Click or drag to resize

StkEphemerisFileCovarianceTimePosVelCreateBlender Method (StkEphemerisFileEphemerisTimePosVel)

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

The InertialPropagationFrame is set to the inertial frame of the instance of EarthCentralBody in the CentralBodiesFacet of the CalculationContext. The GravitationalParameter is set to that of the WorldGeodeticSystem1984.

Namespace:  AGI.Foundation.Stk
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.2.419.0 (24.2.419.0)
Syntax
public Covariance6By6TwoBodyBlender CreateBlender(
	StkEphemerisFileEphemerisTimePosVel orbitStates
)

Parameters

orbitStates
Type: AGI.Foundation.StkStkEphemerisFileEphemerisTimePosVel
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.

Return Value

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