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Volumn 24, Issue 3, 2001, Pages 502-509

Adaptive output feedback control of an aeroelastic system with unstructured uncertainties

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONVERGENCE OF NUMERICAL METHODS; EQUATIONS OF MOTION; FEEDBACK CONTROL; MATHEMATICAL MODELS; SYSTEM STABILITY; UNCERTAIN SYSTEMS; WINGS;

EID: 0035333968     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4739     Document Type: Article
Times cited : (62)

References (26)
  • 4
    • 0020098320 scopus 로고
    • Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling
    • (1982) Journal of Aircraft , vol.19 , Issue.3 , pp. 221-227
    • Karpel, M.1
  • 6
    • 0003210433 scopus 로고
    • Analytical and experimental investigation of flutter suppression by piezoelectric actuation
    • Sept.
    • (1993) NASA TP 3241
    • Heeg, J.1
  • 11
    • 0022662802 scopus 로고
    • Flutter analysis of a two-dimensional airfoil with cubic nonlinear restoring force
    • National Aeronautical Establishment, Aeronautical Note 36, Canada National Research Council No. 25438, Ottawa, Canada, Feb.
    • (1986)
    • Lee, B.H.K.1    LeBlanc, P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.