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Coupled Multiple Sliding-Mode Control for Robust Trajectory Tracking of Hovercraft with External Disturbances
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Publication Year
2018-05-01
Publisher
Institute of Electrical and Electronics Engineers Inc.
Citation
IEEE Transactions on Industrial Electronics, Vol.65, pp.4103-4113
Keyword
Coupled multiple siding-mode control (CMSMC)disturbance compensationdisturbance observerhovercraftrobust tracking control
Mesh Keyword
Disturbance compensationDisturbance observerMultiple sliding mode controlMultiple sliding surfacesNon holonomic constraintReference trajectoriesRobust tracking controlSiding mode controls
All Science Classification Codes (ASJC)
Control and Systems EngineeringElectrical and Electronic Engineering
Abstract
This paper proposes a robust coupled multiple sliding-mode control (CMSMC) method for tracking control of underactuated hovercraft systems with nonholonomic constraints and external disturbances. First, a friction model for the hovercraft, one of the main disturbance factors, is proposed by considering viscosity, and its validity is demonstrated through experiments. Second, a disturbance model in the actual hovercraft system is estimated using a least-square-estimation-based disturbance observer. Third, pseudo forces and pseudo heading direction angle for tracking control and disturbance compensation are proposed considering the characteristics of underactuated hovercraft systems. Fourth, coupled multiple sliding surfaces (CMSSs) are newly introduced in terms of the tracking errors between the pseudo control variables and actual ones, and then, a CMSMC-based controller is proposed so that the CMSSs converge to zero within finite time in the case of zero disturbance estimation errors. In this way, three posture variables of the hovercraft converge to reference ones using only two control inputs. Finally, stability analysis and verification by simulations and experiments show that both the pseudo control tracking errors and posture tracking errors are ultimately bounded and asymptotically converge to zero when disturbance estimation errors become zero.
ISSN
0278-0046
Language
eng
URI
https://dspace.ajou.ac.kr/dev/handle/2018.oak/30031
DOI
https://doi.org/10.1109/tie.2017.2774772
Fulltext

Type
Article
Funding
Manuscript received July 21, 2017; revised September 26, 2017; accepted November 1, 2017. Date of publication November 17, 2017; date of current version January 16, 2018. This work was supported by the Basic Science Research Program through the National Research Foundation of Korea (NRF) funded by the Ministry of Science, ICT, and Future Planning under Grant 2017R1A2B4009486. (Corresponding author: Dongkyoung Chwa.) S. Jeong is with the TmaxOS, Seongnam 13613, Korea (e-mail: jsc1214@ajou.ac.kr).
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Chwa, Dongkyoung Image
Chwa, Dongkyoung좌동경
Department of Electrical and Computer Engineering
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