Homing device system for missile

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

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Details

250342, 250347, 250334, 359213, 359214, F41G 700, F42B 1000, G01J 502, G02B 2608

Patent

active

058268200

ABSTRACT:
A guidance system for guiding a missile to a target including an array of photosensitive elements arranged orthogonally to the axis of the missile, a scanning arrangement for enabling scanning of the array of photosensitive elements by means of an optical system, and a target detecting arrangement for controlling the field and the pace of scanning executed by the scanning arrangement so that the field of scanning is smaller and the pace of scanning is greater after detecting a target than before target detection.

REFERENCES:
patent: 3603686 (1971-09-01), Paine et al.
patent: 3622788 (1971-11-01), Briggs
patent: 4123134 (1978-10-01), Meyers
patent: 4189747 (1980-02-01), Funari
patent: 4262199 (1981-04-01), Bridges et al.
patent: 4277039 (1981-07-01), Blanning et al.
patent: 4486662 (1984-12-01), Abel
patent: 4709876 (1987-12-01), Pinson

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