Optical guide beam steering for projectiles

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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F41G 724

Patent

active

050186841

ABSTRACT:
In an optical beam riding guidance for missiles according to the beam rider method, a definite recognition of the roll attitude and the location assignment is carried out in dependence on the expiring time in a simple manner and without previous synchronization with the launching installation.

REFERENCES:
patent: 4020339 (1977-04-01), Gustafson
patent: 4030686 (1977-06-01), Buchman
patent: 4318591 (1982-03-01), Elterman

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