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StkEphemerisFile.CovarianceTimePosVel.CreateBlender Method (StkEphemerisFile.EphemerisTimePosVel, ReferenceFrame, Nullable<Double>)

Creates a two-body covariance blender from the orbit states ephemeris and the covariance data. Also, sets the Blender property to the created value.

Namespace:  AGI.Foundation.Stk
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)
Syntax
public Covariance6By6TwoBodyBlender CreateBlender(
	StkEphemerisFile.EphemerisTimePosVel orbitStates,
	ReferenceFrame inertialPropagationFrame,
	double? gravitationalParameter
)

Parameters

orbitStates
Type: AGI.Foundation.Stk.StkEphemerisFile.EphemerisTimePosVel
The orbit states that are used for blending. These must be consistent with a spacecraft in a two-body orbital regime for the results to be correct.
inertialPropagationFrame
Type: AGI.Foundation.Geometry.ReferenceFrame
The inertial propagation frame that is used to propagate the orbitStates and the CovarianceData.
gravitationalParameter
Type: System.Nullable<Double>
The gravitational parameter of the central body that the spacecraft described by orbitStates is orbiting.

Return Value

Type: Covariance6By6TwoBodyBlender
The created two-body covariance blender.
See Also