public interface SpacecraftStateProvider extends PVCoordinatesProvider
| Modifier and Type | Method and Description |
|---|---|
default PVCoordinates |
getPVCoordinates(AbsoluteDate date,
Frame frame)
Default implementation for PVCoordinatesProvider feature using the
SpacecraftState
object's orbit. |
SpacecraftState |
getSpacecraftState(AbsoluteDate date)
Get the
SpacecraftState at provided date. |
getNativeFrameSpacecraftState getSpacecraftState(AbsoluteDate date) throws PropagationException
SpacecraftState at provided date.date - target datePropagationException - if state cannot be computeddefault PVCoordinates getPVCoordinates(AbsoluteDate date, Frame frame) throws PatriusException
SpacecraftState
object's orbit.
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates in interface PVCoordinatesProviderdate - current dateframe - the frame where to define the positionPatriusException - if position cannot be computed in given frameCopyright © 2024 CNES. All rights reserved.