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    Titel :

    MANEUVER LOAD ALLEVIATION OF VERY FLEXIBLE AIRCRAFT VIA NONLINEAR DECOUPLING CONTROL


    Beteiligte:

    Kongress:

    AIAA SciTech Forum and Exposition ; 2021 ; Online



    Erscheinungsdatum :

    2021


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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