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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    Title :

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


    Contributors:
    G. H. N. Looye (author) / S. Bennani (author)

    Publication date :

    1996


    Size :

    186 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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