Class SsrVtecIonosphericModel
- java.lang.Object
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- org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
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- All Implemented Interfaces:
IonosphericModel
,ParameterDriversProvider
public class SsrVtecIonosphericModel extends Object implements IonosphericModel
Ionospheric model based on SSR IM201 message.Within this message, the ionospheric VTEC is provided using spherical harmonic expansions. For a given ionospheric layer, the slant TEC value is calculated using the satellite elevation and the height of the corresponding layer. The total slant TEC is computed by the sum of the individual slant TEC for each layer.
- Since:
- 11.0
- Author:
- Bryan Cazabonne
- See Also:
- "IGS State Space Representation (SSR) Format, Version 1.00, October 2020."
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Constructor Summary
Constructors Constructor Description SsrVtecIonosphericModel(SsrIm201 vtecMessage)
Constructor.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description List<ParameterDriver>
getParametersDrivers()
Get the drivers for parameters.<T extends CalculusFieldElement<T>>
TpathDelay(FieldSpacecraftState<T> state, TopocentricFrame baseFrame, double frequency, T[] parameters)
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.double
pathDelay(SpacecraftState state, TopocentricFrame baseFrame, double frequency, double[] parameters)
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.-
Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
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Methods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
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Constructor Detail
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SsrVtecIonosphericModel
public SsrVtecIonosphericModel(SsrIm201 vtecMessage)
Constructor.- Parameters:
vtecMessage
- SSR Ionosphere VTEC Spherical Harmonics Message.
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Method Detail
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pathDelay
public double pathDelay(SpacecraftState state, TopocentricFrame baseFrame, double frequency, double[] parameters)
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.This method is intended to be used for orbit determination issues. In that respect, if the elevation is below 0° the path delay will be equal to zero.
For individual use of the ionospheric model (i.e. not for orbit determination), another method signature can be implemented to compute the path delay for any elevation angle.
- Specified by:
pathDelay
in interfaceIonosphericModel
- Parameters:
state
- spacecraft statebaseFrame
- base frame associated with the stationfrequency
- frequency of the signal in Hzparameters
- ionospheric model parameters at state date- Returns:
- the path delay due to the ionosphere in m
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pathDelay
public <T extends CalculusFieldElement<T>> T pathDelay(FieldSpacecraftState<T> state, TopocentricFrame baseFrame, double frequency, T[] parameters)
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.This method is intended to be used for orbit determination issues. In that respect, if the elevation is below 0° the path delay will be equal to zero.
For individual use of the ionospheric model (i.e. not for orbit determination), another method signature can be implemented to compute the path delay for any elevation angle.
- Specified by:
pathDelay
in interfaceIonosphericModel
- Type Parameters:
T
- type of the elements- Parameters:
state
- spacecraft statebaseFrame
- base frame associated with the stationfrequency
- frequency of the signal in Hzparameters
- ionospheric model parameters at state date- Returns:
- the path delay due to the ionosphere in m
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getParametersDrivers
public List<ParameterDriver> getParametersDrivers()
Get the drivers for parameters.- Specified by:
getParametersDrivers
in interfaceParameterDriversProvider
- Returns:
- drivers for parameters
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