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Investigation of control law for active flutter suppressionDiscussed is the technology of active flutter suppression research by the use of the wind-tunnel model of a delta wing with low aspect ratio. The research includes the establishment of a mathematical model for the servo-aeroelastic system, and the synthesis and analysis of sub-optimal output feedback control laws for active flutter suppression.
Document ID
19880001436
Acquisition Source
Legacy CDMS
Document Type
Technical Translation (TT)
Authors
Wang, Weipeng (NASA Headquarters Washington, DC United States)
Gu, Zhongquan (NASA Headquarters Washington, DC United States)
Zhu, Demao (NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1987
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TT-20126
NAS 1.77:20126
Report Number: NASA-TT-20126
Report Number: NAS 1.77:20126
Accession Number
88N10818
Funding Number(s)
CONTRACT_GRANT: NASW-4005
Distribution Limits
Public
Copyright
Public Use Permitted.
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