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Volumn 21, Issue 5, 1998, Pages 718-725

Stability and control of a structurally nonlinear aeroelastic system

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ASYMPTOTIC STABILITY; BIFURCATION (MATHEMATICS); CLOSED LOOP CONTROL SYSTEMS; CONTROL NONLINEARITIES; CONTROL SYSTEM ANALYSIS; EQUATIONS OF MOTION; FEEDBACK; LINEARIZATION; SYSTEM STABILITY;

EID: 0032166295     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4317     Document Type: Article
Times cited : (149)

References (22)
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    • Dowell, E.H.1
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    • Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity
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  • 10
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    • Chaotic Motions of an Airfoil with Nonlinear Stiffness in Incompressible Flow
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    • March
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  • 22
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    • Adaptive Feedback Linearization for the Control of a Typical Wing Section with Structural Nonlinearity
    • to be published
    • Ko, J., Strganac, T. W., and Kurdila, A. J., "Adaptive Feedback Linearization for the Control of a Typical Wing Section with Structural Nonlinearity," Nonlinear Dynamics (to be published).
    • Nonlinear Dynamics
    • Ko, J.1    Strganac, T.W.2    Kurdila, A.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.