The research reported upon in this paper describes an effective method of gust alleviation using direct measurements of atmospheric turbulence to drive the aircraft control surfaces in a way that attempts to directly counter or cancel those forces and moments produced on the aircraft by gusts. The method yields a feedforward or open loop control law, simple to mechanize and relatively insensitive to changes in flight condition. When applied directly, the resulting control law effectively gust-alleviates in the low frequency phugoid and short period range but has a tendency to amplify structural mode vehicle motions due to the phase lag of the actuators. A method of design based upon the use of a diagonal or Jordan form of the equations of motion enables the designer to avoid this problem of structural mode excitation.


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    Titel :

    Gust alleviation using direct turbulence measurements


    Beteiligte:
    Rynaski, E. G. (Autor:in) / Andrisani, D., II (Autor:in) / Eulrich, B. J. (Autor:in)

    Kongress:

    Atmospheric Flight Mechanics Conference for Future Space Systems ; 1979 ; Boulder, CO


    Erscheinungsdatum :

    01.01.1979


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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