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    Titel :

    CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H□‡ STRUCTURE WITH GWO


    Beteiligte:
    Deveerasetty, K. (Autor:in) / Oka, K. (Autor:in) / Harada, A. (Autor:in)

    Kongress:

    33rd International Council of the Aeronautical Sciences congress, ICAS



    Erscheinungsdatum :

    01.01.2022


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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