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B-52 stability augmentation system reliabilityThe B-52 SAS (Stability Augmentation System) was developed and retrofitted to nearly 300 aircraft. It actively controls B-52 structural bending, provides improved yaw and pitch damping through sensors and electronic control channels, and puts complete reliance on hydraulic control power for rudder and elevators. The system has experienced over 300,000 flight hours and has exhibited service reliability comparable to the results of the reliability test program. Development experience points out numerous lessons with potential application in the mechanization and development of advanced technology control systems of high reliability.
Document ID
19760024079
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bowling, T. C.
(Boeing Co. Wichita, KS, United States)
Key, L. W.
(Boeing Co. Wichita, KS, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: NASA. Dryden Flight Res. Center Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Stability And Control
Accession Number
76N31167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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