Package | Description |
---|---|
org.orekit.attitudes |
This package provides classes to represent simple attitudes.
|
org.orekit.propagation |
Propagation
|
org.orekit.propagation.analytical |
Top level package for analytical propagators.
|
org.orekit.propagation.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
|
org.orekit.propagation.numerical |
Top level package for numerical propagators.
|
Modifier and Type | Method | Description |
---|---|---|
<T extends RealFieldElement<T>> |
AttitudesSequence.registerSwitchEvents(Field<T> field,
FieldPropagator<T> propagator) |
Register all wrapped switch events to the propagator.
|
Modifier and Type | Interface | Description |
---|---|---|
interface |
FieldBoundedPropagator<T extends RealFieldElement<T>> |
This interface is intended for ephemerides valid only during a time range.
|
Modifier and Type | Class | Description |
---|---|---|
class |
FieldAbstractPropagator<T extends RealFieldElement<T>> |
Common handling of
Propagator methods for analytical propagators. |
Modifier and Type | Class | Description |
---|---|---|
class |
FieldAbstractAnalyticalPropagator<T extends RealFieldElement<T>> |
Common handling of
FieldPropagator methods for analytical propagators. |
class |
FieldEcksteinHechlerPropagator<T extends RealFieldElement<T>> |
This class propagates a
FieldSpacecraftState
using the analytical Eckstein-Hechler model. |
class |
FieldKeplerianPropagator<T extends RealFieldElement<T>> |
Simple Keplerian orbit propagator.
|
Modifier and Type | Class | Description |
---|---|---|
class |
FieldAbstractIntegratedPropagator<T extends RealFieldElement<T>> |
Common handling of
FieldPropagator
methods for both numerical and semi-analytical propagators. |
class |
FieldIntegratedEphemeris<T extends RealFieldElement<T>> |
This class stores sequentially generated orbital parameters for
later retrieval.
|
Modifier and Type | Class | Description |
---|---|---|
class |
FieldNumericalPropagator<T extends RealFieldElement<T>> |
This class propagates
orbits using
numerical integration. |
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