Control of a Nonlinear Wing Section Using Leading- and Trailing-Edge Surfaces

The control of nonlinear aeroelastic response of a wing section with a continuous stiffening-type structural nonlinearity is examined through analytical and experimental studies. Motivated by the limited effectiveness of using a single, trailing-edge control surface for the suppression of limit-cycl...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2004-01, Vol.27 (1), p.52-58
Hauptverfasser:	Platanitis, George, Strganac, Thomas W
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engineering Applied sciences Computer science control theory systems Control theory Control theory. Systems Controllers Exact sciences and technology Experiments Nonlinear control
Online-Zugang:	Volltext
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