This paper develops a new design method for aircraft control system, which is called 'optimal variable craft control system.' This system can make the aircraft keep good control performance in different space areas; it compensates the deficiency of the classical design of PID. Furthermore, because of that it can be realized easily in engineering, so it is a more practical and effective design method. Digital simulation shows that the result is good.


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    Titel :

    Aircraft Optimal Variable Structure Control System


    Beteiligte:
    A. Sun (Autor:in) / C. Shen (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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