Experimental Nonlinear Control for Flutter Suppression in a Nonlinear Aeroelastic System
نویسندگان
چکیده
منابع مشابه
Adaptive Control of a Nonlinear Aeroelastic System
Aeroelastic two-dimensional wing section with both trailing-edge (TE) and leading-edge (LE) was investigated in this paper through numerical simulation in time domain. Structural stiffness and damping in pitch degree of freedom were represented by nonlinear polynomials. Open-loop limit cycle oscillation (LCO) characters of two examples were studied, and flutter boundaries with initial condition...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2017
ISSN: 0731-5090,1533-3884
DOI: 10.2514/1.g002519