Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1972-05-18
1976-08-17
Tudor, Harold
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
250203R, F41G 700, F42B 1502
Patent
active
039749851
ABSTRACT:
A two axis, three gimbal tracker for use with a missile or the like. The cker utilizes a lens barrel which has unlimited angular freedom in one axis, and more than 50.degree. of angular freedom in the other axis, and is mounted to the side of the carrying vehicle.
REFERENCES:
patent: 2941082 (1960-06-01), Carbonara et al.
patent: 3015249 (1962-01-01), Taylor
patent: 3180587 (1965-04-01), Garner et al.
patent: 3219822 (1965-11-01), Kutzscher et al.
patent: 3293437 (1966-12-01), Boydell
patent: 3617016 (1968-05-01), Bolsey
Campbell John M.
Oestreich James W.
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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