The effect of geometric and aerodynamic characteristics on the stability of the lateral degrees of freedom of a typical helicopter sling load is examined. The feasibility of stabilizing the suspended load by controllable fins was also studied. Linear control theory was applied to the design of a simple control law that stabilized the load over a wide range of helicopter airspeeds. (Author)


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    Titel :

    A Method of Automatically Stabilizing Helicopter Sling Loads


    Beteiligte:
    J. Gera (Autor:in) / S. W. Farmer (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    42 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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