This report documents the revisions made to a mathematical model of a single main rotor helicopter. These revisions were necessary to model the UH-60 helicopter accurately. The major modifications to the model include fuselage aerodynamic force and moment equations that are specific to the UH-60, a canted tail rotor, a horizontal stabilator with variable incidence, and a pitch bias actuator (PBA). In addition, the model requires a full set of parameters which describe the helicopter configuration and its physical characteristics.


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    Titel :

    Mathematical model of the UH-60 helicopter


    Weitere Titelangaben:

    Mathematisches Modell des UH-60-Hubschraubers


    Beteiligte:
    Hilbert, K.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1984


    Format / Umfang :

    45 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




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