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
public Covariance6By6TwoBodyBlender CreateBlender( StkEphemerisFileEphemerisTimePosVel orbitStates )