The exact nonlinear equations of motion are derived for a helicopter with an external load suspended by fore and aft, rigid-link cables. Lagrange's form of D'Alembert's principle is used. Ten degrees of freedom are necessary to represent the motion of this system in an inertial reference frame: six for the helicopter relative to inertial space and four for the load relative to the helicopter.


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    Titel :

    Lagrange-d'Alembert Formulation of the Equations of Motion of a Helicopter Carrying an Externally Suspended Load


    Beteiligte:
    J. M. Weber (Autor:in) / R. K. Greif (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    64 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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