Optical digital servo control system

Boots – shoes – and leggings

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244 1713, 244180, 244181, 318580, 318594, 364433, B64C 1350, B64C 1900, G05D 108

Patent

active

044438532

ABSTRACT:
An electrically controlled (16) mechanical actuator (13) is driven by optically generated (23) electrical power through an optically controlled (28) switch (26) in an electrically isolated module (20). Optical transducers (54, 62, 70) and feedback (29), as well as optical inputs (40, 89, etc.) to electrical signal processing equipment (46, 47, 49) in an electrically isolated module (22) dictate the electrical control (28). A helicopter flight control system is wholly digital, with solar remote power and optical intercommunication.

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patent: 4078749 (1978-03-01), Johnson, Jr.
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patent: 4119948 (1978-10-01), Ward et al.
patent: 4164120 (1979-08-01), Funk et al.
patent: 4168045 (1979-09-01), Wright et al.
patent: 4270168 (1981-05-01), Murphy et al.
patent: 4298839 (1981-11-01), Johnston
patent: 4313201 (1982-01-01), Fischer et al.

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