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.


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    Titel :

    A method of automatically stabilizing helicopter sling loads


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

    Erscheinungsdatum :

    1974-07-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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