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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    Title :

    Swing control of helicopter sling load by using command smoothing technique


    Contributors:
    Wang, Haining (author) / Huang, Jie (author)


    Publication date :

    2014-07-01


    Size :

    379046 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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