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Covariance6By6TwoBodyBlender Constructor (DateMotionCollectionCartesian, DateMotionCollectionMatrix, ReferenceFrame, Axes, ReferenceFrame, Double)

Initializes a new instance.

Namespace:  AGI.Foundation.NumericalMethods
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)
Syntax
public Covariance6By6TwoBodyBlender(
	DateMotionCollection<Cartesian> orbitStates,
	DateMotionCollection<Matrix> covarianceData,
	ReferenceFrame orbitStatesFrame,
	Axes covarianceAxes,
	ReferenceFrame inertialPropagationFrame,
	double gravitationalParameter
)

Parameters

orbitStates
Type: AGI.FoundationDateMotionCollectionCartesian
The position and velocity vectors of the spacecraft at the same times as the covarianceData.
covarianceData
Type: AGI.FoundationDateMotionCollectionMatrix
The covariance data that is used for blending.
orbitStatesFrame
Type: AGI.Foundation.GeometryReferenceFrame
The native reference frame of the orbitStates.
covarianceAxes
Type: AGI.Foundation.GeometryAxes
The native axes of the covarianceData.
inertialPropagationFrame
Type: AGI.Foundation.GeometryReferenceFrame
The inertial propagation frame that is used to propagate the orbitStates and the covarianceData.
gravitationalParameter
Type: SystemDouble
The gravitational parameter of the central body that the spacecraft is orbiting.
See Also