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: 24.3.420.0 (24.3.420.0)
Syntax public static Matrix3By3 PerifocalToCartesianMatrix(
double argumentOfPeriapsis,
double inclination,
double ascendingNodeRightAscension
)
Public Shared Function PerifocalToCartesianMatrix (
argumentOfPeriapsis As Double,
inclination As Double,
ascendingNodeRightAscension As Double
) As Matrix3By3
public:
static Matrix3By3 PerifocalToCartesianMatrix(
double argumentOfPeriapsis,
double inclination,
double ascendingNodeRightAscension
)
static member PerifocalToCartesianMatrix :
argumentOfPeriapsis : float *
inclination : float *
ascendingNodeRightAscension : float -> Matrix3By3
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:
Matrix3By3The transformation matrix to convert from the perifocal coordinate system to inertial cartesian coordinates.
See Also