A method by which modern and classical theory techniques may be integrated in a synergistic fashion and used in the design of practical flight control systems is presented. A general procedure is developed, and several illustrative examples are included. Emphasis is placed not only on the synthesis of the design, but on the assessment of the results as well.


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    Title :

    Practical optimal flight control system design for helicopter aircraft. Volume 1: Technical Report


    Contributors:
    Hofmann, L. G. (author) / Riedel, S. A. (author) / Mcruer, D. (author)

    Publication date :

    1980-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English