High-speed, high-G air bearing optical mount for Rosette scan ge

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

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F41G 712

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active

040047547

ABSTRACT:
A missile disposed for operation from a launch pad to impinge on a target th electromagnetic rays emanating therefrom includes a seeker for direction of the rays impinging thereon in patterns for alignment therewith and means for directing the missile to the target responsive to the alignment.

REFERENCES:
patent: 2948813 (1960-08-01), Osborne
patent: 3076095 (1963-01-01), Becklund et al.
patent: 3235733 (1966-02-01), Dauguet
patent: 3297395 (1967-01-01), Dardarian
patent: 3756538 (1973-09-01), McLean

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