AngularMeasurement.java
/* Copyright 2022-2026 Romain Serra
* 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
* limitations under the License.
*/
package org.orekit.estimation.measurements;
import java.util.Arrays;
import java.util.Collections;
import java.util.Map;
import org.hipparchus.analysis.differentiation.Gradient;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.MathUtils;
import org.orekit.frames.Frame;
import org.orekit.signal.FieldAdjustableEmitterSignalTimer;
import org.orekit.signal.FieldSignalReceptionCondition;
import org.orekit.signal.SignalReceptionCondition;
import org.orekit.signal.SignalTravelTimeModel;
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.TimeSpanMap;
/** Abstract class for ground-based angular measurements, when the sensor receives the signal.
*
* @author Romain Serra
* @since 14.0
*/
public abstract class AngularMeasurement<T extends SignalBasedMeasurement<T>> extends SignalBasedMeasurement<T> {
/** Simple constructor.
* @param signalTravelTimeModel signal travel time model
* @param date date of the measurement
* @param angular observed value
* @param measurementQuality measurement quality as used in estimation (in Orekit, the crossed-terms
* of the covariance matrix are only used by Kalman filters, not least squares)
* @param satellite satellite related to this measurement
*/
protected AngularMeasurement(final AbsoluteDate date,
final double[] angular, final MeasurementQuality measurementQuality,
final SignalTravelTimeModel signalTravelTimeModel,
final ObservableSatellite satellite) {
super(date, false, angular, measurementQuality, signalTravelTimeModel, Collections.singletonList(satellite));
}
/**
* Compute the signal emission date.
* @param frame frame where to perform signal propagation
* @param receiverPosition signal receiver position at reception
* @param receptionDate reception date
* @param emitter signal emitter
* @return emission date
*/
protected AbsoluteDate computeEmissionDate(final Frame frame, final Vector3D receiverPosition,
final AbsoluteDate receptionDate, final PVCoordinatesProvider emitter) {
final SignalReceptionCondition receptionCondition = new SignalReceptionCondition(receptionDate,
receiverPosition, frame);
final double signalTravelTime = getSignalTravelTimeModel().getAdjustableEmitterComputer(emitter)
.computeDelay(receptionCondition, receptionDate);
return receptionDate.shiftedBy(-signalTravelTime);
}
/**
* Compute the signal emission date.
* @param frame frame where to perform signal propagation
* @param receiverPosition signal receiver position at reception
* @param receptionDate reception date
* @param emitter signal emitter
* @return emission date
*/
protected FieldAbsoluteDate<Gradient> computeEmissionDateField(final Frame frame,
final FieldVector3D<Gradient> receiverPosition,
final FieldAbsoluteDate<Gradient> receptionDate,
final FieldPVCoordinatesProvider<Gradient> emitter) {
final FieldAdjustableEmitterSignalTimer<Gradient> fieldAdjustableEmitterSignalTimer = getSignalTravelTimeModel().
getFieldAdjustableEmitterComputer(receptionDate.getField(), emitter);
final FieldSignalReceptionCondition<Gradient> receptionCondition = new FieldSignalReceptionCondition<>(receptionDate,
receiverPosition, frame);
final Gradient signalTravelTime = fieldAdjustableEmitterSignalTimer.computeDelay(receptionCondition,
receptionDate);
return receptionDate.shiftedBy(signalTravelTime.negate());
}
/**
* Wrap angle according to observed one.
* @param baseAngle base angle
* @return wrapped angle
*/
protected double wrapFirstAngle(final double baseAngle) {
final double twoPiWrap = MathUtils.normalizeAngle(baseAngle, getObservedValue()[0]) - baseAngle;
return baseAngle + twoPiWrap;
}
/**
* Wrap angle according to observed one.
* @param baseAngle base angle
* @return wrapped angle
*/
protected Gradient wrapFirstAngle(final Gradient baseAngle) {
final double twoPiWrap = MathUtils.normalizeAngle(baseAngle.getReal(), getObservedValue()[0]) - baseAngle.getReal();
return baseAngle.add(twoPiWrap);
}
/**
* Method filling estimated measurement.
* @param firstAngle first angle
* @param secondAngle second angle
* @param paramIndices mapping between parameter name and variable index
* @param estimatedMeasurement object to fill
*/
protected void fillEstimatedMeasurement(final Gradient firstAngle, final Gradient secondAngle,
final Map<String, Integer> paramIndices, final EstimatedMeasurement<T> estimatedMeasurement) {
// azimuth - elevation values
final Gradient wrappedAngle = wrapFirstAngle(firstAngle);
estimatedMeasurement.setEstimatedValue(wrappedAngle.getValue(), secondAngle.getValue());
// First order derivatives of azimuth/elevation with respect to state
final double[] azDerivatives = firstAngle.getGradient();
final double[] elDerivatives = secondAngle.getGradient();
fillDerivatives(azDerivatives, elDerivatives, paramIndices, estimatedMeasurement);
}
/**
* Method filling derivatives in the estimated measurement.
* @param firstAngleDerivatives first angle derivatives
* @param secondAngleDerivatives second angle derivatives
* @param paramIndices mapping between parameter name and variable index
* @param estimatedMeasurement object to fill
*/
protected void fillDerivatives(final double[] firstAngleDerivatives, final double[] secondAngleDerivatives,
final Map<String, Integer> paramIndices, final EstimatedMeasurement<T> estimatedMeasurement) {
estimatedMeasurement.setStateDerivatives(0,
Arrays.copyOfRange(firstAngleDerivatives, 0, 6), Arrays.copyOfRange(secondAngleDerivatives, 0, 6));
// Set first order derivatives of azimuth/elevation with respect to state
for (final ParameterDriver driver : getParametersDrivers()) {
for (TimeSpanMap.Span<String> span = driver.getNamesSpanMap().getFirstSpan(); span != null; span = span.next()) {
final Integer index = paramIndices.get(span.getData());
if (index != null) {
estimatedMeasurement.setParameterDerivatives(driver, span.getStart(), firstAngleDerivatives[index],
secondAngleDerivatives[index]);
}
}
}
}
}