Results of efforts to develop automatic control design procedures for restructurable aircraft control systems is presented. The restructurable aircraft control problem involves designing a fault tolerance control system which can accomodate a wide variety of unanticipated aircraft failure. Under NASA sponsorship, many of the technologies which make such a system possible were developed and tested. Future work will focus on developing a methodology for integrating these technologies and demonstration of a complete system.


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    Titel :

    Initial Design and Evaluation of Automatic Restructurable Flight Control System Concepts


    Beteiligte:
    J. L. Weiss (Autor:in) / D. P. Looze (Autor:in) / J. S. Eterno (Autor:in) / D. B. Grunberg (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    163 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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