메뉴 건너뛰기




Volumn 5, Issue 2, 1996, Pages 216-224

Optimal sizing and placement of piezo-actuators for active flutter suppression

Author keywords

[No Author keywords available]

Indexed keywords

DOUBLET LATTICE METHOD; FLUTTER SUPPRESSION; LAMINATED PLATE WING; LINEAR QUADRATIC REGULATOR THEORY; MINIMUM STATE METHOD; RITZ SOLUTION TECHNIQUE;

EID: 0030125179     PISSN: 09641726     EISSN: None     Source Type: Journal    
DOI: 10.1088/0964-1726/5/2/010     Document Type: Article
Times cited : (33)

References (25)
  • 2
    • 0023437632 scopus 로고
    • Use of piezoelectric actuators as elements of intelligent structures
    • Crawley E F and de Luis J 1987 Use of piezoelectric actuators as elements of intelligent structures AIAA J. 25 1373-85
    • (1987) AIAA J. , vol.25 , pp. 1373-1385
    • Crawley, E.F.1    De Luis, J.2
  • 11
    • 0004728588 scopus 로고
    • An analytical and experimental investigation of flutter suppression via piezoelectric actuators
    • AIAA Paper 92-2106
    • Heeg J 1992 An analytical and experimental investigation of flutter suppression via piezoelectric actuators Proc. AIAA Dynamics Specialist Conf. (1991) AIAA Paper 92-2106
    • (1992) Proc. AIAA Dynamics Specialist Conf. (1991)
    • Heeg, J.1
  • 13
  • 14
    • 0028993516 scopus 로고
    • Optimal design of adaptive composite lifting surface for flutter suppression
    • Nam C and Kim Y 1995 Optimal design of adaptive composite lifting surface for flutter suppression AIAA J. 33 1897-904
    • (1995) AIAA J. , vol.33 , pp. 1897-1904
    • Nam, C.1    Kim, Y.2
  • 17
    • 85007685430 scopus 로고
    • A doublet-lattice method for calculating lift distributions in oscillating surfaces in subsonic flows
    • Albano E and Rodden W P 1969 A doublet-lattice method for calculating lift distributions in oscillating surfaces in subsonic flows AIAA J. 7 279-85
    • (1969) AIAA J. , vol.7 , pp. 279-285
    • Albano, E.1    Rodden, W.P.2
  • 18
    • 0020098320 scopus 로고
    • Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling
    • Karpel M 1982 Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling J. Aircraft 19 221-7
    • (1982) J. Aircraft , vol.19 , pp. 221-227
    • Karpel, M.1
  • 19
    • 0026257294 scopus 로고
    • Application of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximations
    • Hoadley S T and Karpel M 1991 Application of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximations J. Guidance, Control, Dynamics 14 1267-76
    • (1991) J. Guidance, Control, Dynamics , vol.14 , pp. 1267-1276
    • Hoadley, S.T.1    Karpel, M.2
  • 21
    • 0014735304 scopus 로고
    • On the determination of the optimal constant output feedback gains for linear multivariable systems
    • Levine W S and Athans M 1970 On the determination of the optimal constant output feedback gains for linear multivariable systems IEEE Trans. Automatic Control AC-15 44-8
    • (1970) IEEE Trans. Automatic Control , vol.AC-15 , pp. 44-48
    • Levine, W.S.1    Athans, M.2
  • 22
    • 0022118227 scopus 로고
    • Convergence of a numerical algorithm for calculating optimal output feedback gains
    • Moerder D D and Calise A J 1985 Convergence of a numerical algorithm for calculating optimal output feedback gains IEEE Trans. Automatic Control AC-30 900-3
    • (1985) IEEE Trans. Automatic Control , vol.AC-30 , pp. 900-903
    • Moerder, D.D.1    Calise, A.J.2
  • 24
    • 0018534152 scopus 로고
    • Optimal output feedback by gradient methods with optimal stepsize adjustment
    • Mueller G S and Adeniyi V O 1979 Optimal output feedback by gradient methods with optimal stepsize adjustment Proc. IEE, Control and Science vol 126
    • (1979) Proc. IEE, Control and Science , vol.126
    • Mueller, G.S.1    Adeniyi, V.O.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.