The "nested" structure of the control system for the X33 vehicle in launch mode is developed. Employing backstopping concepts, the outer loop (guidance) and the Inner loop (rates) continuous sliding mode controllers are designed. Simulations of the 3-DOF model of the X33 launch vehicle showed an accurate, robust, de-coupled tracking performance.


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    Titel :

    Sliding Mode Control of the X-33 Vehicle in Launch Mode


    Beteiligte:
    Shtessel, Yuri (Autor:in) / Jackson, Mark (Autor:in) / Hall, Charles (Autor:in) / Krupp, Don (Autor:in) / Hendrix, N. Douglas (Autor:in)

    Erscheinungsdatum :

    01.01.1998


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





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