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).
|
Modifier and Type | Method | Description |
---|---|---|
void |
AttitudesSequence.registerSwitchEvents(Propagator propagator) |
Register all wrapped switch events to the propagator.
|
Modifier and Type | Method | Description |
---|---|---|
Propagator |
Generator.getPropagator(ObservableSatellite satellite) |
Get a registered propagator.
|
Modifier and Type | Method | Description |
---|---|---|
ObservableSatellite |
Generator.addPropagator(Propagator propagator) |
Add a propagator.
|
Constructor | Description |
---|---|
EventBasedScheduler(MeasurementBuilder<T> builder,
DatesSelector selector,
Propagator propagator,
EventDetector detector,
SignSemantic signSemantic) |
Simple constructor.
|
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. |
Modifier and Type | Interface | Description |
---|---|---|
interface |
BoundedPropagator |
This interface is intended for ephemerides valid only during a time range.
|
Modifier and Type | Class | Description |
---|---|---|
class |
AbstractPropagator |
Common handling of
Propagator methods for analytical propagators. |
Modifier and Type | Method | Description |
---|---|---|
List<Propagator> |
PropagatorsParallelizer.getPropagators() |
Get an unmodifiable list of the underlying mono-satellite propagators.
|
Constructor | Description |
---|---|
PropagatorsParallelizer(List<Propagator> propagators,
MultiSatStepHandler globalHandler) |
Simple constructor.
|
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.
|
Modifier and Type | Method | Description |
---|---|---|
Propagator |
AdapterPropagator.getPropagator() |
Get the reference propagator.
|
Constructor | Description |
---|---|
AdapterPropagator(Propagator reference) |
Build a propagator from an underlying reference propagator.
|
Modifier and Type | Class | Description |
---|---|---|
class |
GPSPropagator |
This class aims at propagating a GPS orbit from
GPSOrbitalElements . |
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.
|
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.
|
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.
|
Constructor | Description |
---|---|
OsculatingToMeanElementsConverter(SpacecraftState state,
int satelliteRevolution,
Propagator propagator,
double positionScale) |
Constructor.
|
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.
|
Modifier and Type | Class | Description |
---|---|---|
class |
NumericalPropagator |
This class propagates
orbits using
numerical integration. |
Modifier and Type | Class | Description |
---|---|---|
class |
DSSTPropagator |
This class propagates
orbits using the DSST theory. |
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