System for guiding remote-controlled missiles

Details System for guiding remote-controlled missiles System for guiding remote-controlled missiles

1979-10-31

1982-02-02

Cangialosi, Sal

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

F41G 700

Patent

active

043135803

ABSTRACT:
The present invention relates to a system for guiding remote-controlled missiles, enabling these missiles to be fired by bursts, comprising a sighting device, an angular deviation measuring (ADM) device and a device for controlling the path; according to the invention, partial, individual and separate fields are defined in the field of the ADM device, said fields corresponding to various zones where successive missiles may be addressed, and said control device is designed for simultaneously guiding a plurality of missiles on a plurality of distinct predetermined standby courses spaced apart with respect to said line of sight. The invention finds particular application in the guiding of ground-ground, ground-air, or air-ground missiles.

REFERENCES:
patent: 2930894 (1960-03-01), Bozeman
patent: 3544217 (1970-12-01), McEntyre
patent: 4143836 (1979-03-01), Rieger

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