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).
Erratum to “Fast Nonsingular Terminal Sliding Mode Flight Control for Multirotor Aerial Vehicles”
IEEE Transactions on Aerospace and Electronic Systems ; 57 , 5 ; 3549
2021-10-01
359449 byte
Article (Journal)
Electronic Resource
English
Nonsingular and Fast Terminal Sliding Mode Control Method
British Library Online Contents | 2009
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