Honeywell has designed a digital self-adaptive flight control system for flight test in the VALT Research Aircraft (a modified CH-47). The final design resulted from a comparison of two different adaptive concepts: one based on explicit parameter estimates from a real-time maximum likelihood estimation algorithm and the other based on an implicit model reference adaptive system. The two designs are compared on the basis of performance and complexity.


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    Title :

    Digital adaptive control laws for VTOL aircraft


    Contributors:
    Hartmann, G. L. (author) / Stein, G. (author)

    Conference:

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


    Publication date :

    1979-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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