Class BaseRangeRateIonosphericDelayModifier
java.lang.Object
org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
- Direct Known Subclasses:
BistaticRangeRateIonosphericDelayModifier,RangeRateIonosphericDelayModifier
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
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Constructor Summary
ConstructorsModifierConstructorDescriptionprotectedBaseRangeRateIonosphericDelayModifier(IonosphericModel model, double freq) Constructor. -
Method Summary
Modifier and TypeMethodDescriptionGet the name of the effect modifying the measurement.protected IonosphericModelGet the ionospheric delay model.Get the drivers for this modifier parameters.protected <T extends CalculusFieldElement<T>>
TrangeRateErrorIonosphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Ionosphere.protected doublerangeRateErrorIonosphericModel(Observer station, SpacecraftState state) Compute the measurement error due to Ionosphere.
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Constructor Details
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BaseRangeRateIonosphericDelayModifier
Constructor.- Parameters:
model- Ionospheric delay model appropriate for the current range-rate measurement method.freq- frequency of the signal in Hz
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Method Details
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getEffectName
Get the name of the effect modifying the measurement.- Returns:
- name of the effect modifying the measurement
- Since:
- 13.0
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getIonoModel
Get the ionospheric delay model.- Returns:
- ionospheric delay model
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rangeRateErrorIonosphericModel
Compute the measurement error due to Ionosphere.- Parameters:
station- stationstate- spacecraft state- Returns:
- the measurement error due to Ionosphere
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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- stationstate- spacecraft stateparameters- ionospheric model parameters- Returns:
- the measurement error due to Ionosphere
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getParametersDrivers
Get the drivers for this modifier parameters.- Returns:
- drivers for this modifier parameters
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