Application of feedback linearization and continuous sliding mode control to a nonlinear helicopter model

Fuhai Duan; Changan He; Weiguo Zhang; Yi Shen

Application of feedback linearization and continuous sliding mode control to a nonlinear helicopter model

Fuhai Duan
, Changan He
, Weiguo Zhang
, Yi Shen

自动化学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

A continuous sliding mode control method based on feedback linearization is presented to realize the coupling control for a MIMO nonlinear system such as helicopter. A discontinuous sliding mode control can be changed into a continuous one by extending the nonlinear system. Thus the system robustness can be enhanced. The control system for the vertical flight mode of a helicopter is designed. Simulation results are in agreement with the theoretical analysis results and the system can track the given input.

源语言	英语
页（从-至）	378-381
页数	4
期刊	Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
卷	18
期	3
出版状态	已出版 - 8月 2000

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引用此

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title = "Application of feedback linearization and continuous sliding mode control to a nonlinear helicopter model",

abstract = "A continuous sliding mode control method based on feedback linearization is presented to realize the coupling control for a MIMO nonlinear system such as helicopter. A discontinuous sliding mode control can be changed into a continuous one by extending the nonlinear system. Thus the system robustness can be enhanced. The control system for the vertical flight mode of a helicopter is designed. Simulation results are in agreement with the theoretical analysis results and the system can track the given input.",

author = "Fuhai Duan and Changan He and Weiguo Zhang and Yi Shen",

year = "2000",

month = aug,

language = "英语",

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T1 - Application of feedback linearization and continuous sliding mode control to a nonlinear helicopter model

AU - Duan, Fuhai

AU - He, Changan

AU - Zhang, Weiguo

AU - Shen, Yi

PY - 2000/8

Y1 - 2000/8

N2 - A continuous sliding mode control method based on feedback linearization is presented to realize the coupling control for a MIMO nonlinear system such as helicopter. A discontinuous sliding mode control can be changed into a continuous one by extending the nonlinear system. Thus the system robustness can be enhanced. The control system for the vertical flight mode of a helicopter is designed. Simulation results are in agreement with the theoretical analysis results and the system can track the given input.

AB - A continuous sliding mode control method based on feedback linearization is presented to realize the coupling control for a MIMO nonlinear system such as helicopter. A discontinuous sliding mode control can be changed into a continuous one by extending the nonlinear system. Thus the system robustness can be enhanced. The control system for the vertical flight mode of a helicopter is designed. Simulation results are in agreement with the theoretical analysis results and the system can track the given input.

UR - https://www.scopus.com/pages/publications/0034240429

M3 - 文章

AN - SCOPUS:0034240429

SN - 1000-2758

VL - 18

SP - 378

EP - 381

JO - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

JF - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

IS - 3

ER -

Application of feedback linearization and continuous sliding mode control to a nonlinear helicopter model

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