KeplerianElements Constructor (DelaunayElements, Double, Double)

Initialize a set of classical Keplerian elements from a set of DelaunayElements.

Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

public KeplerianElements(
	DelaunayElements elements,
	double eccentricityTolerance,
	double inclinationTolerance
)

Public Sub New ( 
	elements As DelaunayElements,
	eccentricityTolerance As Double,
	inclinationTolerance As Double
)

public:
KeplerianElements(
	DelaunayElements^ elements, 
	double eccentricityTolerance, 
	double inclinationTolerance
)

new : 
        elements : DelaunayElements * 
        eccentricityTolerance : float * 
        inclinationTolerance : float -> KeplerianElements

elements: Type: AGI.Foundation.CoordinatesDelaunayElements
A set of Delaunay elements.
eccentricityTolerance: Type: SystemDouble
The tolerance which defines the value of 'zero' to use when checking whether the eccentricity is zero below which the orbit is circular.
inclinationTolerance: Type: SystemDouble
The tolerance which defines the value of 'zero' to use when checking whether the inclination is zero below which the orbit is equatorial.

Exceptions

Exception	Condition
ArgumentNullException	Thrown when the parameter elements is .
ArgumentOutOfRangeException	Thrown if either eccentricityTolerance or inclinationTolerance is negative.