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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    Title :

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


    Additional title:

    AGARD -- Report


    Contributors:
    Dathe, H.M. (author)

    Published in:

    Publication date :

    1963


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Effect of stabilization on VTOL aircraft in hovering flight

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


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    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