Uses of Interface
org.orekit.propagation.Propagator

Packages that use Propagator

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.estimation.measurements.generation	This package provides Orbit Determination measurements generation.
org.orekit.gnss	This package provides classes related to GNSS applications.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.analytical.gnss	This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

Uses of Propagator in org.orekit.attitudes

Methods in org.orekit.attitudes with parameters of type Propagator

Modifier and Type	Method	Description
void	AttitudesSequence.registerSwitchEvents(Propagator propagator)	Register all wrapped switch events to the propagator.

Uses of Propagator in org.orekit.estimation.measurements.generation

Methods in org.orekit.estimation.measurements.generation that return Propagator

Modifier and Type	Method	Description
Propagator	Generator.getPropagator(ObservableSatellite satellite)	Get a registered propagator.

Methods in org.orekit.estimation.measurements.generation with parameters of type Propagator

Modifier and Type	Method	Description
ObservableSatellite	Generator.addPropagator(Propagator propagator)	Add a propagator.

Constructors in org.orekit.estimation.measurements.generation with parameters of type Propagator

Constructor	Description
EventBasedScheduler(MeasurementBuilder<T> builder, DatesSelector selector, Propagator propagator, EventDetector detector, SignSemantic signSemantic)	Simple constructor.

Uses of Propagator in org.orekit.gnss

Method parameters in org.orekit.gnss with type arguments of type Propagator

Modifier and Type	Method	Description
DOP	DOPComputer.compute(AbsoluteDate date, List<Propagator> gnss)	Compute the DOP at a given date for a set of GNSS spacecrafts.

Uses of Propagator in org.orekit.propagation

Subinterfaces of Propagator in org.orekit.propagation

Modifier and Type	Interface	Description
interface	BoundedPropagator	This interface is intended for ephemerides valid only during a time range.

Classes in org.orekit.propagation that implement Propagator

Modifier and Type	Class	Description
class	AbstractPropagator	Common handling of Propagator methods for analytical propagators.

Methods in org.orekit.propagation that return types with arguments of type Propagator

Modifier and Type	Method	Description
List<Propagator>	PropagatorsParallelizer.getPropagators()	Get an unmodifiable list of the underlying mono-satellite propagators.

Constructor parameters in org.orekit.propagation with type arguments of type Propagator

Constructor	Description
PropagatorsParallelizer(List<Propagator> propagators, MultiSatStepHandler globalHandler)	Simple constructor.

Uses of Propagator in org.orekit.propagation.analytical

Classes in org.orekit.propagation.analytical that implement Propagator

Modifier and Type	Class	Description
class	AbstractAnalyticalPropagator	Common handling of Propagator methods for analytical propagators.
class	AdapterPropagator	Orbit propagator that adapts an underlying propagator, adding differential effects.
class	AggregateBoundedPropagator	A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.
class	EcksteinHechlerPropagator	This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
class	Ephemeris	This class is designed to accept and handle tabulated orbital entries.
class	KeplerianPropagator	Simple Keplerian orbit propagator.

Methods in org.orekit.propagation.analytical that return Propagator

Modifier and Type	Method	Description
Propagator	AdapterPropagator.getPropagator()	Get the reference propagator.

Constructors in org.orekit.propagation.analytical with parameters of type Propagator

Constructor	Description
AdapterPropagator(Propagator reference)	Build a propagator from an underlying reference propagator.

Uses of Propagator in org.orekit.propagation.analytical.gnss

Classes in org.orekit.propagation.analytical.gnss that implement Propagator

Modifier and Type	Class	Description
class	GPSPropagator	This class aims at propagating a GPS orbit from GPSOrbitalElements.

Uses of Propagator in org.orekit.propagation.analytical.tle

Classes in org.orekit.propagation.analytical.tle that implement Propagator

Modifier and Type	Class	Description
class	DeepSDP4	This class contains the methods that compute deep space perturbation terms.
class	SGP4	This class contains methods to compute propagated coordinates with the SGP4 model.
class	TLEPropagator	This class provides elements to propagate TLE's.

Uses of Propagator in org.orekit.propagation.conversion

Methods in org.orekit.propagation.conversion that return Propagator

Modifier and Type	Method	Description
Propagator	EcksteinHechlerPropagatorBuilder.buildPropagator(double[] normalizedParameters)	Build a propagator.
Propagator	KeplerianPropagatorBuilder.buildPropagator(double[] normalizedParameters)	Build a propagator.
Propagator	PropagatorBuilder.buildPropagator(double[] normalizedParameters)	Build a propagator.
Propagator	TLEPropagatorBuilder.buildPropagator(double[] normalizedParameters)	Build a propagator.
Propagator	AbstractPropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, String... freeParameters)	Find the propagator that minimize the mean square error for a sample of states.
Propagator	AbstractPropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, List<String> freeParameters)	Find the propagator that minimize the mean square error for a sample of states.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters)	Convert a propagator to another.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters)	Convert a propagator to another.
Propagator	PropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, String... freeParameters)	Find the propagator that minimize the mean square error for a sample of states.
Propagator	PropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, List<String> freeParameters)	Find the propagator that minimize the mean square error for a sample of states.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters)	Convert a propagator into another one.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters)	Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.getAdaptedPropagator()	Get the adapted propagator.

Methods in org.orekit.propagation.conversion with parameters of type Propagator

Modifier and Type	Method	Description
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters)	Convert a propagator to another.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters)	Convert a propagator to another.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters)	Convert a propagator into another one.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters)	Convert a propagator into another one.

Constructors in org.orekit.propagation.conversion with parameters of type Propagator

Constructor	Description
OsculatingToMeanElementsConverter(SpacecraftState state, int satelliteRevolution, Propagator propagator, double positionScale)	Constructor.

Uses of Propagator in org.orekit.propagation.integration

Classes in org.orekit.propagation.integration that implement Propagator

Modifier and Type	Class	Description
class	AbstractIntegratedPropagator	Common handling of Propagator methods for both numerical and semi-analytical propagators.
class	IntegratedEphemeris	This class stores sequentially generated orbital parameters for later retrieval.

Uses of Propagator in org.orekit.propagation.numerical

Classes in org.orekit.propagation.numerical that implement Propagator

Modifier and Type	Class	Description
class	NumericalPropagator	This class propagates orbits using numerical integration.

Uses of Propagator in org.orekit.propagation.semianalytical.dsst

Classes in org.orekit.propagation.semianalytical.dsst that implement Propagator

Modifier and Type	Class	Description
class	DSSTPropagator	This class propagates orbits using the DSST theory.