Class BaseRangeIonosphericDelayModifier

java.lang.Object
org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Direct Known Subclasses:
BistaticRangeIonosphericDelayModifier, RangeIonosphericDelayModifier

public abstract class BaseRangeIonosphericDelayModifier extends Object
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.

Since 10.0, state derivatives and ionospheric parameters derivates are computed using automatic differentiation.

Since:
11.2
Author:
Joris Olympio
  • Constructor Details

    • BaseRangeIonosphericDelayModifier

      protected BaseRangeIonosphericDelayModifier(IonosphericModel model, double freq)
      Constructor.
      Parameters:
      model - Ionospheric delay model appropriate for the current range-rate measurement method.
      freq - frequency of the signal in Hz
  • Method Details

    • getEffectName

      public String getEffectName()
      Get the name of the effect modifying the measurement.
      Returns:
      name of the effect modifying the measurement
      Since:
      13.0
    • getIonoModel

      protected IonosphericModel getIonoModel()
      Get the ionospheric delay model.
      Returns:
      ionospheric delay model
    • rangeErrorIonosphericModel

      protected double rangeErrorIonosphericModel(Observer station, SpacecraftState state)
      Compute the measurement error due to Ionosphere.
      Parameters:
      station - station
      state - spacecraft state
      Returns:
      the measurement error due to Ionosphere
    • rangeErrorIonosphericModel

      protected <T extends CalculusFieldElement<T>> T rangeErrorIonosphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters)
      Compute the measurement error due to Ionosphere.
      Type Parameters:
      T - type of the elements
      Parameters:
      station - station
      state - spacecraft state
      parameters - ionospheric model parameters
      Returns:
      the measurement error due to Ionosphere
    • getParametersDrivers

      public List<ParameterDriver> getParametersDrivers()
      Get the drivers for this modifier parameters.
      Returns:
      drivers for this modifier parameters