Adaptive control of a nonlinear aeroelastic system

Aerospace Science and Technology

Volumn 15, Issue 5, 2011, Pages 343-352

  Li, Daochun ^a   Xiang, Jinwu ^a   Guo, Shijun ^b  

^a BEIHANG UNIVERSITY   (China)

^b CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

Adaptive control; Aeroelastic airfoil; Nonlinearity; Parametric uncertainty

Indexed keywords

ADAPTIVE CONTROL; ADAPTIVE CONTROL LAW; ADAPTIVE CONTROLLERS; AEROELASTIC AIRFOIL; AEROELASTIC SYSTEM; CONTROL LAWS; DEGREE OF FREEDOM; FLUTTER BOUNDARIES; FLUTTER CONTROL; FLUTTER SPEED; FLUTTER SUPPRESSION; INITIAL CONDITIONS; LEADING EDGE; LIMIT CYCLE OSCILLATIONS; NON-LINEARITY; NONLINEAR AEROELASTIC SYSTEM; NONLINEAR POLYNOMIALS; OPEN LOOPS; PARAMETRIC UNCERTAINTIES; PARTIAL FEEDBACK LINEARIZATION; PITCH STIFFNESS; POSITIVE EFFECTS; STRUCTURAL STIFFNESS; STRUCTURED MODEL; TIME DOMAIN; WING SECTION;

AEROELASTICITY; AIRFOILS; CONTROL SURFACES; CONTROL THEORY; DAMPING; FEEDBACK LINEARIZATION; FLUTTER (AERODYNAMICS); STIFFNESS;

MODEL REFERENCE ADAPTIVE CONTROL;

EID: 79959963373     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2010.08.006     Document Type: Article

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