ContinuousScheduler.java
/* Copyright 2002-2019 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
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*
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package org.orekit.estimation.measurements.generation;
import java.util.List;
import java.util.SortedSet;
import java.util.TreeSet;
import org.orekit.estimation.measurements.ObservedMeasurement;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.sampling.OrekitStepInterpolator;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.DatesSelector;
/** {@link Scheduler} generating measurements sequences continuously.
* <p>
* Continuous schedulers continuously generate measurements following a repetitive pattern.
* The repetitive pattern can be either a continuous stream of measurements separated by
* a constant step (for example one measurement every 60s), or several sequences of measurements
* at high rate up to a maximum number, with a rest period between sequences (for example
* sequences of up to 256 measurements every 100ms with 300s between each sequence).
* </p>
* @param <T> the type of the measurement
* @author Luc Maisonobe
* @since 9.3
*/
public class ContinuousScheduler<T extends ObservedMeasurement<T>> extends AbstractScheduler<T> {
/** Simple constructor.
* @param builder builder for individual measurements
* @param selector selector for dates
*/
public ContinuousScheduler(final MeasurementBuilder<T> builder, final DatesSelector selector) {
super(builder, selector);
}
/** {@inheritDoc} */
@Override
public SortedSet<T> generate(final List<OrekitStepInterpolator> interpolators) {
// select dates in the current step, using arbitrarily interpolator 0
// as all interpolators cover the same range
final List<AbsoluteDate> dates = getSelector().selectDates(interpolators.get(0).getPreviousState().getDate(),
interpolators.get(0).getCurrentState().getDate());
// generate measurements when feasible
final SortedSet<T> measurements = new TreeSet<>();
for (final AbsoluteDate date : dates) {
// interpolate states at measurement date
final SpacecraftState[] states = new SpacecraftState[interpolators.size()];
for (int i = 0; i < states.length; ++i) {
states[i] = interpolators.get(i).getInterpolatedState(date);
}
// generate measurement
measurements.add(getBuilder().build(states));
}
return measurements;
}
}