Gust alleviation concepts were studied numerically on a Boeing 707 aircraft with autopilot. Stochastic gust processes were studied in the frequency domain. The calculations show that the best solution is the control of the pitch position and the pitch velocity by using the autopilot mode pitch-hold. It is shown that additional control systems (e.g. transverse control) can substantially reduce disturbance. The influence of aircraft elasticity can only be assessed in a very simplified way. Deformations of airfoils and effects on stationary aerodynamics are determined.


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    Titel :

    Gust Alleviation Boenabminderung


    Beteiligte:
    G. Bruening (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    167 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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