Package org.jeospace.physics.orbit

Contains interfaces and classes supporting physics based orbital mechanics.

See:
Description

Interface Summary

CelestialBody	Defines the base requirements for identifying and positioning a celestial body.
EllipticMotion	Defines the requirements for classes that will be calculating the elliptic motion of orbital objects from their orbital elements.
GeocentricWorld	Describes the requirements specific to transforming the positions of worlds in the Solar System from heliocentric ecliptic to geocentric ecliptic form.
OrbitalBody	Defines the base requirements for identifying an orbital body and describing it's geometric relationship to an orbital system.
Satellite	Defines the requirements for positioning satellites.
SDP4Constants	Defines constants specific to the SDP4 algorithm utilized by SxP4EllipticMotion.
SxP4Constants	Defines constants utilized by SxP4EllipticMotion.
World	Defines the requirements necessary to describe a world's physical characteristics and motions as they relate to being a part of an orbital system.

Class Summary

AnomalyType	Constant object identifiers of the type of orbital anomaly.
BaseSatellite	A concrete implementation of Satellite for identifying and tracking satellites in 'unperturbed' orbits about their parent worlds.
BaseWorld	A concrete implementation of World intended to be initialized parametrically.
Earth	Earth, third planet from the Sun.
EarthSatellite	A concrete implementation of Satellite specific to identifying and tracking Earth orbiting satellites.
Epoch	An immutable object, an epoch is a representation of an instant in time that is used as a point of reference - typically in astronomical calculations.
Jupiter	Jupiter, the fifth planet from the Sun.
LunarPhase	An abstract class containing utility functions for calculating the lunar phase and times of the Moon's arrival at the New Moon, First Quarter, Full Moon, and Last Quarter phases.
LunarPhaseID	Constant object identifiers of lunar phases.
Mars	Mars, the fourth planet from the Sun.
Mercury	Mercury, the first planet from the Sun.
Moon	The Moon, primary satellite of the Earth.
Neptune	Neptune, the eighth planet from the Sun.
OrbitalElements	An immutable object containing a set of measure objects that together represent orbital elements.
OrbitalElementsType	Constant object identifiers of the type of orbital elements.
Pluto	Pluto, the ninth planet from the Sun.
RotationalAxis	Utility class to obtain the rotational axis orientation of a world.
SatelliteFactory	Factory for creating Satellites
Saturn	Saturn, the sixth planet from the Sun.
SolarNode	An abstract class containing utility functions for calculating the times of Earth's passages through the nodes.
SolarNodeID	Constant object identifiers of the solar nodes.
SolarWorld	The base implementation for the major planets of the Solar System.
Sun	The Sun, the primary SolarWorld.
SxP4EllipticMotion	Implements the SGP4/SDP4 models for elliptic motion of satellites in Earth orbit.
UnperturbedEllipticMotion	A solution to the equation of Kepler for calculating the elliptic motion of an object in orbit.
Uranus	Uranus, the seventh planet from the Sun.
Venus	Venus, the second planet from the Sun.
Visibility	Constant object identifiers of the visibility status of an orbital object

Package org.jeospace.physics.orbit Description

Contains interfaces and classes supporting physics based orbital mechanics.