org.orekit.data

Class BodiesElements

java.lang.Object

org.orekit.data.DelaunayArguments

org.orekit.data.BodiesElements

All Implemented Interfaces:

Serializable, TimeStamped

public final class BodiesElements
extends DelaunayArguments
implements Serializable

Elements of the bodies having an effect on nutation.

This class is a simple placeholder, it does not provide any processing method.

Author:

Luc Maisonobe

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
BodiesElements(AbsoluteDate date, double tc, double gamma, double l, double lPrime, double f, double d, double omega, double lMe, double lVe, double lE, double lMa, double lJu, double lSa, double lUr, double lNe, double pa) Simple constructor.

Method Summary

Methods

Modifier and Type	Method and Description
double	getLE() Get the mean Earth longitude.
double	getLJu() Get the mean Jupiter longitude.
double	getLMa() Get the mean Mars longitude.
double	getLMe() Get the mean Mercury longitude.
double	getLNe() Get the mean Neptune longitude.
double	getLSa() Get the mean Saturn longitude.
double	getLUr() Get the mean Uranus longitude.
double	getLVe() Get the mean Venus longitude.
double	getPa() Get the general accumulated precession in longitude.

Methods inherited from class org.orekit.data.DelaunayArguments

getD, getDate, getF, getGamma, getL, getLPrime, getOmega, getTC

Methods inherited from class java.lang.Object

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

Constructor Detail

BodiesElements

public BodiesElements(AbsoluteDate date,
              double tc,
              double gamma,
              double l,
              double lPrime,
              double f,
              double d,
              double omega,
              double lMe,
              double lVe,
              double lE,
              double lMa,
              double lJu,
              double lSa,
              double lUr,
              double lNe,
              double pa)

Simple constructor.

Parameters:

date - current date

tc - offset in Julian centuries

gamma - tide parameter γ = GMST + π

l - mean anomaly of the Moon

lPrime - mean anomaly of the Sun

f - L - Ω where L is the mean longitude of the Moon

d - mean elongation of the Moon from the Sun

omega - mean longitude of the ascending node of the Moon

lMe - mean Mercury longitude

lVe - mean Venus longitude

lE - mean Earth longitude

lMa - mean Mars longitude

lJu - mean Jupiter longitude

lSa - mean Saturn longitude

lUr - mean Uranus longitude

lNe - mean Neptune longitude

pa - general accumulated precession in longitude

Method Detail

getLMe

public double getLMe()

Get the mean Mercury longitude.

Returns:

mean Mercury longitude.

getLVe

public double getLVe()

Get the mean Venus longitude.

Returns:

mean Venus longitude.

getLE

public double getLE()

Get the mean Earth longitude.

Returns:

mean Earth longitude.

getLMa

public double getLMa()

Get the mean Mars longitude.

Returns:

mean Mars longitude.

getLJu

public double getLJu()

Get the mean Jupiter longitude.

Returns:

mean Jupiter longitude.

getLSa

public double getLSa()

Get the mean Saturn longitude.

Returns:

mean Saturn longitude.

getLUr

public double getLUr()

Get the mean Uranus longitude.

Returns:

mean Uranus longitude.

getLNe

public double getLNe()

Get the mean Neptune longitude.

Returns:

mean Neptune longitude.

getPa

public double getPa()

Get the general accumulated precession in longitude.

Returns:

general accumulated precession in longitude.