Modifier and Type | Class and Description |
---|---|
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.
|
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 | 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 |
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.
|
Copyright © 2020 CNES. All rights reserved.