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 develpoed, 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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    Titel :

    Practical Optimal Flight Control System Design for Helicopter Aircraft. Volume 1: Technical Report


    Beteiligte:
    L. G. Hofmann (Autor:in) / S. A. Riedel (Autor:in) / D. Mcruer (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    273 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch