Package gaiasky.scenegraph.component

Class OrbitComponent

java.lang.Object
gaiasky.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)  
    java.lang.String toString()  

    Methods inherited from class java.lang.Object

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

  • Field Details

    • 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 Details

    • OrbitComponent

      public OrbitComponent()

  • Method Details

    • 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)

    • toString

      public java.lang.String toString()
      Overrides:
      toString in class java.lang.Object