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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    Title :

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




    Publication date :

    2021-10-01


    Size :

    359449 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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