org.orekit.propagation.numerical

Class GLONASSNumericalPropagatorBuilder

java.lang.Object

org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder

public class GLONASSNumericalPropagatorBuilder
extends Object

This nested class aims at building a GLONASSNumericalPropagator.

It implements the classical builder pattern.

Since:

11.0

Author:

Bryan Cazabonne

Constructor Summary

Constructors

Constructor and Description
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator integrator, GLONASSOrbitalElements glonassOrbElt, boolean isAccAvailable) Initializes the builder.
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator integrator, GLONASSOrbitalElements glonassOrbElt, boolean isAccAvailable, DataContext context) Initializes the builder.

Method Summary

Modifier and Type	Method and Description
GLONASSNumericalPropagatorBuilder	attitudeProvider(AttitudeProvider userProvider) Sets the attitude provider.
GLONASSNumericalPropagator	build() Finalizes the build.
GLONASSNumericalPropagatorBuilder	eci(Frame inertial) Sets the Earth Centered Inertial frame used for propagation.
GLONASSNumericalPropagatorBuilder	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

GLONASSNumericalPropagatorBuilder

@DefaultDataContext
public GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator integrator,
                                                             GLONASSOrbitalElements glonassOrbElt,
                                                             boolean isAccAvailable)

Initializes the builder.

The attitude provider is set by default to EME2000 aligned in the default data context.
The mass is set by default to the DEFAULT_MASS.
The data context is by default to the default data context.
The ECI frame is set by default to the EME2000 frame in the default data context.

Parameters:

integrator - 4th order Runge-Kutta as recommended by GLONASS ICD

glonassOrbElt - the GLONASS orbital elements to be used by the GLONASSNumericalPropagator.

isAccAvailable - flag for availability of the projections of accelerations transmitted within the navigation message

See Also:

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

GLONASSNumericalPropagatorBuilder

public GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator integrator,
                                         GLONASSOrbitalElements glonassOrbElt,
                                         boolean isAccAvailable,
                                         DataContext context)

Initializes the builder.

The attitude provider is set by default to EME2000 aligned in the provided 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.

Parameters:

integrator - 4th order Runge-Kutta as recommended by GLONASS ICD

glonassOrbElt - the GLONASS orbital elements to be used by the GLONASSNumericalPropagator.

isAccAvailable - flag for availability of the projections of accelerations transmitted within the navigation message

context - data context

See Also:

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

Method Detail

attitudeProvider

public GLONASSNumericalPropagatorBuilder attitudeProvider(AttitudeProvider userProvider)

Sets the attitude provider.

Parameters:

userProvider - the attitude provider

Returns:

the updated builder

mass

public GLONASSNumericalPropagatorBuilder mass(double userMass)

Sets the mass.

Parameters:

userMass - the mass (in kg)

Returns:

the updated builder

eci

public GLONASSNumericalPropagatorBuilder eci(Frame inertial)

Sets the Earth Centered Inertial frame used for propagation.

Parameters:

inertial - the ECI frame

Returns:

the updated builder

build

public GLONASSNumericalPropagator build()

Finalizes the build.

Returns:

the built Glonass numerical propagator