Uses of Class
org.orekit.propagation.AbstractPropagator

Packages that use AbstractPropagator

Package	Description
org.orekit.control.heuristics.lambert	This package provides routines related to Lambert problems.
org.orekit.files.general	This package provides interfaces for orbit file representations and corresponding parsers.
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.intelsat	This package provides classes to propagate Intelsat's 11 elements.
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 AbstractPropagator in org.orekit.control.heuristics.lambert

Methods in org.orekit.control.heuristics.lambert with parameters of type AbstractPropagator

Modifier and Type	Method	Description
protected SpacecraftState	LambertDifferentialCorrector.buildInitialState(AbstractPropagator propagator, SpacecraftState templateState, Vector3D initialVelocity)	Method creating an initial state.
protected void	LambertDifferentialCorrector.init(AbstractPropagator propagator, Vector3D guessInitialVelocity)	Initialize propagator.
protected LambertBoundaryVelocities	LambertDifferentialCorrector.iterate(AbstractPropagator propagator)	Apply differential corrections until convergence (interrupted by maximum iterations count).
LambertBoundaryVelocities	LambertDifferentialCorrector.solve(AbstractPropagator propagator, Vector3D guessInitialVelocity)	Method applying differential correction on the guess (Newton-Raphson algorithm).

Uses of AbstractPropagator in org.orekit.files.general

Subclasses of AbstractPropagator in org.orekit.files.general

Modifier and Type	Class	Description
class	EphemerisSegmentPropagator<C extends TimeStampedPVCoordinates>	A Propagator based on a EphemerisFile.EphemerisSegment.

Uses of AbstractPropagator in org.orekit.propagation.analytical

Subclasses of AbstractPropagator in org.orekit.propagation.analytical

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	BrouwerLyddanePropagator	This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
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.

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

Subclasses of AbstractPropagator in org.orekit.propagation.analytical.gnss

Modifier and Type	Class	Description
class	GLONASSAnalyticalPropagator	This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.
class	GNSSPropagator	Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.
class	SBASPropagator	This class aims at propagating a SBAS orbit from SBASOrbitalElements.

Uses of AbstractPropagator in org.orekit.propagation.analytical.intelsat

Subclasses of AbstractPropagator in org.orekit.propagation.analytical.intelsat

Modifier and Type	Class	Description
class	IntelsatElevenElementsPropagator	This class provides elements to propagate Intelsat's 11 elements.

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

Subclasses of AbstractPropagator in org.orekit.propagation.analytical.tle

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 AbstractPropagator in org.orekit.propagation.conversion

Classes in org.orekit.propagation.conversion with type parameters of type AbstractPropagator

Modifier and Type	Class	Description
class	AbstractPropagatorBuilder<T extends AbstractPropagator>	Base class for propagator builders.

Uses of AbstractPropagator in org.orekit.propagation.integration

Subclasses of AbstractPropagator in org.orekit.propagation.integration

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 AbstractPropagator in org.orekit.propagation.numerical

Subclasses of AbstractPropagator in org.orekit.propagation.numerical

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

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

Subclasses of AbstractPropagator in org.orekit.propagation.semianalytical.dsst

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