protected FieldRawLongitudeCrossingDetector(
- final FieldAdaptableInterval<TT> maxCheck,
- final TT threshold,
- final int maxIter,
- final FieldEventHandler<TT> handler) {
- super(maxCheck, threshold, maxIter, handler);
- }
- /**
- * {@inheritDoc}
- */
- @Override
- protected FieldRawLongitudeCrossingDetector<TT> create(
- final FieldAdaptableInterval<TT> newMaxCheck,
- final TT newThreshold,
- final int newMaxIter,
- final FieldEventHandler<TT> newHandler) {
- return new FieldRawLongitudeCrossingDetector<>(newMaxCheck, newThreshold, newMaxIter, newHandler);
- }
- /**
- * Compute the value of the detection function.
- * <p>
- * The value is the longitude difference between the spacecraft and the fixed
- * longitude to be crossed, and it <em>does</em> change sign twice around
- * the central body: once at expected longitude and once at antimeridian.
- * The second sign change is a spurious one and is filtered out by the
- * outer class.
- * </p>
- *
- * @param s the current state information: date, kinematics, attitude
- * @return longitude difference between the spacecraft and the fixed
- * longitude
- */
- public TT g(final FieldSpacecraftState<TT> s) {
- // convert state to geodetic coordinates
- final FieldGeodeticPoint<TT> gp = body.transform(s.getPosition(),
- s.getFrame(), s.getDate());
- // longitude difference
- final TT zero = gp.getLongitude().getField().getZero();
- return MathUtils.normalizeAngle(gp.getLongitude().subtract(longitude), zero);
- }
- }
- }