Two-axis gimbal arrangement

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

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F41G 726

Patent

active

052191320

ABSTRACT:
A gyroscopically stabilized optical seeker for use in a cannon-launched projectile is shown to include a gimbal arrangement wherein a two-axis rate gyroscope and associated torque motors are utilized to attain the requisite stabilization however such seeker is oriented with respect to such projectile, the two-axis rate gyroscope being arranged so that the complete optical system, including the detector unit, may be mounted on the inner gimbal.

REFERENCES:
patent: 2963973 (1960-12-01), Estey
patent: 3729172 (1973-04-01), Stephenson
patent: 4009848 (1977-03-01), Albert et al.
patent: 4039246 (1977-08-01), Voigt
patent: 4155521 (1979-05-01), Evans et al.
patent: 4168813 (1979-09-01), Pinson et al.

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