Application of output feedback sliding mode control to active flutter suppression of two-dimensional airfoil
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-010-0099-z.pdf
Reference24 articles.
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3. Roger K L, Hodges G E, Felt L. Active flutter suppression-a flight test demonstration. J Aircraft, 1975, 12(6): 551–556
4. Waszak M R, Srinathkumar S. Flutter suppression for the active flexible wing: control system design and experimental validation. AIAA-92-2097, 1992
5. Waszak M R, Srinathkumar S. Flutter suppression for the active flexible wing: a classical design. J Aircraft, 1995, 32(1): 61–67
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