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A summary of the Active Flexible Wing programThis paper presents a summary of the NASA/Rockwell Active Flexible Wing program. Major elements of the program are presented. Key program accomplishments included single- and multiple-mode flutter suppression, load alleviation and load control during rapid roll maneuvers, and multi-input/multi-ouput multiple-function active controls tests above the open-loop flutter boundary.
Document ID
19920053028
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Perry, Boyd, III
(NASA Langley Research Center Hampton, VA, United States)
Cole, Stanley R.
(NASA Langley Research Center Hampton, VA, United States)
Miller, Gerald D.
(Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 92-2080
Report Number: AIAA PAPER 92-2080
Meeting Information
Meeting: AIAA Dynamics Specialists Conference
Location: Dallas, TX
Country: United States
Start Date: April 16, 1992
End Date: April 17, 1992
Accession Number
92A35652
Distribution Limits
Public
Copyright
Other

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