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

    Kongress:

    AIAA Guidance, Navigation, and Control Conference and Exhibit ; 2007 ; Hilton Head, SC, United States


    Erscheinungsdatum :

    2007-08-20


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Investigation of hovering control of VTOL transport

    Pfaff, K. | Engineering Index Backfile | 1964



    Stability and control of VTOL capable airships in hovering flight

    Curtiss, H. C., Jr. / Sumantran, V. | NTRS | 1985


    Hovering and low speed controllability of VTOL aircraft

    Crim, A.D. | Engineering Index Backfile | 1959


    Stability and control of VTOL capable airships in hovering flight

    CURTISS, H. C. / SUMANTRAN, V. | AIAA | 1985