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

Initialize a set of Kozai-Izsak mean orbital elements. Inputs are assumed to be mean elements.

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(
	double radius,
	double radiusDot,
	double parameter,
	double argumentOfLatitude,
	double inclination,
	double rightAscensionOfAscendingNode,
	double gravitationalParameter,
	double j2UnnormalizedValue,
	double referenceDistance
)

Public Sub New ( 
	radius As Double,
	radiusDot As Double,
	parameter As Double,
	argumentOfLatitude As Double,
	inclination As Double,
	rightAscensionOfAscendingNode As Double,
	gravitationalParameter As Double,
	j2UnnormalizedValue As Double,
	referenceDistance As Double
)

public:
KozaiIzsakMeanElements(
	double radius, 
	double radiusDot, 
	double parameter, 
	double argumentOfLatitude, 
	double inclination, 
	double rightAscensionOfAscendingNode, 
	double gravitationalParameter, 
	double j2UnnormalizedValue, 
	double referenceDistance
)

new : 
        radius : float * 
        radiusDot : float * 
        parameter : float * 
        argumentOfLatitude : float * 
        inclination : float * 
        rightAscensionOfAscendingNode : float * 
        gravitationalParameter : float * 
        j2UnnormalizedValue : float * 
        referenceDistance : float -> KozaiIzsakMeanElements

Parameters

radius: Type: SystemDouble
Mean magnitude of position vector.
radiusDot: Type: SystemDouble
Mean rate of change of magnitude of position vector.
parameter: Type: SystemDouble
Mean semi-latus rectum.
argumentOfLatitude: Type: SystemDouble
Mean argument of latitude.
inclination: Type: SystemDouble
Mean inclination (radians).
rightAscensionOfAscendingNode: Type: SystemDouble
Mean right ascension of the ascending node.
gravitationalParameter: Type: SystemDouble
The gravitational parameter.
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. The exception is thrown if the eccentricity is not below unity or if the semimajor axis is not finitely positive.
ArgumentException	The semimajor axis cannot be zero or nearly zero. Thrown if the computed semimajor axis is less than Epsilon8.

Reference

KozaiIzsakMeanElements Class

KozaiIzsakMeanElements Overload

AGI.Foundation.Coordinates Namespace