This document describes the design of a flight controller for the Research Civil Aircraft Model (RCAM), suing mu-synthesis. The controller has to satisfy design requirements formulated in a manual prepared by action group FM(AG08) of the GARTEUR organization ((FLi96b)). The resulting control system is implemented in a software environment, in which performance and robustness characteristics are evaluated by simulating a flight along a predefined trajectory.


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    Titel :

    Design of a Flight Controller for the Research Civil Aircraft Model (RCAM) Using mu-Synthesis


    Beteiligte:
    G. H. N. Looye (Autor:in) / S. Bennani (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    186 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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