To study the effectiveness of various control system design methodologies, the NASA Langley Research Center initiated the Benchmark Active Controls Project. In this project, the various methodologies were applied to design a flutter suppression system for the Benchmark Active Controls Technology (BACT) Wing. This report describes the user's manual and software toolbox developed at the University of Washington to design a multirate flutter suppression control law for the BACT wing.
Multirate Flutter Suppression System Design for the Benchmark Active Controls Technology Wing
2002-12-01
Report
No indication
English
Multirate Flutter Suppression System Design for a Model Wing
Online Contents | 1994
|SCAR arrow-wing active flutter suppression system
NTRS | 1977
|Scar Arrow-Wing Active Flutter Suppression System
NTIS | 1977
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