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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    Title :

    Initial design and evaluation of automatic restructurable flight control system concepts


    Contributors:

    Publication date :

    1986-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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