KozaiIzsakMeanElements Constructor (Cartesian, Cartesian, Double, Double, Double)

Initialize a set of Kozai-Izsak mean elements from a Cartesian position and velocity. Please note that there must be a correspondence between the inertial and fixed frames used for the input position and velocity. Specifically, the XY plane of the input motion should correspond to the equatorial plane.

Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 25.1.421.0 (25.1.421.0)

Syntax

C++

Copy

public KozaiIzsakMeanElements(
	Cartesian position,
	Cartesian velocity,
	double gravitationalParameter,
	double j2UnnormalizedValue,
	double referenceDistance
)

Public Sub New ( 
	position As Cartesian,
	velocity As Cartesian,
	gravitationalParameter As Double,
	j2UnnormalizedValue As Double,
	referenceDistance As Double
)

public:
KozaiIzsakMeanElements(
	Cartesian position, 
	Cartesian velocity, 
	double gravitationalParameter, 
	double j2UnnormalizedValue, 
	double referenceDistance
)

new : 
        position : Cartesian * 
        velocity : Cartesian * 
        gravitationalParameter : float * 
        j2UnnormalizedValue : float * 
        referenceDistance : float -> KozaiIzsakMeanElements

Parameters

position: Type: AGI.Foundation.CoordinatesCartesian
The Cartesian position.
velocity: Type: AGI.Foundation.CoordinatesCartesian
The Cartesian velocity.
gravitationalParameter: Type: SystemDouble
The gravitational parameter to use to create this set.
j2UnnormalizedValue: Type: SystemDouble
The non-normalized J2 zonal harmonic coefficient.
referenceDistance: Type: SystemDouble
The reference distance (equatorial radius) associated with the J2 coefficient.

Exceptions

Exception	Condition
ArgumentException	The given elements must represent a closed orbit. Thrown when the eccentricity is negative or not below unity or if the semimajor axis is not finitely positive.

Reference

KozaiIzsakMeanElements Class

KozaiIzsakMeanElements Overload

AGI.Foundation.Coordinates Namespace