KozaiIzsakMeanElements Constructor (KeplerianElements, Boolean, Double, Double)

Initialize a set of Kozai-Izsak mean elements from a set of osculating or mean KeplerianElements.

Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public KozaiIzsakMeanElements(
	KeplerianElements elements,
	bool inputIsMean,
	double j2UnnormalizedValue,
	double referenceDistance
)

Public Sub New ( 
	elements As KeplerianElements,
	inputIsMean As Boolean,
	j2UnnormalizedValue As Double,
	referenceDistance As Double
)

public:
KozaiIzsakMeanElements(
	KeplerianElements^ elements, 
	bool inputIsMean, 
	double j2UnnormalizedValue, 
	double referenceDistance
)

new : 
        elements : KeplerianElements * 
        inputIsMean : bool * 
        j2UnnormalizedValue : float * 
        referenceDistance : float -> KozaiIzsakMeanElements

Parameters

elements: Type: AGI.Foundation.CoordinatesKeplerianElements
The Keplerian elements.
inputIsMean: Type: SystemBoolean
True if input elements are mean elements, false if input elements are osculating.
j2UnnormalizedValue: Type: SystemDouble
The non-normalized J2 zonal harmonic coefficient of the central body around which to propagate.
referenceDistance: Type: SystemDouble
The reference distance (equatorial radius) associated with the J2 coefficient.

Exceptions

Exception	Condition
ArgumentNullException	Thrown when the parameter elements is null.
ArgumentException	The given elements must represent a closed orbit. The exception is thrown if the eccentricity is negative or not below unity or if the semimajor axis is not finitely positive. For other orbit types, use ModifiedKeplerianElements.

Reference

KozaiIzsakMeanElements Class

KozaiIzsakMeanElements Overload

AGI.Foundation.Coordinates Namespace