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Volumn 2005, Issue , 2005, Pages 93-98

Different affine decomposition of the model of the prototypical aeroelastic wing section by TP model transformation

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; MATHEMATICAL MODELS; MATRIX ALGEBRA; SOFTWARE PROTOTYPING;

EID: 33845489435     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/INES.2005.1555138     Document Type: Conference Paper
Times cited : (10)

References (15)
  • 3
    • 1942423639 scopus 로고    scopus 로고
    • TP model transformation as a way to LMI based controller design
    • April
    • P. Baranyi. TP model transformation as a way to LMI based controller design. IEEE Transaction on Industrial Electronics, 51(2), April 2004.
    • (2004) IEEE Transaction on Industrial Electronics , vol.51 , Issue.2
    • Baranyi, P.1
  • 4
    • 0042700003 scopus 로고    scopus 로고
    • From differential equations to PDC controller design via numerical transformation
    • P. Baranyi, D. Tikk, Y. Yam, and R. J. Patton. From differential equations to PDC controller design via numerical transformation. Computers in Industry, Elsevier Science, 51:281 -297, 2003.
    • (2003) Computers in Industry, Elsevier Science , vol.51 , pp. 281-297
    • Baranyi, P.1    Tikk, D.2    Yam, Y.3    Patton, R.J.4
  • 9
    • 0031275376 scopus 로고    scopus 로고
    • Nonlinear control of a prototypical wing section with torsional nonlinearity
    • November-December
    • J. Ko, A. J. Kurdila, and T. W. Strganac. Nonlinear control of a prototypical wing section with torsional nonlinearity. Journal, of Guidance, Control, and Dynamics, 20(6):1181-1189, November-December 1997.
    • (1997) Journal, of Guidance, Control, and Dynamics , vol.20 , Issue.6 , pp. 1181-1189
    • Ko, J.1    Kurdila, A.J.2    Strganac, T.W.3
  • 10
    • 0032166295 scopus 로고    scopus 로고
    • Stability and control of a structurally nonlinear aeroelastic system
    • J. Ko and T. W. Strganac. Stability and control of a structurally nonlinear aeroelastic system. Journal of Guidance, Control, and Dynamics, 21(5):718-725, 1998.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.5 , pp. 718-725
    • Ko, J.1    Strganac, T.W.2
  • 14
    • 0034314450 scopus 로고    scopus 로고
    • Adaptive output feedback control of a nonlinear aeroelastic structure
    • W. Xing and S. N. Singh. Adaptive output feedback control of a nonlinear aeroelastic structure. Journal of Guidance. Control, and Dynamics, 23(6):1109-1116. 2000.
    • (2000) Journal of Guidance. Control, and Dynamics , vol.23 , Issue.6 , pp. 1109-1116
    • Xing, W.1    Singh, S.N.2
  • 15
    • 0025415998 scopus 로고
    • Chaotic motions of an airfoil with nonlinear stiffness in incompressible flow
    • L. C. Zhao and Z. C. Yang. Chaotic motions of an airfoil with nonlinear stiffness in incompressible flow. Journal of Sound and Vibration, 138(2):245-254, 1990.
    • (1990) Journal of Sound and Vibration , vol.138 , Issue.2 , pp. 245-254
    • Zhao, L.C.1    Yang, Z.C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.