This paper describes how Control Moment Gyroscopes (CMGs) can be used for stability augmentation to a thrust vectoring system for a generic Vertical Take-Off and Landing platform. The response characteristics of the platform which uses only thrust vectoring and a second configuration which includes a single-gimbal CMG array are simulated and compared for hovering flight while subject to severe air turbulence. Simulation results demonstrate the effectiveness of a CMG array in its ability to significantly reduce the agility requirement on the thrust vectoring system. Albeit simplifying physical assumptions on a generic CMG configuration, the numerical results also suggest that reasonably sized CMGs will likely be sufficient for a small hovering vehicle.


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    Titel :

    CMG-Augmented Control of a Hovering VTOL Platform


    Beteiligte:
    K. B. Lim (Autor:in) / D. D. Moerder (Autor:in)

    Erscheinungsdatum :

    2007


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    CMG-Augmented Control of a Hovering VTOL Platform

    Lim, K. B. / Moerder, D. D. | NTRS | 2007


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