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Cited 39 time in webofscience Cited 47 time in scopus
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Decentrailized formation flight control of quadcopters using robust feedback linearization

Authors
Mahmood, ArshadKim, Yoonsoo
Issue Date
Jan-2017
Publisher
PERGAMON-ELSEVIER SCIENCE LTD
Citation
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, v.354, no.2, pp 852 - 871
Pages
20
Indexed
SCIE
SCOPUS
Journal Title
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS
Volume
354
Number
2
Start Page
852
End Page
871
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/13979
DOI
10.1016/j.jfranklin.2016.10.039
ISSN
0016-0032
1879-2693
Abstract
In this paper, a decentralized formation flight control scheme is proposed for a group of quadcopters using classical feedback linearization. Existing works typically involve a complicated design of nonlinear formation control laws, whereas the present work uses a linear control law for under-actuated nonlinear quadcopters. This linear formation control approach has a strong merit, in that it can be easily designed in a way to clearly guarantee the stability and performance of the collective nonlinear system quantitatively in terms of classical measures (e.g. stability and robustness margins). In this paper, the feedback linearization can transform nonlinear quadcopters dynamics into simple fourth-order and double integrators, for which a linear formation control law is designed to achieve a desired formation and heading synchronization through local information exchanges only. Moreover, a sliding-mode compensator is designed for possible dynamics inversion errors during the feedback linearization. Simulation results including a comparison with a recently proposed control law are presented to demonstrate the practical usefulness of the present work. (C) 2016 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
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Kim, Yoon Soo
대학원 (기계항공우주공학부)
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