Package org.orekit.propagation.analytical.gnss

Class GNSSPropagatorBuilder<O extends GNSSOrbitalElements<O>>

java.lang.Object

org.orekit.propagation.conversion.AbstractPropagatorBuilder<GNSSPropagator<O>,O,GNSSOrbitalElementsFactory<O>>

org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder<GNSSPropagator<O>,O,GNSSOrbitalElementsFactory<O>>

org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder<O>

Type Parameters:

O - type of the orbital elements

All Implemented Interfaces:

Cloneable, PropagatorBuilder

public class GNSSPropagatorBuilder<O extends GNSSOrbitalElements<O>>
extends AbstractAnalyticalPropagatorBuilder<GNSSPropagator<O>,O,GNSSOrbitalElementsFactory<O>>

Builder for GNSSPropagator.

Since:

11.0

Author:

Pascal Parraud, Luc Maisonobe

Constructor Summary

Constructors

Constructor	Description
GNSSPropagatorBuilder(GNSSOrbitalElementsFactory<O> factory)	Initializes the builder.

Method Summary

Modifier and Type	Method	Description
GNSSPropagator<O>	buildPropagator()	Build a propagator from current value of selected normalized parameters.
GNSSPropagator<O>	buildPropagator(double[] normalizedParameters)	Build a propagator.

Methods inherited from class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder

addImpulseManeuver, buildLeastSquaresModel, clearImpulseManeuvers, getImpulseManeuvers

Methods inherited from class org.orekit.propagation.conversion.AbstractPropagatorBuilder

addAdditionalDerivativesProvider, addPropagationParameters, clone, deselectDynamicParameters, getAdditionalDerivativesProviders, getAttitudeProvider, getMass, getOrbitalParameterFactory, getPropagationParametersDrivers, getSelectedNormalizedParameters, resetOrbit, setAttitudeProvider, setMass, setParameters

Methods inherited from class java.lang.Object

equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Details

GNSSPropagatorBuilder

public GNSSPropagatorBuilder(GNSSOrbitalElementsFactory<O> factory)

Initializes the builder.

The attitude provider is set by default to be aligned with the provided inertial frame. This can be changed after construction by calling setAttitudeProvider

The mass is set to the DEFAULT_MASS. This can be changed after construction by calling setMass

Parameters:

factory - factory for initial orbit

Method Details

buildPropagator

public GNSSPropagator<O> buildPropagator(double[] normalizedParameters)

Build a propagator.

Specified by:

buildPropagator in interface PropagatorBuilder

Specified by:

buildPropagator in class AbstractPropagatorBuilder<GNSSPropagator<O extends GNSSOrbitalElements<O>>,O extends GNSSOrbitalElements<O>,GNSSOrbitalElementsFactory<O extends GNSSOrbitalElements<O>>>

Parameters:

normalizedParameters - normalized values for the selected parameters

Returns:

an initialized propagator

buildPropagator

public GNSSPropagator<O> buildPropagator()

Build a propagator from current value of selected normalized parameters.

Specified by:

buildPropagator in interface PropagatorBuilder

Overrides:

buildPropagator in class AbstractPropagatorBuilder<GNSSPropagator<O extends GNSSOrbitalElements<O>>,O extends GNSSOrbitalElements<O>,GNSSOrbitalElementsFactory<O extends GNSSOrbitalElements<O>>>

Returns:

an initialized propagator