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();
    }

}