Continuous Robust Control for Two-Dimensional Airfoils with Leading- and Trailing-Edge Flaps | Zendy

Z. Wang | Zendy; Aman Behal | Zendy; Pier Marzocca | Zendy

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Continuous Robust Control for Two-Dimensional Airfoils with Leading- and Trailing-Edge Flaps

Author(s) -

Z. Wang,

Aman Behal,

Pier Marzocca

Publication year - 2012

Publication title -

journal of guidance control and dynamics

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 1.573

H-Index - 143

eISSN - 1533-3884

pISSN - 0731-5090

DOI - 10.2514/1.54347

Subject(s) - airfoil , trailing edge , control theory (sociology) , aeroelasticity , limit (mathematics) , bounded function , flight control surfaces , leading edge , computer science , stability (learning theory) , robust control , aerodynamics , physics , control (management) , nonlinear system , mathematics , mechanics , mathematical analysis , artificial intelligence , quantum mechanics , machine learning

yields a semiglobal asymptotic stability result, leading to rapid suppression of the plunging and pitching motions. Numerical simulation results demonstrate the performance of the multi-input/multi-output continuous robust control toward suppressing aeroelastic vibration and limit cycle oscillations at pre- and postflutter flight-speed regimes, even in the presence of bounded unknown external disturbance.

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