System for automatically guiding a missile and missile provided

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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244 315, F41G 722

Patent

active

047353791

ABSTRACT:
This invention relates to a multi-target guiding system for missile, wherein it is provided with an electronic scanning antenna; it effects a classification of the targets by order of priority and orients the missile by controlling the control surfaces towards the target of highest priority. During classification, the system causes the direction of advance of said missile to vary in order to maintain said targets in its domain of action for as long as possible.

REFERENCES:
patent: 3779492 (1973-12-01), Grumet
patent: 3974328 (1976-08-01), Thomas et al.
patent: 4021801 (1977-05-01), Chernick
patent: 4108400 (1978-08-01), Groutage et al.
patent: 4136343 (1979-01-01), Heffner et al.
Decision Theunetic Target Classification by J. P. Toomey & C. L. Bennett--Paper at 1980 Symposium of IEEE on Antennas--and Propagation.

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