MultiplexedMeasurement.java
/* Copyright 2002-2020 CS GROUP
* 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.
* CS 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
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*/
package org.orekit.estimation.measurements;
import java.util.ArrayList;
import java.util.Arrays;
import java.util.IdentityHashMap;
import java.util.List;
import java.util.Map;
import java.util.function.Function;
import org.orekit.propagation.SpacecraftState;
import org.orekit.utils.ParameterDriver;
import org.orekit.utils.ParameterDriversList;
import org.orekit.utils.TimeStampedPVCoordinates;
/** Class multiplexing several measurements as one.
* <p>
* Date comes from the first measurement, observed and estimated
* values result from gathering all underlying measurements values.
*
* @author Luc Maisonobe
* @since 10.1
*/
public class MultiplexedMeasurement extends AbstractMeasurement<MultiplexedMeasurement> {
/** Multiplexed measurements. */
private final List<ObservedMeasurement<?>> observedMeasurements;
/** Multiplexed measurements. */
private final List<EstimatedMeasurement<?>> estimatedMeasurements;
/** Multiplexed parameters drivers. */
private ParameterDriversList parametersDrivers;
/** Total dimension. */
private final int dimension;
/** Total number of satellites involved. */
private final int nbSat;
/** States mapping. */
private final int[][] mapping;
/** Simple constructor.
* @param measurements measurements to multiplex
* @since 10.1
*/
public MultiplexedMeasurement(final List<ObservedMeasurement<?>> measurements) {
super(measurements.get(0).getDate(),
multiplex(measurements, m -> m.getObservedValue()),
multiplex(measurements, m -> m.getTheoreticalStandardDeviation()),
multiplex(measurements, m -> m.getBaseWeight()),
multiplex(measurements));
this.observedMeasurements = measurements;
this.estimatedMeasurements = new ArrayList<>();
this.parametersDrivers = new ParameterDriversList();
// gather parameters drivers
int dim = 0;
for (final ObservedMeasurement<?> m : measurements) {
for (final ParameterDriver driver : m.getParametersDrivers()) {
parametersDrivers.add(driver);
}
dim += m.getDimension();
}
parametersDrivers.sort();
for (final ParameterDriver driver : parametersDrivers.getDrivers()) {
addParameterDriver(driver);
}
this.dimension = dim;
// set up states mappings for observed satellites
final List<ObservableSatellite> deduplicated = getSatellites();
this.nbSat = deduplicated.size();
this.mapping = new int[measurements.size()][];
for (int i = 0; i < mapping.length; ++i) {
final List<ObservableSatellite> satellites = measurements.get(i).getSatellites();
mapping[i] = new int[satellites.size()];
for (int j = 0; j < mapping[i].length; ++j) {
final int index = satellites.get(j).getPropagatorIndex();
for (int k = 0; k < nbSat; ++k) {
if (deduplicated.get(k).getPropagatorIndex() == index) {
mapping[i][j] = k;
break;
}
}
}
}
}
/** Get the underlying measurements.
* @return underlying measurements
*/
public List<ObservedMeasurement<?>> getMeasurements() {
return observedMeasurements;
}
/** Get the underlying estimated measurements.
* @return underlying estimated measurements
*/
public List<EstimatedMeasurement<?>> getEstimatedMeasurements() {
return estimatedMeasurements;
}
/** {@inheritDoc} */
@Override
protected EstimatedMeasurement<MultiplexedMeasurement> theoreticalEvaluation(final int iteration, final int evaluation,
final SpacecraftState[] states) {
final SpacecraftState[] evaluationStates = new SpacecraftState[nbSat];
final List<TimeStampedPVCoordinates> participants = new ArrayList<>();
final double[] value = new double[dimension];
// loop over all multiplexed measurements
estimatedMeasurements.clear();
int index = 0;
for (int i = 0; i < observedMeasurements.size(); ++i) {
// filter states involved in the current measurement
final SpacecraftState[] filteredStates = new SpacecraftState[mapping[i].length];
for (int j = 0; j < mapping[i].length; ++j) {
filteredStates[j] = states[mapping[i][j]];
}
// perform evaluation
final EstimatedMeasurement<?> eI = observedMeasurements.get(i).estimate(iteration, evaluation, filteredStates);
estimatedMeasurements.add(eI);
// extract results
final double[] valueI = eI.getEstimatedValue();
System.arraycopy(valueI, 0, value, index, valueI.length);
index += valueI.length;
// extract states
final SpacecraftState[] statesI = eI.getStates();
for (int j = 0; j < mapping[i].length; ++j) {
evaluationStates[mapping[i][j]] = statesI[j];
}
}
// create multiplexed estimation
final EstimatedMeasurement<MultiplexedMeasurement> multiplexed =
new EstimatedMeasurement<>(this, iteration, evaluation,
evaluationStates,
participants.toArray(new TimeStampedPVCoordinates[0]));
// copy multiplexed value
multiplexed.setEstimatedValue(value);
// combine derivatives
final int stateSize = estimatedMeasurements.get(0).getStateSize();
final double[] zeroDerivative = new double[stateSize];
final double[][][] stateDerivatives = new double[nbSat][dimension][];
for (final double[][] m : stateDerivatives) {
Arrays.fill(m, zeroDerivative);
}
final Map<ParameterDriver, double[]> parametersDerivatives = new IdentityHashMap<>();
index = 0;
for (int i = 0; i < observedMeasurements.size(); ++i) {
final EstimatedMeasurement<?> eI = estimatedMeasurements.get(i);
final int idx = index;
final int dimI = eI.getObservedMeasurement().getDimension();
// state derivatives
for (int j = 0; j < mapping[i].length; ++j) {
System.arraycopy(eI.getStateDerivatives(j), 0,
stateDerivatives[mapping[i][j]], index,
dimI);
}
// parameters derivatives
eI.getDerivativesDrivers().forEach(driver -> {
final ParameterDriversList.DelegatingDriver delegating = parametersDrivers.findByName(driver.getName());
double[] derivatives = parametersDerivatives.get(delegating);
if (derivatives == null) {
derivatives = new double[dimension];
parametersDerivatives.put(delegating, derivatives);
}
System.arraycopy(eI.getParameterDerivatives(driver), 0, derivatives, idx, dimI);
});
index += dimI;
}
// set states derivatives
for (int i = 0; i < nbSat; ++i) {
multiplexed.setStateDerivatives(i, stateDerivatives[i]);
}
// set parameters derivatives
parametersDerivatives.
entrySet().
stream().
forEach(e -> multiplexed.setParameterDerivatives(e.getKey(), e.getValue()));
return multiplexed;
}
/** Multiplex measurements data.
* @param measurements measurements to multiplex
* @param extractor data extraction function
* @return multiplexed data
*/
private static double[] multiplex(final List<ObservedMeasurement<?>> measurements,
final Function<ObservedMeasurement<?>, double[]> extractor) {
// gather individual parts
final List<double[]> parts = new ArrayList<> (measurements.size());
int n = 0;
for (final ObservedMeasurement<?> measurement : measurements) {
final double[] p = extractor.apply(measurement);
parts.add(p);
n += p.length;
}
// create multiplexed data
final double[] multiplexed = new double[n];
int index = 0;
for (final double[] p : parts) {
System.arraycopy(p, 0, multiplexed, index, p.length);
index += p.length;
}
return multiplexed;
}
/** Multiplex satellites data.
* @param measurements measurements to multiplex
* @return multiplexed satellites data
*/
private static List<ObservableSatellite> multiplex(final List<ObservedMeasurement<?>> measurements) {
final List<ObservableSatellite> satellites = new ArrayList<>();
// gather all satellites, removing duplicates
for (final ObservedMeasurement<?> measurement : measurements) {
for (final ObservableSatellite satellite : measurement.getSatellites()) {
boolean searching = true;
for (int i = 0; i < satellites.size() && searching; ++i) {
// check if we already know this satellite
searching = satellite.getPropagatorIndex() != satellites.get(i).getPropagatorIndex();
}
if (searching) {
// this is a new satellite, add it to the global list
satellites.add(satellite);
}
}
}
return satellites;
}
}