Covariance6By6TwoBodyBlender Constructor

Overload List

	Name	Description
	Covariance6By6TwoBodyBlender(DateMotionCollectionCartesian, DateMotionCollectionMatrix)	Initializes a new instance. By default, the OrbitStatesFrame and InertialPropagationFrame are set to the inertial frame of the instance of EarthCentralBody in the CentralBodiesFacet of the CalculationContext. Similarly, the CovarianceAxes are set to the Axes of that inertial frame. The GravitationalParameter is set to that of the WorldGeodeticSystem1984. to the
	Covariance6By6TwoBodyBlender(DateMotionCollectionCartesian, IDateMotionCollectionMatrix6By6Symmetric)	Initializes a new instance. By default, the OrbitStatesFrame and InertialPropagationFrame are set to the inertial frame of the instance of EarthCentralBody in the CentralBodiesFacet of the CalculationContext. Similarly, the CovarianceAxes are set to the Axes of that inertial frame. The GravitationalParameter is set to that of the WorldGeodeticSystem1984.
	Covariance6By6TwoBodyBlender(DateMotionCollectionCartesian, DateMotionCollectionMatrix, ReferenceFrame, Axes, ReferenceFrame, Double)	Initializes a new instance.
	Covariance6By6TwoBodyBlender(DateMotionCollectionCartesian, IDateMotionCollectionMatrix6By6Symmetric, ReferenceFrame, Axes, ReferenceFrame, Double)	Initializes a new instance.