Jeospace API

Uses of Class
org.jeospace.physics.orbit.OrbitalElements

Packages that use OrbitalElements
org.jeospace.navigation Contains classes that implement the navigation capabilities. 
org.jeospace.physics.orbit Contains interfaces and classes supporting physics based orbital mechanics. 
org.jeospace.simulation Contains classes to configure, manage and control the simulation/visulation environment. 
org.jeospace.x3d.geometry Contains classes used in the construction of x3d geometry. 
 

Uses of OrbitalElements in org.jeospace.navigation
 

Methods in org.jeospace.navigation with parameters of type OrbitalElements
 void OrbitInterpolator.set(OrbitalElements elements)
          Set the OrbitalElements of the satellite
 

Constructors in org.jeospace.navigation with parameters of type OrbitalElements
OrbitInterpolator(OrbitalElements elements)
          Construct an instance
 

Uses of OrbitalElements in org.jeospace.physics.orbit
 

Methods in org.jeospace.physics.orbit that return OrbitalElements
 OrbitalElements BaseSatellite.getOrbitalElements(double timeValue)
          Return the OrbitalElements of the satellite
 OrbitalElements Pluto.getOrbitalElements(double julianDay)
          Return the orbital elements for the world at the specified time
 OrbitalElements Moon.getOrbitalElements(double julianDay)
          Return the orbital elements for the world at the specified time
 OrbitalElements Sun.getOrbitalElements(double julianDay)
          Over-rides SolarWorld.
 OrbitalElements SolarWorld.getOrbitalElements(double julianDay)
          Return the orbital elements for the world at the specified time
 OrbitalElements BaseWorld.getOrbitalElements(double timeValue)
          Return the orbital elements for the world at the specified time
 OrbitalElements OrbitalBody.getOrbitalElements(double timeValue)
          Return the OrbitalElements of the object at the specified time
 

Methods in org.jeospace.physics.orbit with parameters of type OrbitalElements
static Satellite SatelliteFactory.create(Identification ident, ReferenceFrame refFrame, OrbitalElements elements)
          The factory method
 void EarthSatellite.setOrbitalElements(OrbitalElements elements)
          Set the OrbitalElements of the satellite
 void SxP4EllipticMotion.set(OrbitalElements oe)
          Set the value of the orbital elements and element dependant variables used in the calculation of the satellite's elliptic motion
 void BaseSatellite.setOrbitalElements(OrbitalElements elements)
          Set the OrbitalElements of the satellite
 void Satellite.setOrbitalElements(OrbitalElements elements)
          Set the OrbitalElements of the satellite
 void BaseWorld.setOrbitalElements(OrbitalElements elements)
          Set the orbital elements for the world
 void UnperturbedEllipticMotion.set(OrbitalElements oe)
          Set the value of the orbital elements to be used in the calculation of the orbital object in it's elliptic motion
 void EllipticMotion.set(OrbitalElements oe)
          Set the value of the orbital elements to be used in the calculation of the orbital object in it's elliptic motion
 

Constructors in org.jeospace.physics.orbit with parameters of type OrbitalElements
EarthSatellite(Identification ident, OrbitalElements elements)
          Construct an instance
SxP4EllipticMotion(OrbitalElements oe)
          Construct an instance
BaseSatellite(Identification ident, ReferenceFrame refFrame, OrbitalElements elements)
          Construct a Satellite instance
BaseWorld(Identification ident, ReferenceFrame refFrame, Ellipsoid ellipsoid, Mass mass, OrbitalElements elements)
          Construct a World instance
UnperturbedEllipticMotion(OrbitalElements oe)
          Construct an instance
 

Uses of OrbitalElements in org.jeospace.simulation
 

Methods in org.jeospace.simulation that return OrbitalElements
 OrbitalElements Unmarshal.getOrbitalElements(org.w3c.dom.Element oe_element, World parent_world)
          Return the OrbitalElements that coorespond to the argument
 

Methods in org.jeospace.simulation with parameters of type OrbitalElements
 org.w3c.dom.Element Marshal.createOrbitalElements(OrbitalElements orbitalElements)
          Create and return an orbital element Element
 org.w3c.dom.Element Marshal.createEllipticPathSystemComponent(java.lang.String name, ReferenceFrame refFrame, OrbitalElements oe, java.awt.Color color)
          Create and return an elliptic path component Element (a type of system component)
 

Uses of OrbitalElements in org.jeospace.x3d.geometry
 

Methods in org.jeospace.x3d.geometry with parameters of type OrbitalElements
static ILSDataSource EllipticPathFactory.create(OrbitalElements oe, World world, double julianDay)
          The factory method
 

Constructors in org.jeospace.x3d.geometry with parameters of type OrbitalElements
EllipticPath(OrbitalElements oe)
          Constructor
EarthEllipticPath(OrbitalElements oe, double julianDay)
          Constructor
 


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