An analytical study was performed to define a Gust Alleviation System on a preliminary configuration of a commuter airplane. The analysis takes into account the influence of elasticity of the airplane, unsteady aerodynamic effects, mechanical nonlinearities such as backlash deadzone and control surface rate and deflection limitations. A relatively simple model shows that ride comfort can be improved by at least 50%.


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    Titel :

    Gust Alleviation on a Transport Airplane


    Beteiligte:
    J. Becker (Autor:in) / F. Weiss (Autor:in) / E. Cavatorta (Autor:in) / C. Caldarelli (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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