A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight Simulator

A compound fuzzy disturbance observer based on sliding modes is developed, and its application on flight simulator is presented. Fuzzy disturbance observer (FDO) is an effective method in nonlinear control. However, traditional FDO is confined to monitor dynamic disturbance, and the frequency bandwi...

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Main Authors: Yunjie Wu, Youmin Liu, Dapeng Tian
Format: Article
Language:English
Published: Hindawi Limited 2013-01-01
Series:Mathematical Problems in Engineering
Online Access:http://dx.doi.org/10.1155/2013/913538
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spelling doaj-cd18999115ae4777a4a8d01f2ec686882020-11-24T23:31:21ZengHindawi LimitedMathematical Problems in Engineering1024-123X1563-51472013-01-01201310.1155/2013/913538913538A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight SimulatorYunjie Wu0Youmin Liu1Dapeng Tian2School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaSchool of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaChangchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Science, Jilin 130033, ChinaA compound fuzzy disturbance observer based on sliding modes is developed, and its application on flight simulator is presented. Fuzzy disturbance observer (FDO) is an effective method in nonlinear control. However, traditional FDO is confined to monitor dynamic disturbance, and the frequency bandwidth of the system is restricted. Sliding mode control (SMC) compensates the high-frequency component of disturbance while it is limited by the chattering phenomenon. The proposed method uses the sliding mode technique to deal with the uncompensated dynamic equivalent disturbance. The switching gain of sliding mode control designed according to the error of disturbance estimation is a small value. Therefore, the proposal also helps to decrease the chattering. The validity of the proposal method is confirmed by experiments on flight simulator.http://dx.doi.org/10.1155/2013/913538
collection DOAJ
language English
format Article
sources DOAJ
author Yunjie Wu
Youmin Liu
Dapeng Tian
spellingShingle Yunjie Wu
Youmin Liu
Dapeng Tian
A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight Simulator
Mathematical Problems in Engineering
author_facet Yunjie Wu
Youmin Liu
Dapeng Tian
author_sort Yunjie Wu
title A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight Simulator
title_short A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight Simulator
title_full A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight Simulator
title_fullStr A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight Simulator
title_full_unstemmed A Compound Fuzzy Disturbance Observer Based on Sliding Modes and Its Application on Flight Simulator
title_sort compound fuzzy disturbance observer based on sliding modes and its application on flight simulator
publisher Hindawi Limited
series Mathematical Problems in Engineering
issn 1024-123X
1563-5147
publishDate 2013-01-01
description A compound fuzzy disturbance observer based on sliding modes is developed, and its application on flight simulator is presented. Fuzzy disturbance observer (FDO) is an effective method in nonlinear control. However, traditional FDO is confined to monitor dynamic disturbance, and the frequency bandwidth of the system is restricted. Sliding mode control (SMC) compensates the high-frequency component of disturbance while it is limited by the chattering phenomenon. The proposed method uses the sliding mode technique to deal with the uncompensated dynamic equivalent disturbance. The switching gain of sliding mode control designed according to the error of disturbance estimation is a small value. Therefore, the proposal also helps to decrease the chattering. The validity of the proposal method is confirmed by experiments on flight simulator.
url http://dx.doi.org/10.1155/2013/913538
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