Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2007-09-25
2007-09-25
Gregory, Bernarr E. (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
C244S003100, C244S003150, C342S061000, C342S062000, C102S384000
Reexamination Certificate
active
07409512
ABSTRACT:
The centroid of the discrete components forming the overall radar return from a target onto which a homing weapon is being guided may not coincide with a desired aimpoint on the target. Herein proposed is the discrimination and comparison of returns from different portions of the weapon sensor's field-of-view, i.e. different portions of the target and guidance of the weapon in dependence upon the relative values of the differences between those returns. As a result, the weapon can hit say the center of a tank turret roof rather than the probably heavily armored area forward of the turret roof.
REFERENCES:
patent: 3107070 (1963-10-01), Willits et al.
patent: 4103847 (1978-08-01), Thomas et al.
BAE Systems plc
Gregory Bernarr E.
Nixon & Vanderhye P.C.
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