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Use of active control technology to improve ride qualities of large transport aircraftAnalyses, construction and flight testing of two systems: Beta-vane and Modal Suppression Augmentation System (MSAS), which were developed to suppress gust induced lateral accelerations of large aircraft, are described. The 747 transport was used as the test vehicle. The purpose of the Beta-vane system is to reduce acceleration levels at the dutch roll frequency whereas the function of the MSAS system is to reduce accelerations due to flexible body motions caused by turbulence. Data from flight test, with both systems engaged shows a 50 to 70 percent reduction in lateral aft body acceleration levels. Furthermore, it is suggested that present day techniques used for developing dynamic equations of motion in the flexible mode region are limited.
Document ID
19760024062
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cohen, G. C.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Cotter, C. J.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Taylor, D. L.
(Boeing Commercial Airplane Co. Seattle, WA, 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
76N31150
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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