PVCoordinatesProvider (ORbit Extrapolation KIT 9.3 API)

All Known Subinterfaces:

BoundedPropagator, CelestialBody, ExtendedPVCoordinatesProvider, Propagator

All Known Implementing Classes:

AbstractAnalyticalPropagator, AbstractIntegratedPropagator, AbstractPropagator, AdapterPropagator, AggregateBoundedPropagator, CartesianOrbit, CircularOrbit, DeepSDP4, DSSTPropagator, EcksteinHechlerPropagator, Ephemeris, EquinoctialOrbit, GPSPropagator, IntegratedEphemeris, KeplerianOrbit, KeplerianPropagator, NumericalPropagator, Orbit, SGP4, TLEPropagator, TopocentricFrame
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public interface PVCoordinatesProvider
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Interface for PV coordinates providers.

Author:

Veronique Pommier
The PV coordinates provider interface can be used by any class used for position/velocity computation, for example celestial bodies or spacecraft position/velocity propagators, and many others...

Method Summary

All Methods Instance Methods Abstract Methods
Modifier and Type	Method	Description
`TimeStampedPVCoordinates`	`getPVCoordinates(AbsoluteDate date, Frame frame)`	Get the `PVCoordinates` of the body in the selected frame.

- Method Detail
  - getPVCoordinates
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TimeStampedPVCoordinates getPVCoordinates(AbsoluteDate date,
                                          Frame frame)
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    Get the PVCoordinates of the body in the selected frame.
    
    Parameters:
    
    date - current date
    
    frame - the frame where to define the position
    
    Returns:
    
    time-stamped position/velocity of the body (m and m/s)