Flutter suppression (FS) is one of the active control concepts being investigated by the AFW program. The design goal for FS control laws was to increase the passive flutter dynamic pressure by 30 percent. In order to meet this goal, the FS control laws had to be capable of suppressing both symmetric and antisymmetric flutter instabilities simultaneously. In addition, the FS control laws had to be practical and low-order, robust and capable of real time execution within the 200 hz. sampling time. The purpose here is to present an overview of the development, simulation validation, and wind tunnel testing of a digital controller system for flutter suppression.
Development, simulation validation, and wind tunnel testing of a digital controller system for flutter suppression
01.03.1991
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2014
|AIAA-2004-1854 Wind-Tunnel Model and a Controller for Flutter Suppression
British Library Conference Proceedings | 2004
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