Inertial optical stabilizer

Machine element or mechanism – Gyroscopes – With caging or parking means

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Details

74 522, 74 56A, 33275G, 33318, 356149, G01C 1924

Patent

active

040275400

ABSTRACT:
Gyroscope instrumentation for providing stabilization of the direction of a ine-of-sight of more than 45.degree. about one or more axes is described utilizing a two axes optical system. An inner gimbal supports a gyro rotor and a first mirror diagonal with a clearance window to admit light. The gyro rotor keeps the first mirror aligned in a fixed direction relative to an inner gimbal axis. The inner gimbal is supported by an outer gimbal. The outer gimbal has a second mirror mounted on it. The gyro rotor keeps the second mirror aligned with the outer gimbal axis. The net effect is that the optical axis at the input has a fixed orientation in space and the optical axis at the output axis has a fixed orientation relative to a platform on which the system is mounted.

REFERENCES:
patent: 2177094 (1939-10-01), Carter et al.
patent: 2470773 (1949-05-01), Haskins, Jr.
patent: 2505819 (1950-05-01), Wrigley
patent: 2567053 (1951-09-01), Catravas
patent: 2905371 (1955-04-01), Hammond, Jr.
patent: 3097299 (1963-07-01), Rasmussen
patent: 3205718 (1965-09-01), Wierenga et al.
patent: 3522993 (1970-08-01), Gabriet

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