Package org.orekit.propagation.conversion

Class KeplerianPropagatorBuilder

java.lang.Object

org.orekit.propagation.conversion.AbstractPropagatorBuilder<T>

org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder<KeplerianPropagator>

org.orekit.propagation.conversion.KeplerianPropagatorBuilder

All Implemented Interfaces:

Cloneable, PropagatorBuilder

public class KeplerianPropagatorBuilder
extends AbstractAnalyticalPropagatorBuilder<KeplerianPropagator>

Builder for Keplerian propagator.

Since:

6.0

Author:

Pascal Parraud

Constructor Summary

Constructors

Constructor	Description
KeplerianPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale)	Build a new instance.
KeplerianPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider)	Build a new instance.

Method Summary

Modifier and Type	Method	Description
KeplerianPropagator	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, addSupportedParameters, buildPropagator, clone, createInitialOrbit, deselectDynamicParameters, getAdditionalDerivativesProviders, getAttitudeProvider, getFrame, getInitialOrbitDate, getMass, getMu, getOrbitalParametersDrivers, getOrbitType, getPositionAngleType, getPositionScale, getPropagationParametersDrivers, getSelectedNormalizedParameters, resetOrbit, setAttitudeProvider, setMass, setParameters

Methods inherited from class java.lang.Object

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

Constructor Detail

KeplerianPropagatorBuilder

public KeplerianPropagatorBuilder(Orbit templateOrbit,
                                  PositionAngleType positionAngleType,
                                  double positionScale)

Build a new instance.

The template orbit is used as a model to create initial orbit. It defines the inertial frame, the central attraction coefficient, the orbit type, and is also used together with the positionScale to convert from the normalized parameters used by the callers of this builder to the real orbital parameters. The default attitude provider is aligned with the orbit's inertial frame.

Parameters:

templateOrbit - reference orbit from which real orbits will be built

positionAngleType - position angle type to use

positionScale - scaling factor used for orbital parameters normalization (typically set to the expected standard deviation of the position)

Since:

8.0

See Also:

KeplerianPropagatorBuilder(Orbit, PositionAngleType, double, AttitudeProvider)

KeplerianPropagatorBuilder

public KeplerianPropagatorBuilder(Orbit templateOrbit,
                                  PositionAngleType positionAngleType,
                                  double positionScale,
                                  AttitudeProvider attitudeProvider)

Build a new instance.

The template orbit is used as a model to create initial orbit. It defines the inertial frame, the central attraction coefficient, the orbit type, and is also used together with the positionScale to convert from the normalized parameters used by the callers of this builder to the real orbital parameters.

Parameters:

templateOrbit - reference orbit from which real orbits will be built

positionAngleType - position angle type to use

positionScale - scaling factor used for orbital parameters normalization (typically set to the expected standard deviation of the position)

attitudeProvider - attitude law to use.

Since:

10.1

Method Detail

buildPropagator

public KeplerianPropagator buildPropagator(double[] normalizedParameters)

Build a propagator.

Specified by:

buildPropagator in interface PropagatorBuilder

Specified by:

buildPropagator in class AbstractPropagatorBuilder<KeplerianPropagator>

Parameters:

normalizedParameters - normalized values for the selected parameters

Returns:

an initialized propagator