In accordance with AGARD recommendations for handling qualities in hovering flight control power and control thrust requirements for aircraft gross weights between 1 and 100 tons are estimated using statistical data for moments of inertia; results are compared with analysis of aircraft motions following disturbances and control inputs and with maneuver capability; effects of damping, dead time, gust level, etc, are investigated and some control system design criteria are obtained.


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    Titel :

    Review of hovering control requirements for VTOL aircraft by flight dynamics analysis


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Dathe, H.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Effect of stabilization on VTOL aircraft in hovering flight

    Greif, R. K. / Fry, E. B. / Gerdes, R. M. et al. | NTRS | 1972



    Effect of Stabilization on VTOL Aircraft in Hovering Flight

    R. K. Greif / E. B. Fry / R. M. Gerdes et al. | NTIS | 1972


    A visual flight investigation of hovering and low-speed vtol control requirements

    Garren, J. F., Jr. / Kelly, J. R. / Reeder, J. P. | NTRS | 1965


    A visual flight investigation of hovering and low-speed VTOL control requirements

    Garren, John F. / Kelly, James R. / Reeder, John P. | TIBKAT | 1965