KeplerianElements Constructor (Cartesian, Cartesian, Double)

Initialize a set of classical Keplerian elements from a Cartesian position and velocity. The given elements must represent a closed orbit. For other orbit types, use ModifiedKeplerianElements.

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

Syntax

C++

Copy

public KeplerianElements(
	Cartesian position,
	Cartesian velocity,
	double gravitationalParameter
)

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

public:
KeplerianElements(
	Cartesian position, 
	Cartesian velocity, 
	double gravitationalParameter
)

new : 
        position : Cartesian * 
        velocity : Cartesian * 
        gravitationalParameter : float -> KeplerianElements

Parameters

position: Type: AGI.Foundation.CoordinatesCartesian
The cartesian position (distance).
velocity: Type: AGI.Foundation.CoordinatesCartesian
The cartesian velocity (distance per time).
gravitationalParameter: Type: SystemDouble
The gravitational parameter to use to create this set (distance cubed per time squared).

Exceptions

Exception	Condition
ArgumentOutOfRangeException	Thrown when the eccentricity is negative or not below unity or if the semimajor axis is not finitely positive.

Reference

KeplerianElements Class

KeplerianElements Overload

AGI.Foundation.Coordinates Namespace