Class BaseRangeRateIonosphericDelayModifier

java.lang.Object
org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Direct Known Subclasses:
BistaticRangeRateIonosphericDelayModifier, RangeRateIonosphericDelayModifier

public abstract class BaseRangeRateIonosphericDelayModifier extends Object
Base class modifying theoretical range-rate measurement with ionospheric delay. The effect of ionospheric correction on the range-rate is directly computed through the computation of the ionospheric delay difference with respect to time. 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

    • BaseRangeRateIonosphericDelayModifier

      protected BaseRangeRateIonosphericDelayModifier(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
    • rangeRateErrorIonosphericModel

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

      protected <T extends CalculusFieldElement<T>> T rangeRateErrorIonosphericModel(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