Covariance6By6TwoBodyBlender Constructor (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.

Namespace: AGI.Foundation.NumericalMethods
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public Covariance6By6TwoBodyBlender(
	DateMotionCollection<Cartesian> orbitStates,
	IDateMotionCollection<Matrix6By6Symmetric> covarianceData
)

Public Sub New ( 
	orbitStates As DateMotionCollection(Of Cartesian),
	covarianceData As IDateMotionCollection(Of Matrix6By6Symmetric)
)

public:
Covariance6By6TwoBodyBlender(
	DateMotionCollection<Cartesian>^ orbitStates, 
	IDateMotionCollection<Matrix6By6Symmetric^>^ covarianceData
)

new : 
        orbitStates : DateMotionCollection<Cartesian> * 
        covarianceData : IDateMotionCollection<Matrix6By6Symmetric> -> Covariance6By6TwoBodyBlender

Parameters

orbitStates: Type: AGI.FoundationDateMotionCollectionCartesian
The position and velocity vectors of the spacecraft at the same times as the covarianceData.
covarianceData: Type: AGI.FoundationIDateMotionCollectionMatrix6By6Symmetric
The covariance data that is used for blending.

Exceptions

Exception	Condition
ArgumentNullException	Thrown when covarianceData is .

Reference

Covariance6By6TwoBodyBlender Class

Covariance6By6TwoBodyBlender Overload

AGI.Foundation.NumericalMethods Namespace