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Jeospace API | ||||||||||
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| 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 |
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| 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 |
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SxP4EllipticMotion(OrbitalElements oe)
Construct an instance |
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BaseSatellite(Identification ident,
ReferenceFrame refFrame,
OrbitalElements elements)
Construct a Satellite instance |
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BaseWorld(Identification ident,
ReferenceFrame refFrame,
Ellipsoid ellipsoid,
Mass mass,
OrbitalElements elements)
Construct a World instance |
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UnperturbedEllipticMotion(OrbitalElements oe)
Construct an instance |
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| 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 |
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EarthEllipticPath(OrbitalElements oe,
double julianDay)
Constructor |
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