Due to a production error, in the original article [1], Figs. 1, 2 and 3 were incorrectly published. We apologize for this error. The correct figures, with their corresponding captions, are shown below: Fig. 1. Schematic representation of MAVs with fixed single (a) or double (b) rotors. Fig. 2. Hierarchical flight control architecture for MAVs with fixed rotors. PC: position controller; AC: attitude controller; CA 1, CA 2: control allocators. Fig. 3. Rotational control errors along the time (above) and in the phase plane (below).


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    Titel :

    Erratum to “Fast Nonsingular Terminal Sliding Mode Flight Control for Multirotor Aerial Vehicles”


    Beteiligte:


    Erscheinungsdatum :

    01.10.2021


    Format / Umfang :

    359449 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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