Wide angle seeker

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

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Details

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

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