Covariance6By6TwoBodyBlender Constructor (DateMotionCollection<Cartesian>, DateMotionCollection<Matrix>)

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

Namespace: AGI.Foundation.NumericalMethods
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 25.1.421.0 (25.1.421.0)

Syntax

public Covariance6By6TwoBodyBlender(
	DateMotionCollection<Cartesian> orbitStates,
	DateMotionCollection<Matrix> covarianceData
)

Public Sub New ( 
	orbitStates As DateMotionCollection(Of Cartesian),
	covarianceData As DateMotionCollection(Of Matrix)
)

public:
Covariance6By6TwoBodyBlender(
	DateMotionCollection<Cartesian>^ orbitStates, 
	DateMotionCollection<Matrix^>^ covarianceData
)

new : 
        orbitStates : DateMotionCollection<Cartesian> * 
        covarianceData : DateMotionCollection<Matrix> -> Covariance6By6TwoBodyBlender

orbitStates: Type: AGI.Foundation.DateMotionCollection<Cartesian>
The position and velocity vectors of the spacecraft at the same times as the covarianceData.
covarianceData: Type: AGI.Foundation.DateMotionCollection<Matrix>
The covariance data that is used for blending.