TDOATroposphericDelayModifier.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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package org.orekit.estimation.measurements.modifiers;
import java.util.List;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.Field;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.attitudes.FrameAlignedProvider;
import org.orekit.estimation.measurements.EstimatedMeasurement;
import org.orekit.estimation.measurements.EstimatedMeasurementBase;
import org.orekit.estimation.measurements.EstimationModifier;
import org.orekit.estimation.measurements.GroundStation;
import org.orekit.estimation.measurements.TDOA;
import org.orekit.models.earth.troposphere.TroposphericModel;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.SpacecraftState;
import org.orekit.utils.Constants;
import org.orekit.utils.FieldTrackingCoordinates;
import org.orekit.utils.ParameterDriver;
import org.orekit.utils.TrackingCoordinates;
/** Class modifying theoretical TDOA measurements with tropospheric delay.
* <p>
* The effect of tropospheric correction on the TDOA is a time delay computed
* directly from the difference in tropospheric delays for each downlink.
* </p><p>
* Tropospheric delay is not frequency dependent for signals up to 15 GHz.
* </p>
* @author Pascal Parraud
* @since 11.2
*/
public class TDOATroposphericDelayModifier implements EstimationModifier<TDOA> {
/** Tropospheric delay model. */
private final TroposphericModel tropoModel;
/** Constructor.
*
* @param model tropospheric model appropriate for the current TDOA measurement method.
* @since 12.1
*/
public TDOATroposphericDelayModifier(final TroposphericModel model) {
tropoModel = model;
}
/** {@inheritDoc} */
@Override
public String getEffectName() {
return "troposphere";
}
/** Compute the measurement error due to Troposphere on a single downlink.
* @param station station
* @param state spacecraft state
* @return the measurement error due to Troposphere (s)
*/
private double timeErrorTroposphericModel(final GroundStation station, final SpacecraftState state) {
final Vector3D position = state.getPosition();
// tracking
final TrackingCoordinates trackingCoordinates =
station.getBaseFrame().getTrackingCoordinates(position, state.getFrame(), state.getDate());
// only consider measurements above the horizon
if (trackingCoordinates.getElevation() > 0) {
// Delay in meters
final double delay = tropoModel.pathDelay(trackingCoordinates,
station.getOffsetGeodeticPoint(state.getDate()),
station.getPressureTemperatureHumidity(state.getDate()),
tropoModel.getParameters(state.getDate()), state.getDate()).
getDelay();
// return delay in seconds
return delay / Constants.SPEED_OF_LIGHT;
}
return 0;
}
/** Compute the measurement error due to Troposphere on a single downlink.
* @param <T> type of the element
* @param station station
* @param state spacecraft state
* @param parameters tropospheric model parameters
* @return the measurement error due to Troposphere (s)
*/
private <T extends CalculusFieldElement<T>> T timeErrorTroposphericModel(final GroundStation station,
final FieldSpacecraftState<T> state,
final T[] parameters) {
// Field
final Field<T> field = state.getDate().getField();
final T zero = field.getZero();
// tracking
final FieldVector3D<T> pos = state.getPosition();
final FieldTrackingCoordinates<T> trackingCoordinates =
station.getBaseFrame().getTrackingCoordinates(pos, state.getFrame(), state.getDate());
// only consider measurements above the horizon
if (trackingCoordinates.getElevation().getReal() > 0) {
// delay in meters
final T delay = tropoModel.pathDelay(trackingCoordinates,
station.getOffsetGeodeticPoint(state.getDate()),
station.getPressureTemperatureHumidity(state.getDate()),
parameters, state.getDate()).
getDelay();
// return delay in seconds
return delay.divide(Constants.SPEED_OF_LIGHT);
}
return zero;
}
/** {@inheritDoc} */
@Override
public List<ParameterDriver> getParametersDrivers() {
return tropoModel.getParametersDrivers();
}
/** {@inheritDoc} */
@Override
public void modifyWithoutDerivatives(final EstimatedMeasurementBase<TDOA> estimated) {
final TDOA measurement = estimated.getObservedMeasurement();
final GroundStation primeStation = measurement.getPrimeStation();
final GroundStation secondStation = measurement.getSecondStation();
TDOAModifierUtil.modifyWithoutDerivatives(estimated, primeStation, secondStation,
this::timeErrorTroposphericModel, this);
}
/** {@inheritDoc} */
@Override
public void modify(final EstimatedMeasurement<TDOA> estimated) {
final TDOA measurement = estimated.getObservedMeasurement();
final GroundStation primeStation = measurement.getPrimeStation();
final GroundStation secondStation = measurement.getSecondStation();
final SpacecraftState state = estimated.getStates()[0];
TDOAModifierUtil.modify(estimated, tropoModel,
new ModifierGradientConverter(state, 6, new FrameAlignedProvider(state.getFrame())),
primeStation, secondStation,
this::timeErrorTroposphericModel,
this::timeErrorTroposphericModel,
this);
}
}