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    Initial design and evaluation of automatic restructurable flight control system concepts

    Initial design and evaluation of automatic restructurable flight control system concepts


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

    1986-06-01

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Aircraft Stability And Control

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