Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1991-08-30
1993-05-18
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 316, F41G 722
Patent
active
052113566
ABSTRACT:
A method for rejecting inaccurate subimages is disclosed for subimages used to track an aimpoint. The difference between the actual location of each subimage and the location of the subimage based on an estimated aimpoint is compared to a threshold value. The subimage is discarded if the difference exceeds the threshold value. The aimpoint may then be reestimated using the revised set of subimages.
REFERENCES:
patent: 3912198 (1975-10-01), Dell et al.
patent: 4133004 (1979-01-01), Fitts
patent: 4476494 (1984-10-01), Tugaye
McWilliams Joel K.
Van Rheeden Don R.
Donaldson Richard L.
Grossman Rene E.
Jordan Charles T.
Texas Instruments Incorporated
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