Modifier and Type | Method and Description |
---|---|
void |
AttitudesSequence.registerSwitchEvents(Propagator propagator)
Register all wrapped switch events to the propagator.
|
Constructor and Description |
---|
SatToSatMutualVisibilityDetector(SensorModel mainSensorModel,
SensorModel secondarySensorModel,
Propagator secondSpacecraftPropagator,
boolean withMasking,
double maxCheck,
double threshold)
Constructor to be used for single spacecraft propagation only (
Propagator ). |
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 ). |
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 ). |
SecondarySpacecraft(Assembly assembly,
Propagator propagator,
String name)
Constructor for a secondary spacecraft to be used in events detections.
|
Modifier and Type | Interface and Description |
---|---|
interface |
BoundedPropagator
This interface is intended for ephemerides valid only during a time range.
|
Modifier and Type | Class and Description |
---|---|
class |
AbstractPropagator
Common handling of
Propagator methods for analytical propagators. |
class |
AnalyticalIntegratedEphemeris
This class stores sequentially generated orbital parameters for
later retrieval.
|
class |
PVCoordinatesPropagator
This class is an analytical propagator which propagates states from the input PV, Attitude, and additional state
provider.
|
Constructor and Description |
---|
AnalyticalIntegratedEphemeris(List<AbsoluteDate> initialDatesIn,
List<AbsoluteDate> finalDatesIn,
List<SpacecraftState> initialStatesIn,
Propagator propagatorIn,
AttitudeProvider attForcesProvider,
AttitudeProvider attEventsProvider,
boolean isForwardIn)
Constructor.
|
Modifier and Type | Class and Description |
---|---|
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.
|
Modifier and Type | Method and Description |
---|---|
Propagator |
AdapterPropagator.getPropagator()
Get the reference propagator.
|
Constructor and Description |
---|
AdapterPropagator(Propagator referenceIn)
Build a propagator from an underlying reference propagator.
|
AnalyticalEphemerisModeHandler(Propagator propagatorIn,
AttitudeProvider attForcesProvider,
AttitudeProvider attEventsProvider)
Constructor.
|
Modifier and Type | Class and Description |
---|---|
class |
TLEPropagator
This class provides elements to propagate TLE's.
|
Modifier and Type | Class and Description |
---|---|
class |
Analytical2DPropagator
This class propagates an analytical 2D orbit model and extends the
AbstractPropagator class. |
Modifier and Type | Class and Description |
---|---|
class |
NumericalPropagator
This class propagates
SpacecraftState using numerical integration. |
Modifier and Type | Class and Description |
---|---|
class |
Ephemeris
This class is designed to accept and handle tabulated orbital entries.
|
class |
IntegratedEphemeris
This class stores sequentially generated orbital parameters for
later retrieval.
|
Modifier and Type | Class and Description |
---|---|
class |
MultiIntegratedEphemeris
This interface is copied from IntegratedEphemeris and adapted to multi propagation.
|
Constructor and Description |
---|
BasicStepInterpolator(Propagator propagatorIn)
Build a new instance from a basic propagator.
|
Modifier and Type | Class and Description |
---|---|
class |
StelaAbstractPropagator
Common handling of
Propagator methods for analytical propagators. |
class |
StelaGTOPropagator
STELA propagator for Geostationnary Transfert Orbits (GTO).
|
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