org.orekit.propagation.conversion

Class KeplerianPropagatorBuilder

java.lang.Object

org.orekit.propagation.conversion.AbstractPropagatorBuilder

org.orekit.propagation.conversion.KeplerianPropagatorBuilder

All Implemented Interfaces:

PropagatorBuilder

public class KeplerianPropagatorBuilder
extends AbstractPropagatorBuilder

Builder for Keplerian propagator.

Since:

6.0

Author:

Pascal Parraud

Constructor Summary

Constructors

Constructor and Description
KeplerianPropagatorBuilder(double mu, Frame frame) Deprecated. as of 7.1, replaced with KeplerianPropagatorBuilder(double, Frame, OrbitType, PositionAngle)
KeplerianPropagatorBuilder(double mu, Frame frame, OrbitType orbitType, PositionAngle positionAngle) Build a new instance.

Method Summary

Methods

Modifier and Type	Method and Description
Propagator	buildPropagator(AbsoluteDate date, double[] parameters) Build a propagator.

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

addSupportedParameter, checkParameters, createInitialOrbit, getFrame, getFreeParameters, getOrbitType, getParameter, getPositionAngle, getSupportedParameters, setFreeParameters, setParameter

Methods inherited from class java.lang.Object

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

Constructor Detail

KeplerianPropagatorBuilder

@Deprecated
public KeplerianPropagatorBuilder(double mu,
                                     Frame frame)

Deprecated. as of 7.1, replaced with KeplerianPropagatorBuilder(double, Frame, OrbitType, PositionAngle)

Build a new instance.

Parameters:

mu - central attraction coefficient (m³/s²)

frame - the frame in which the orbit is propagated (must be a pseudo-inertial frame)

KeplerianPropagatorBuilder

public KeplerianPropagatorBuilder(double mu,
                          Frame frame,
                          OrbitType orbitType,
                          PositionAngle positionAngle)

Build a new instance.

Parameters:

mu - central attraction coefficient (m³/s²)

frame - the frame in which the orbit is propagated (must be a pseudo-inertial frame)

orbitType - orbit type to use

positionAngle - position angle type to use

Since:

7.1

Method Detail

buildPropagator

public Propagator buildPropagator(AbsoluteDate date,
                         double[] parameters)
                           throws OrekitException

Build a propagator.

Parameters:

date - date associated to the parameters to configure the initial state

parameters - set of position/velocity(/free) parameters to configure the propagator

Returns:

an initialized propagator

Throws:

OrekitException - if propagator cannot be build