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    Titel :

    Computing the Stability Limits of Pole-Zero Actuator Dynamics on Adaptive Control Laws for Aerospace Applications (AIAA 2018-0844)


    Beteiligte:

    Kongress:

    Guidance, navigation and control (Conference)



    Erscheinungsdatum :

    01.01.2018


    Format / Umfang :

    15 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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