Factors influencing magnitude of hover control power, and methods of scanning control effectiveness and specifying control criteria are discussed; it is mathematically shown that amount of simultaneous roll and pitch acceleration establishes location of axis of rotation and magnitude of resulting acceleration about axis; optimum distance from aircraft center of gravity for various control system lift device arrangements is analyzed and effects of aircraft moment of inertia and control response lag are discussed.


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    Titel :

    Some fundamentals for efficient VTOL aircraft hover control


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Hill, T.G. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Hover Control Tests on Flying Test Bed for VTOL Aircraft

    N. Takizawa / H. Fujieda / K. Ono et al. | NTIS | 1975


    Analysis of spread multi-jet VTOL aircraft in hover

    Albang, L. F. / Roberts, A. S. | NTRS | 1974


    Synthesis of hover autopilots for rotary-wing VTOL aircraft

    Hall, W. E. / Bryson, A. E., Jr. | NTRS | 1972


    Analysis of Spread Multi-Jet VTOL Aircraft in Hover

    L. F. Albang / A. S. Roberts | NTIS | 1974


    On gyroscopic inherent stability of VTOL aircraft near hover condition

    Vrana, J.C. | Engineering Index Backfile | 1963