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Volumn 212, Issue 4, 1998, Pages 287-298

A method for identification of non-linear multi-degree-of-freedom systems

Author keywords

Aeroelasticity; Bilinear stiffness; Cubic stiffness; Freeplay stiffness; Hysteresis; Multi degree of freedom systems; Non linear systems; System identification

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); FUNCTIONS; HYSTERESIS; STIFFNESS;

EID: 0032463321     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/0954410981532441     Document Type: Article
Times cited : (11)

References (13)
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    • 0001058679 scopus 로고
    • Spectral analysis for nonlinear systems. Part I: Parametric nonlinear spectral analysis
    • Billings, S. A. and Tsang, K. M. Spectral analysis for nonlinear systems. Part I: parametric nonlinear spectral analysis. Mech. Systems and Signal Processing, 1989, 3(4), 319-339.
    • (1989) Mech. Systems and Signal Processing , vol.3 , Issue.4 , pp. 319-339
    • Billings, S.A.1    Tsang, K.M.2
  • 2
    • 0024631931 scopus 로고
    • Representations of non-linear Systems: The NARMAX model
    • Chen, S. and Billings, S. A. Representations of non-linear Systems: the NARMAX model. Int. J. Control, 1989, 49(3), 1013-1032.
    • (1989) Int. J. Control , vol.49 , Issue.3 , pp. 1013-1032
    • Chen, S.1    Billings, S.A.2
  • 4
    • 38249017708 scopus 로고
    • Application of the forcestate mapping approach to the identification of non-linear systems
    • Al-Hadid, M. A. and Wright, J. R. Application of the forcestate mapping approach to the identification of non-linear systems. Mech. Systems and Signal Processing, 1990, 4(6), 463-482.
    • (1990) Mech. Systems and Signal Processing , vol.4 , Issue.6 , pp. 463-482
    • Al-Hadid, M.A.1    Wright, J.R.2
  • 5
    • 38249021289 scopus 로고
    • Developments in the force-state mapping technique for non-linear systems and the extension to the location of non-linear elements in a lumpedparameter system
    • Al-Hadid, M. A. and Wright, J. R. Developments in the force-state mapping technique for non-linear systems and the extension to the location of non-linear elements in a lumpedparameter system. Mech. Systems and Signal Processing, 1989,3(3), 269-290.
    • (1989) Mech. Systems and Signal Processing , vol.3 , Issue.3 , pp. 269-290
    • Al-Hadid, M.A.1    Wright, J.R.2
  • 7
    • 0005645146 scopus 로고
    • A new type of time series model for the identification of non-linear dynamical systems
    • Chen, Q. and Tomlinson, G. R. A new type of time series model for the identification of non-linear dynamical systems. Mech. Systems and Signal Processing, 1994, 8(5), 531-549.
    • (1994) Mech. Systems and Signal Processing , vol.8 , Issue.5 , pp. 531-549
    • Chen, Q.1    Tomlinson, G.R.2
  • 8
    • 0024011347 scopus 로고
    • Analysis of limit cycle flutter of an airfoil in incompressible flow
    • Yang, Z. C. and Zhao, L. C. Analysis of limit cycle flutter of an airfoil in incompressible flow. J. Sound Vibr., 1988, 123(1), 1-13.
    • (1988) J. Sound Vibr. , vol.123 , Issue.1 , pp. 1-13
    • Yang, Z.C.1    Zhao, L.C.2
  • 9
    • 0019063456 scopus 로고
    • An application of system identification to flutter testing
    • Gaukrogcr, D. R., Skingle, C. W. and Heron, K. H. An application of system identification to flutter testing. J. Sound Vibr., 1980,72(2), 141-150.
    • (1980) J. Sound Vibr. , vol.72 , Issue.2 , pp. 141-150
    • Gaukrogcr, D.R.1    Skingle, C.W.2    Heron, K.H.3
  • 11
    • 0022514714 scopus 로고
    • Identification of nonlinear structural elements by force-state mapping
    • Crawlcy, E. F. and Aubert, A. C. Identification of nonlinear structural elements by force-state mapping. Am. Inst. Aeronaut. Astronaut. J., 1986,24(1), 155-162.
    • (1986) Am. Inst. Aeronaut. Astronaut. J. , vol.24 , Issue.1 , pp. 155-162
    • Crawlcy, E.F.1    Aubert, A.C.2
  • 12
    • 0005324423 scopus 로고
    • Some effects of system non-linearities in the problem of aircraft flutter
    • NASA, October
    • Woolston, D. S., Runyan, H. L. and Byrdsong, T. A. Some effects of system non-linearities in the problem of aircraft flutter. Technical Note TN 3539, NASA, October 1955.
    • (1955) Technical Note TN 3539
    • Woolston, D.S.1    Runyan, H.L.2    Byrdsong, T.A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.