• DocumentCode
    2164500
  • Title

    Systems integration using evolutionary algorithms

  • Author

    Chipperfield, A.J. ; Fleming, P.J.

  • Author_Institution
    Sheffield Univ., UK
  • Volume
    1
  • fYear
    1996
  • fDate
    2-5 Sept. 1996
  • Firstpage
    705
  • Abstract
    This paper describes an approach to the systems integration problem using multiobjective genetic algorithms. An architecture for evolutionary systems integration is presented and the component parts discussed. An example of an aircraft gas turbine engine control system design problem is shown demonstrating aspects of the proposed architecture that allow many design objectives from different disciplines to be considered in parallel. Potential closed-loop control configurations are evaluated and compared against one another within an optimization framework. As a result of this analysis, it is shown how informed decisions may be made regarding the nature of the control employed, acceptable performance margins and elements of the engine design.
  • Keywords
    aerospace engines; aircraft control; closed loop systems; control system synthesis; gas turbines; genetic algorithms; performance index; aircraft; closed-loop control; evolutionary algorithms; gas turbine engine control system; multiobjective genetic algorithms; optimization; performance margins; systems integration;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Control '96, UKACC International Conference on (Conf. Publ. No. 427)
  • ISSN
    0537-9989
  • Print_ISBN
    0-85296-668-7
  • Type

    conf

  • DOI
    10.1049/cp:19960637
  • Filename
    651465