BaseRangeIonosphericDelayModifier.java
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package org.orekit.estimation.measurements.modifiers;
import java.util.List;
import org.hipparchus.CalculusFieldElement;
import org.orekit.estimation.measurements.GroundStation;
import org.orekit.frames.TopocentricFrame;
import org.orekit.models.earth.ionosphere.IonosphericModel;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.SpacecraftState;
import org.orekit.utils.ParameterDriver;
/** Base class modifying theoretical range measurement with ionospheric delay.
* The effect of ionospheric correction on the range is directly computed
* through the computation of the ionospheric delay.
*
* The ionospheric delay depends on the frequency of the signal (GNSS, VLBI, ...).
* For optical measurements (e.g. SLR), the ray is not affected by ionosphere charged particles.
* <p>
* Since 10.0, state derivatives and ionospheric parameters derivates are computed
* using automatic differentiation.
* </p>
* @author Joris Olympio
* @since 11.2
*/
public abstract class BaseRangeIonosphericDelayModifier {
/** Ionospheric delay model. */
private final IonosphericModel ionoModel;
/** Frequency [Hz]. */
private final double frequency;
/** Constructor.
*
* @param model Ionospheric delay model appropriate for the current range-rate measurement method.
* @param freq frequency of the signal in Hz
*/
protected BaseRangeIonosphericDelayModifier(final IonosphericModel model, final double freq) {
this.ionoModel = model;
this.frequency = freq;
}
/** Get the ionospheric delay model.
* @return ionospheric delay model
*/
protected IonosphericModel getIonoModel() {
return ionoModel;
}
/** Compute the measurement error due to Ionosphere.
* @param station station
* @param state spacecraft state
* @return the measurement error due to Ionosphere
*/
protected double rangeErrorIonosphericModel(final GroundStation station, final SpacecraftState state) {
// Base frame associated with the station
final TopocentricFrame baseFrame = station.getBaseFrame();
// delay in meters
final double delay = ionoModel.pathDelay(state, baseFrame, frequency, ionoModel.getParameters());
return delay;
}
/** Compute the measurement error due to Ionosphere.
* @param <T> type of the elements
* @param station station
* @param state spacecraft state
* @param parameters ionospheric model parameters
* @return the measurement error due to Ionosphere
*/
protected <T extends CalculusFieldElement<T>> T rangeErrorIonosphericModel(final GroundStation station,
final FieldSpacecraftState<T> state,
final T[] parameters) {
// Base frame associated with the station
final TopocentricFrame baseFrame = station.getBaseFrame();
// delay in meters
final T delay = ionoModel.pathDelay(state, baseFrame, frequency, parameters);
return delay;
}
/** Get the drivers for this modifier parameters.
* @return drivers for this modifier parameters
*/
public List<ParameterDriver> getParametersDrivers() {
return ionoModel.getParametersDrivers();
}
}