DocumentCode
485881
Title
Adaptive Control Algorithm for Flutter Suppression
Author
Harvey, C.A.
Author_Institution
HONEYWELL SYSTEMS & RESEARCH CENTER, Minneapolis, Minnesota
fYear
1983
fDate
22-24 June 1983
Firstpage
801
Lastpage
802
Abstract
Adaptive control of wing/store flutter was investigated and successfully demonstrated in wind tunnel tests in the NASA Langley Transonic Dynamics Tunnel. The complete adaptive control algorithm was exercised. It provided flutter suppression during varying flight conditions for a single store configuration.
Keywords
Adaptive control; Adaptive systems; Aerodynamics; Aerospace control; Aircraft; Feedback; Filtering; Frequency; Least squares approximation; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1983
Conference_Location
San Francisco, CA, USA
Type
conf
Filename
4788223
Link To Document