Detailed Information

Cited 21 time in webofscience Cited 23 time in scopus
Metadata Downloads

Finite-time disturbance observer-based modified super-twisting algorithm for systems with mismatched disturbances: Application to fixed-wing UAVs under wind disturbancesopen access

Authors
Ngo Phong NguyenOh, HyondongKim, YoonsooMoon, JunYang, JunChen, Wen-Hua
Issue Date
Oct-2021
Publisher
John Wiley & Sons Inc.
Keywords
finite-time disturbance observer; fixed-wing UAVs; matched and mismatched disturbances; modified super-twisting algorithm; path following control
Citation
International Journal of Robust and Nonlinear Control, v.31, no.15, pp 7317 - 7343
Pages
27
Indexed
SCIE
SCOPUS
Journal Title
International Journal of Robust and Nonlinear Control
Volume
31
Number
15
Start Page
7317
End Page
7343
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/3221
DOI
10.1002/rnc.5678
ISSN
1049-8923
1099-1239
Abstract
This article proposes a finite-time disturbance observer-based modified super-twisting algorithm (FDO-STA) for disturbed high-order integrator-chain systems under matched and mismatched disturbances. We first design a finite-time observer for disturbance estimation, in which we show the finite-time convergence of disturbance estimation errors to zero. Second, by employing the estimates of disturbances and their derivatives, a new dynamic sliding surface is derived, which ensures the finite-time convergence of the controlled output to zero in the sliding phase. Then, based on the estimates of disturbances and their derivatives, the designed sliding surface, and a modified super-twisting algorithm, we develop the FDO-STA, which guarantees the finite-time convergence of the sliding variable to zero in the reaching phase. Rigorous analysis is provided to show the finite-time stability of the overall closed-loop system under the proposed control scheme. We finally apply the proposed FDO-STA framework to the path following control for fixed-wing UAVs under wind disturbances. Various simulation results are provided to show the effectiveness of the proposed controller, compared with the existing control approaches.
Files in This Item
There are no files associated with this item.
Appears in
Collections
공학계열 > 기계항공우주공학부 > Journal Articles

qrcode

Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.

Related Researcher

Researcher Kim, Yoon Soo photo

Kim, Yoon Soo
대학원 (기계항공우주공학부)
Read more

Altmetrics

Total Views & Downloads

BROWSE