Motion-induced oscillations of helicopter sling load seriously degrade their effectiveness and safety. The modeling and dynamics of helicopter sling load are derived. A novel control scheme is designed for reducing the payload swing. Simulations of a large range of motions and various system parameters are used to analyze the dynamic behavior and the robustness of the control scheme. Experimental results obtained from a model helicopter sling load validate the simulated dynamic behavior and the effectiveness of the control scheme.


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    Titel :

    Swing control of helicopter sling load by using command smoothing technique


    Beteiligte:
    Wang, Haining (Autor:in) / Huang, Jie (Autor:in)


    Erscheinungsdatum :

    2014-07-01


    Format / Umfang :

    379046 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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