CovarianceTimePosVelCreateBlender Method

Overload List

	Name	Description
	CreateBlender(StkEphemerisFileEphemerisTimePosVel)	Creates a two-body covariance blender from the orbit states ephemeris and the covariance data. Also, sets the Blender property to the created value. The InertialPropagationFrame is set to the inertial frame of the instance of EarthCentralBody in the CentralBodiesFacet of the CalculationContext. The GravitationalParameter is set to that of the WorldGeodeticSystem1984.
	CreateBlender(StkEphemerisFileEphemerisTimePosVel, ReferenceFrame, NullableDouble)	Creates a two-body covariance blender from the orbit states ephemeris and the covariance data. Also, sets the Blender property to the created value.

CovarianceTimePosVelAddLanguageSpecificTextSet("LST49D257F1_0?cpp=::|nu=.");CreateBlender Method