org.orekit.propagation.analytical.gnss

Class GalileoPropagator.Builder

java.lang.Object

org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder

Enclosing class:

GalileoPropagator

public static class GalileoPropagator.Builder
extends Object

This nested class aims at building a GalileoPropagator.

It implements the classical builder pattern.

Constructor Summary

Constructors

Constructor and Description
Builder(GalileoOrbitalElements galileoOrbElt) Initializes the builder.
Builder(GalileoOrbitalElements galileoOrbElt, Frames frames) Initializes the builder.

Method Summary

Modifier and Type	Method and Description
GalileoPropagator.Builder	attitudeProvider(AttitudeProvider userProvider) Sets the attitude provider.
GalileoPropagator	build() Finalizes the build.
GalileoPropagator.Builder	ecef(Frame bodyFixed) Sets the Earth Centered Earth Fixed frame.
GalileoPropagator.Builder	eci(Frame inertial) Sets the Earth Centered Inertial frame used for propagation.
GalileoPropagator.Builder	mass(double userMass) Sets the mass.

Methods inherited from class java.lang.Object

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

Constructor Detail

Builder

@DefaultDataContext
public Builder(GalileoOrbitalElements galileoOrbElt)

Initializes the builder.

The Galileo orbital elements is the only requested parameter to build a GalileoPropagator.

The attitude provider is set by default to the DEFAULT_LAW in the default data context.
The mass is set by default to the DEFAULT_MASS.
The ECI frame is set by default to the EME2000 frame in the default data context.
The ECEF frame is set by default to the CIO/2010-based ITRF simple EOP in the default data context.

This constructor uses the default data context. Another data context can be set using Builder(final GalileoOrbitalElements gpsOrbElt, final Frames frames)

Parameters:

galileoOrbElt - the Galileo orbital elements to be used by the Galileo propagator.

See Also:

attitudeProvider(AttitudeProvider provider), mass(double mass), eci(Frame inertial), ecef(Frame bodyFixed)

Builder

public Builder(GalileoOrbitalElements galileoOrbElt,
               Frames frames)

Initializes the builder.

The Galileo orbital elements is the only requested parameter to build a GalileoPropagator.

The attitude provider is set by default to the DEFAULT_LAW.
The mass is set by default to the DEFAULT_MASS.
The ECI frame is set by default to the EME2000 frame.
The ECEF frame is set by default to the CIO/2010-based ITRF simple EOP.

Parameters:

galileoOrbElt - the Galileo orbital elements to be used by the Galileo propagator.

frames - to use building the propagator.

Since:

10.1

See Also:

attitudeProvider(AttitudeProvider provider), mass(double mass), eci(Frame inertial), ecef(Frame bodyFixed)

Method Detail

attitudeProvider

public GalileoPropagator.Builder attitudeProvider(AttitudeProvider userProvider)

Sets the attitude provider.

Parameters:

userProvider - the attitude provider

Returns:

the updated builder

mass

public GalileoPropagator.Builder mass(double userMass)

Sets the mass.

Parameters:

userMass - the mass (in kg)

Returns:

the updated builder

eci

public GalileoPropagator.Builder eci(Frame inertial)

Sets the Earth Centered Inertial frame used for propagation.

Parameters:

inertial - the ECI frame

Returns:

the updated builder

ecef

public GalileoPropagator.Builder ecef(Frame bodyFixed)

Sets the Earth Centered Earth Fixed frame.

Parameters:

bodyFixed - the ECEF frame

Returns:

the updated builder

build

public GalileoPropagator build()

Finalizes the build.

Returns:

the built GalileoPropagator