Title :
Adaptive Control Algorithm for Flutter Suppression
Author_Institution :
HONEYWELL SYSTEMS & RESEARCH CENTER, Minneapolis, Minnesota
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;
Conference_Titel :
American Control Conference, 1983
Conference_Location :
San Francisco, CA, USA
