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Volumn 14, Issue 4, 2006, Pages 337-350

Inverse problem of aircraft structural parameter identification: Application of genetic algorithms compared with artificial neural networks

Author keywords

Aircraft structures; Finite elements; Genetic algorithms; Parameter estimation

Indexed keywords


EID: 33745607298     PISSN: 17415977     EISSN: 17415985     Source Type: Journal    
DOI: 10.1080/17415970600573338     Document Type: Conference Paper
Times cited : (3)

References (11)
  • 1
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    • The use of genetic algorithms in dynamic finite element model identification for aerospace structures
    • Reston, Virginia, USA
    • Dunn, S.A., 1996, The use of genetic algorithms in dynamic finite element model identification for aerospace structures, presented at the 20th Congress of the International Council of the Aeronautical Sciences, Reston, Virginia, USA.
    • (1996) 20th Congress of the International Council of the Aeronautical Sciences
    • Dunn, S.A.1
  • 3
    • 0026988817 scopus 로고
    • Genetic algorithms
    • Holland, J.H., 1992, Genetic algorithms. Scientific America, 267, 44-50.
    • (1992) Scientific America , vol.267 , pp. 44-50
    • Holland, J.H.1
  • 4
    • 0027640931 scopus 로고
    • Genetic algorithms: Principles of natural selection applied to computation
    • Forrest, S., 1993, Genetic algorithms: principles of natural selection applied to computation. Science, 261, 872-878.
    • (1993) Science , vol.261 , pp. 872-878
    • Forrest, S.1
  • 5
    • 0031098528 scopus 로고    scopus 로고
    • Modified genetic algorithm for the identification of aircraft structures
    • Dunn, S.A., 1997, Modified genetic algorithm for the identification of aircraft structures. Journal of Aircraft, 34(2), 251-253.
    • (1997) Journal of Aircraft , vol.34 , Issue.2 , pp. 251-253
    • Dunn, S.A.1
  • 6
    • 0343215968 scopus 로고    scopus 로고
    • Optimisation of the structural dynamic finite element model for a complete aircraft
    • Melbourne, Victoria, Australia, 13-18 September
    • Dunn, S.A., 1998. Optimisation of the structural dynamic finite element model for a complete aircraft, presented at the 21st Congress of the International Council of the Aeronautical Sciences, Melbourne, Victoria, Australia, 13-18 September.
    • (1998) 21st Congress of the International Council of the Aeronautical Sciences
    • Dunn, S.A.1
  • 7
    • 0031996259 scopus 로고    scopus 로고
    • The use of genetic algorithms and stochastic hill-climbing in dynamic finite element model identification
    • Dunn, S.A., 1998, The use of genetic algorithms and stochastic hill-climbing in dynamic finite element model identification. Computers & Structures, 66(4), 489-497.
    • (1998) Computers & Structures , vol.66 , Issue.4 , pp. 489-497
    • Dunn, S.A.1
  • 8
    • 0033336229 scopus 로고    scopus 로고
    • Technique for unique optimisation of dynamic finite element models
    • Dunn, S.A., 1999, Technique for unique optimisation of dynamic finite element models. Journal of Aircraft, 36(6), 919-925.
    • (1999) Journal of Aircraft , vol.36 , Issue.6 , pp. 919-925
    • Dunn, S.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.