Click or drag to resize

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: 24.1.418.0 (24.1.418.0)
Syntax
public KeplerianElements(
	Cartesian position,
	Cartesian velocity,
	double gravitationalParameter
)

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
ExceptionCondition
ArgumentOutOfRangeException Thrown when the eccentricity is negative or not below unity or if the semimajor axis is not finitely positive.
See Also