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OrbitalElementsPerifocalToCartesianMatrix Method

Calculates the transformation matrix from the perifocal axes to the inertial axes.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 19.1.398.0 (19.1.398.0)
Syntax
public static Matrix3By3 PerifocalToCartesianMatrix(
	double argumentOfPeriapsis,
	double inclination,
	double ascendingNodeRightAscension
)

Parameters

argumentOfPeriapsis
Type: SystemDouble
The argument of periapsis (radians).
inclination
Type: SystemDouble
The inclination (radians).
ascendingNodeRightAscension
Type: SystemDouble
The right ascension of the ascending node (radians).

Return Value

Type: Matrix3By3
The transformation matrix to convert from the perifocal coordinate system to inertial cartesian coordinates.
See Also