Package | Description |
---|---|
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.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
|
Modifier and Type | Class and Description |
---|---|
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.
|
Constructor and Description |
---|
AbstractAnalyticalGradientConverter(AbstractAnalyticalPropagator propagator,
double mu,
int freeStateParameters)
Constructor.
|
AbstractAnalyticalMatricesHarvester(AbstractAnalyticalPropagator propagator,
String stmName,
RealMatrix initialStm,
DoubleArrayDictionary initialJacobianColumns)
Simple constructor.
|
Modifier and Type | Class and 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 . |
Modifier and Type | Class and 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.
|
Modifier and Type | Class and Description |
---|---|
class |
IntegratedEphemeris
This class stores sequentially generated orbital parameters for
later retrieval.
|
Copyright © 2002-2023 CS GROUP. All rights reserved.