Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1972-05-08
1978-05-02
Tudor, Harold
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
350 16, 356248, G02B 2302
Patent
active
040870618
ABSTRACT:
A wide angle seeker for missile guidance systems and the like which utili a dual motion mirror in an optical transfer system to allow a missile sensor to be mounted in a stationary position in the missile body remote from the seeker.
REFERENCES:
patent: 2873381 (1959-02-01), Lauroesch
patent: 3100264 (1963-08-01), Jaffe et al.
patent: 3165749 (1965-01-01), Cushner
patent: 3293437 (1966-12-01), Boydell
patent: 3612643 (1971-10-01), Weber
patent: 3617016 (1971-11-01), Bolsey
patent: 3698790 (1972-10-01), Berry
Hennen Thomas W.
Miller Roy
Sciascia R. S.
The United States of America as represented by the Secretary of
Tudor Harold
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