DelaunayArguments (ORbit Extrapolation KIT 9.0.1 API)

java.lang.Object
- org.orekit.data.DelaunayArguments

All Implemented Interfaces:

Serializable, TimeStamped

Direct Known Subclasses:

BodiesElements
```
public class DelaunayArguments
extends Object
implements TimeStamped, Serializable
```
Delaunay arguments used for nutation or tides.
This class is a simple placeholder, it does not provide any processing method.

Since:

6.1

Author:

Luc Maisonobe

See Also:

Serialized Form

Constructor Summary

Constructors
Constructor and Description
`DelaunayArguments(AbsoluteDate date, double tc, double gamma, double gammaDot, double l, double lDot, double lPrime, double lPrimeDot, double f, double fDot, double d, double dDot, double omega, double omegaDot)` Simple constructor.

Method Summary

All Methods Instance Methods Concrete Methods
Modifier and Type	Method and Description
`double`	`getD()` Get the mean elongation of the Moon from the Sun.
`AbsoluteDate`	`getDate()` Get the date.
`double`	`getDDot()` Get the mean elongation of the Moon from the Sun time derivative.
`double`	`getF()` Get L - Ω where L is the mean longitude of the Moon.
`double`	`getFDot()` Get L - Ω where L is the mean longitude of the Moon time derivative.
`double`	`getGamma()` Get the tide parameter γ = GMST + π.
`double`	`getGammaDot()` Get the tide parameter γ = GMST + π time derivative.
`double`	`getL()` Get the mean anomaly of the Moon.
`double`	`getLDot()` Get the mean anomaly of the Moon time derivative.
`double`	`getLPrime()` Get the mean anomaly of the Sun.
`double`	`getLPrimeDot()` Get the mean anomaly of the Sun time derivative.
`double`	`getOmega()` Get the mean longitude of the ascending node of the Moon.
`double`	`getOmegaDot()` Get the mean longitude of the ascending node of the Moon time derivative.
`double`	`getTC()` Get the offset in Julian centuries.

Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

- Constructor Detail
  - DelaunayArguments
```
public DelaunayArguments(AbsoluteDate date,
                         double tc,
                         double gamma,
                         double gammaDot,
                         double l,
                         double lDot,
                         double lPrime,
                         double lPrimeDot,
                         double f,
                         double fDot,
                         double d,
                         double dDot,
                         double omega,
                         double omegaDot)
```
    Simple constructor.
    
    Parameters:
    
    date - current date
    
    tc - offset in Julian centuries
    
    gamma - tide parameter γ = GMST + π
    
    gammaDot - tide parameter γ = GMST + π time derivative
    
    l - mean anomaly of the Moon
    
    lDot - mean anomaly of the Moon time derivative
    
    lPrime - mean anomaly of the Sun
    
    lPrimeDot - mean anomaly of the Sun time derivative
    
    f - L - Ω where L is the mean longitude of the Moon
    
    fDot - L - Ω where L is the mean longitude of the Moon time derivative
    
    d - mean elongation of the Moon from the Sun
    
    dDot - mean elongation of the Moon from the Sun time derivative
    
    omega - mean longitude of the ascending node of the Moon
    
    omegaDot - mean longitude of the ascending node of the Moon time derivative
- Method Detail
  - getDate
```
public AbsoluteDate getDate()
```
    Get the date.
    
    Specified by:
    
    getDate in interface TimeStamped
    
    Returns:
    
    date attached to the object
  - getTC
```
public double getTC()
```
    Get the offset in Julian centuries.
    
    Returns:
    
    offset in Julian centuries
  - getGamma
```
public double getGamma()
```
    Get the tide parameter γ = GMST + π.
    
    Returns:
    
    tide parameter γ = GMST + π
  - getGammaDot
```
public double getGammaDot()
```
    Get the tide parameter γ = GMST + π time derivative.
    
    Returns:
    
    tide parameter γ = GMST + π time derivative
  - getL
```
public double getL()
```
    Get the mean anomaly of the Moon.
    
    Returns:
    
    mean anomaly of the Moon
  - getLDot
```
public double getLDot()
```
    Get the mean anomaly of the Moon time derivative.
    
    Returns:
    
    mean anomaly of the Moon time derivative
  - getLPrime
```
public double getLPrime()
```
    Get the mean anomaly of the Sun.
    
    Returns:
    
    mean anomaly of the Sun.
  - getLPrimeDot
```
public double getLPrimeDot()
```
    Get the mean anomaly of the Sun time derivative.
    
    Returns:
    
    mean anomaly of the Sun time derivative.
  - getF
```
public double getF()
```
    Get L - Ω where L is the mean longitude of the Moon.
    
    Returns:
    
    L - Ω
  - getFDot
```
public double getFDot()
```
    Get L - Ω where L is the mean longitude of the Moon time derivative.
    
    Returns:
    
    L - Ω time derivative
  - getD
```
public double getD()
```
    Get the mean elongation of the Moon from the Sun.
    
    Returns:
    
    mean elongation of the Moon from the Sun.
  - getDDot
```
public double getDDot()
```
    Get the mean elongation of the Moon from the Sun time derivative.
    
    Returns:
    
    mean elongation of the Moon from the Sun time derivative.
  - getOmega
```
public double getOmega()
```
    Get the mean longitude of the ascending node of the Moon.
    
    Returns:
    
    mean longitude of the ascending node of the Moon.
  - getOmegaDot
```
public double getOmegaDot()
```
    Get the mean longitude of the ascending node of the Moon time derivative.
    
    Returns:
    
    mean longitude of the ascending node of the Moon time derivative.

Class DelaunayArguments

Constructor Summary

Method Summary

Methods inherited from class java.lang.Object

Constructor Detail

DelaunayArguments

Method Detail

getDate

getTC

getGamma

getGammaDot

getL

getLDot

getLPrime

getLPrimeDot

getF

getFDot

getD

getDDot

getOmega

getOmegaDot