The design of an aircraft lateral control system, subject to several performance criteria and constraints, is considered. While in the previous studies of the same model a single criterion optimization, with other performance requirements expressed as constraints, has been pursued, the current approach involves a multiple criteria optimization. In particular, a Pareto optimal solution is sought.


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    Titel :

    A multiple objective optimization approach to aircraft control systems design


    Beteiligte:
    Tabak, D. (Autor:in) / Schy, A. A. (Autor:in) / Johnson, K. G. (Autor:in) / Giesy, D. P. (Autor:in)

    Kongress:

    1978 Conference on Decision and Control ; 1979 ; San Diego, CA


    Erscheinungsdatum :

    1979-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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