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| Packages that use Propagator | |
|---|---|
| fr.cnes.sirius.patrius.events.sensor | |
| fr.cnes.sirius.patrius.propagation | |
| fr.cnes.sirius.patrius.propagation.precomputed.multi | |
| fr.cnes.sirius.patrius.stela.propagation | |
| org.orekit.attitudes | This package provides classes to represent simple attitudes. |
| org.orekit.frames | This package provides classes to handle frames and transforms between them. |
| org.orekit.propagation | This package provides tools to propagate orbital states with different methods. |
| org.orekit.propagation.analytical | |
| org.orekit.propagation.analytical.tle | This package provides classes to read and extrapolate tle's. |
| org.orekit.propagation.analytical.twod | |
| org.orekit.propagation.numerical | |
| org.orekit.propagation.precomputed | |
| org.orekit.propagation.sampling | This package provides interfaces and classes dealing with step handling during propagation. |
| Uses of Propagator in fr.cnes.sirius.patrius.events.sensor |
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| Constructors in fr.cnes.sirius.patrius.events.sensor with parameters of type Propagator | |
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SatToSatMutualVisibilityDetector(SensorModel mainSensorModel,
SensorModel secondarySensorModel,
Propagator secondSpacecraftPropagator,
boolean withMasking,
double maxCheck,
double threshold)
Constructor to be used for single spacecraft propagation only ( Propagator). |
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SatToSatMutualVisibilityDetector(SensorModel mainSensorModel,
SensorModel secondarySensorModel,
Propagator secondSpacecraftPropagator,
boolean withMasking,
double maxCheck,
double threshold,
EventDetector.Action entry,
EventDetector.Action exit)
Constructor to be used for single spacecraft propagation only ( Propagator). |
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SatToSatMutualVisibilityDetector(SensorModel mainSensorModel,
SensorModel secondarySensorModel,
Propagator secondSpacecraftPropagator,
boolean withMasking,
double maxCheck,
double threshold,
EventDetector.Action entry,
EventDetector.Action exit,
boolean removeEntry,
boolean removeExit)
Constructor to be used for single spacecraft propagation only ( Propagator). |
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SecondarySpacecraft(Assembly assembly,
Propagator propagator,
String name)
Constructor for a secondary spacecraft to be used in events detections. |
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| Uses of Propagator in fr.cnes.sirius.patrius.propagation |
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| Classes in fr.cnes.sirius.patrius.propagation that implement Propagator | |
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class |
PVCoordinatePropagator
This class is an analytical propagator which propagates states from the input PV, Attitude, and additional state provider. |
| Uses of Propagator in fr.cnes.sirius.patrius.propagation.precomputed.multi |
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| Classes in fr.cnes.sirius.patrius.propagation.precomputed.multi that implement Propagator | |
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class |
MultiIntegratedEphemeris
This interface is copied from IntegratedEphemeris and adapted to multi propagation. |
| Uses of Propagator in fr.cnes.sirius.patrius.stela.propagation |
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| Classes in fr.cnes.sirius.patrius.stela.propagation that implement Propagator | |
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class |
StelaAbstractPropagator
Common handling of Propagator methods for analytical propagators. |
class |
StelaGTOPropagator
STELA propagator for Geostationnary Transfert Orbits (GTO). |
| Uses of Propagator in org.orekit.attitudes |
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| Methods in org.orekit.attitudes with parameters of type Propagator | |
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void |
AttitudesSequence.registerSwitchEvents(Propagator propagator)
Register all wrapped switch events to the propagator. |
| Uses of Propagator in org.orekit.frames |
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| Methods in org.orekit.frames that return Propagator | |
|---|---|
Propagator |
SpacecraftFrame.getPropagator()
Deprecated. Get the underlying propagator. |
| Constructors in org.orekit.frames with parameters of type Propagator | |
|---|---|
SpacecraftFrame(Propagator propagator,
String name)
Deprecated. Simple constructor. |
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| Uses of Propagator in org.orekit.propagation |
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| Subinterfaces of Propagator in org.orekit.propagation | |
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interface |
BoundedPropagator
This interface is intended for ephemerides valid only during a time range. |
| Classes in org.orekit.propagation that implement Propagator | |
|---|---|
class |
AbstractPropagator
Common handling of Propagator methods for analytical propagators. |
class |
AnalyticalIntegratedEphemeris
This class stores sequentially generated orbital parameters for later retrieval. |
| Constructors in org.orekit.propagation with parameters of type Propagator | |
|---|---|
OsculatingToMeanElementsConverter(SpacecraftState state,
int satelliteRevolution,
Propagator propagator)
Constructor. |
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| Uses of Propagator in org.orekit.propagation.analytical |
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| Classes in org.orekit.propagation.analytical that implement Propagator | |
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class |
AbstractLyddanePropagator
Abstract Lyddane propagator. |
class |
AdapterPropagator
Orbit propagator that adapts an underlying propagator, adding differential effects. |
class |
EcksteinHechlerPropagator
This class propagates a SpacecraftState
using the analytical Eckstein-Hechler model. |
class |
J2SecularPropagator
J2 secular propagator. |
class |
KeplerianPropagator
Simple keplerian orbit propagator. |
class |
LyddaneLongPeriodPropagator
Lyddane long period propagator. |
class |
LyddaneSecularPropagator
Lyddane secular propagator. |
| Methods in org.orekit.propagation.analytical that return Propagator | |
|---|---|
Propagator |
AdapterPropagator.getPropagator()
Get the reference propagator. |
| Constructors in org.orekit.propagation.analytical with parameters of type Propagator | |
|---|---|
AdapterPropagator(Propagator reference)
Build a propagator from an underlying reference propagator. |
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| Uses of Propagator in org.orekit.propagation.analytical.tle |
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| Classes in org.orekit.propagation.analytical.tle that implement Propagator | |
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class |
TLEPropagator
This class provides elements to propagate TLE's. |
| Uses of Propagator in org.orekit.propagation.analytical.twod |
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| Classes in org.orekit.propagation.analytical.twod that implement Propagator | |
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class |
Analytical2DPropagator
This class propagates an analytical 2D orbit model and extends the AbstractPropagator class. |
| Uses of Propagator in org.orekit.propagation.numerical |
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| Classes in org.orekit.propagation.numerical that implement Propagator | |
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class |
NumericalPropagator
This class propagates SpacecraftState using numerical integration. |
| Uses of Propagator in org.orekit.propagation.precomputed |
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| Classes in org.orekit.propagation.precomputed that implement Propagator | |
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class |
AbstractEphemeris
This class handles tabulated spacecraft states entries (either from a pv coordinates provider and an attitude provider or a spacecraft states array). |
class |
Ephemeris
This class is designed to accept and handle tabulated orbital entries. |
class |
HermiteEphemeris
Deprecated. |
class |
IntegratedEphemeris
This class stores sequentially generated orbital parameters for later retrieval. |
class |
LagrangeEphemeris
Deprecated. |
| Uses of Propagator in org.orekit.propagation.sampling |
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| Constructors in org.orekit.propagation.sampling with parameters of type Propagator | |
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BasicStepInterpolator(Propagator propagator)
Build a new instance from a basic propagator. |
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