Package gaia.cu9.ari.gaiaorbit.scenegraph.component

Class OrbitComponent

java.lang.Object

gaia.cu9.ari.gaiaorbit.scenegraph.component.OrbitComponent

public class OrbitComponent
extends java.lang.Object

Field Summary

Fields

Modifier and Type	Field	Description
double	argofpericenter	Argument of perihelion in degrees.
double	ascendingnode	Longitude of the ascending node in degrees.
double	e	Eccentricity of the ellipse.
double	epoch	Base epoch
double	i	Inclination, angle between the reference plane (ecliptic) and the orbital plane.
double	meananomaly	Mean anomaly at epoch, in degrees.
double	mu	G*M of central body (gravitational constant).
double	period	Orbital period in days
double	semimajoraxis	Semi major axis of the ellipse, a in Km.
java.lang.String	source	Source file

Constructor Summary

Constructors

Constructor	Description
OrbitComponent()

Method Summary

Modifier and Type	Method	Description
void	loadDataPoint(Vector3d out, java.time.Instant t)
void	setArgofpericenter(java.lang.Double argofpericenter)
void	setAscendingnode(java.lang.Double ascendingnode)
void	setEccentricity(java.lang.Double e)
void	setEpoch(java.lang.Double epoch)
void	setInclination(java.lang.Double i)
void	setMeananomaly(java.lang.Double meanAnomaly)
void	setMu(java.lang.Double mu)
void	setPeriod(java.lang.Double period)
void	setSemimajoraxis(java.lang.Double semimajoraxis)
void	setSource(java.lang.String source)

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Field Detail

source

public java.lang.String source

Source file

period

public double period

Orbital period in days

epoch

public double epoch

Base epoch

semimajoraxis

public double semimajoraxis

Semi major axis of the ellipse, a in Km.

e

public double e

Eccentricity of the ellipse.

i

public double i

Inclination, angle between the reference plane (ecliptic) and the orbital plane.

ascendingnode

public double ascendingnode

Longitude of the ascending node in degrees.

argofpericenter

public double argofpericenter

Argument of perihelion in degrees.

meananomaly

public double meananomaly

Mean anomaly at epoch, in degrees.

mu

public double mu

G*M of central body (gravitational constant). Defaults to the Sun's

Constructor Detail

OrbitComponent

public OrbitComponent()

Method Detail

setSource

public void setSource(java.lang.String source)

setPeriod

public void setPeriod(java.lang.Double period)

setEpoch

public void setEpoch(java.lang.Double epoch)

setSemimajoraxis

public void setSemimajoraxis(java.lang.Double semimajoraxis)

setEccentricity

public void setEccentricity(java.lang.Double e)

setInclination

public void setInclination(java.lang.Double i)

setAscendingnode

public void setAscendingnode(java.lang.Double ascendingnode)

setArgofpericenter

public void setArgofpericenter(java.lang.Double argofpericenter)

setMeananomaly

public void setMeananomaly(java.lang.Double meanAnomaly)

setMu

public void setMu(java.lang.Double mu)

loadDataPoint

public void loadDataPoint(Vector3d out,
                          java.time.Instant t)