Solarized optical digital servo control system

Details Solarized optical digital servo control system Solarized optical digital servo control system

B - Operations, Transporting

64

C

341/81

B64C 27/04 (2006.01) B64C 13/50 (2006.01) G05D 1/00 (2006.01)

Patent

CA 1184271

- 17 - Solarized Optical Digital Servo Control System 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 elec- trical 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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