Uses of Interface
org.orekit.orbits.orbitalparameters.IOrbitalParameters

Packages that use IOrbitalParameters
fr.cnes.sirius.patrius.stela.orbits   
org.orekit.orbits This package provides classes to represent orbits. 
org.orekit.orbits.orbitalparameters   
 

Uses of IOrbitalParameters in fr.cnes.sirius.patrius.stela.orbits
 

Methods in fr.cnes.sirius.patrius.stela.orbits that return IOrbitalParameters
 IOrbitalParameters StelaEquinoctialOrbit.getParameters()
          Get underlying orbital parameters.
 

Constructors in fr.cnes.sirius.patrius.stela.orbits with parameters of type IOrbitalParameters
StelaEquinoctialOrbit(IOrbitalParameters params, Frame frame, AbsoluteDate date)
          Creates a new instance.
 

Uses of IOrbitalParameters in org.orekit.orbits
 

Methods in org.orekit.orbits that return IOrbitalParameters
 IOrbitalParameters CircularOrbit.getParameters()
          Get underlying orbital parameters.
 IOrbitalParameters KeplerianOrbit.getParameters()
          Get underlying orbital parameters.
abstract  IOrbitalParameters Orbit.getParameters()
          Get underlying orbital parameters.
 IOrbitalParameters EquatorialOrbit.getParameters()
          Get underlying orbital parameters.
 IOrbitalParameters EquinoctialOrbit.getParameters()
          Get underlying orbital parameters.
 IOrbitalParameters ApsisOrbit.getParameters()
          Get underlying orbital parameters.
 IOrbitalParameters CartesianOrbit.getParameters()
          Get underlying orbital parameters.
 

Constructors in org.orekit.orbits with parameters of type IOrbitalParameters
ApsisOrbit(IOrbitalParameters parameters, Frame frame, AbsoluteDate date)
          Creates a new instance.
CartesianOrbit(IOrbitalParameters parameters, Frame frame, AbsoluteDate date)
          Creates a new instance.
CircularOrbit(IOrbitalParameters parameters, Frame frame, AbsoluteDate date)
          Creates a new instance.
EquatorialOrbit(IOrbitalParameters parameters, Frame frame, AbsoluteDate date)
          Creates a new instance.
EquinoctialOrbit(IOrbitalParameters parameters, Frame frame, AbsoluteDate date)
          Creates a new instance.
KeplerianOrbit(IOrbitalParameters parameters, Frame frame, AbsoluteDate date)
          Creates a new instance.
 

Uses of IOrbitalParameters in org.orekit.orbits.orbitalparameters
 

Classes in org.orekit.orbits.orbitalparameters that implement IOrbitalParameters
 class AbstractOrbitalParameters
          Abstract class for orbital parameters.
 class ApsisAltitudeParameters
          This class handles periapsis altitude/apoapsis altitude parameters.
 class ApsisRadiusParameters
          This class handles periapsis/apoapsis parameters.
 class CartesianParameters
          This class holds cartesian orbital parameters.
 class CircularParameters
          This class handles circular orbital parameters.
 class EquatorialParameters
          This class handles non circular equatorial orbital parameters.
 class EquinoctialParameters
          This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
 class KeplerianParameters
          This class handles traditional keplerian orbital parameters.
 class ReentryParameters
          This class handles reentry parameters.
 class StelaEquinoctialParameters
          This class handles the equinoctial orbital parameters used in Stela; it has been created because the equinoctial parameters associated to Stela differ from the EquinoctialParameters parameters.
 



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