Flexible satellite attitude control via adaptive fuzzy linearization

Ping Guan; Xiang Dong Liu; Jia Bin Chen; Xiao He Liu

Flexible satellite attitude control via adaptive fuzzy linearization

Ping Guan^*
, Xiang Dong Liu
, Jia Bin Chen
, Xiao He Liu

^*此作品的通讯作者

自动化学院

Beijing Institute of Technology
Beijing Institute of Machinery

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

The adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The control method is then applied to the attitude maneuver control of the flexible satellite. The basic control structure is given. The rules of the controller parameter selection, which guarantee the attitude stabilization of the satellite with parameter uncertainties, have been analyzed. Simulation results show that the precise attitude control is accomplished in spite of the uncertainty in the system.

源语言	英语
页（从-至）	140-144
页数	5
期刊	Journal of Beijing Institute of Technology (English Edition)
卷	14
期	2
出版状态	已出版 - 6月 2005

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引用此

@article{f95921cc4abc43749e96ad26d23fbe76,

title = "Flexible satellite attitude control via adaptive fuzzy linearization",

abstract = "The adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The control method is then applied to the attitude maneuver control of the flexible satellite. The basic control structure is given. The rules of the controller parameter selection, which guarantee the attitude stabilization of the satellite with parameter uncertainties, have been analyzed. Simulation results show that the precise attitude control is accomplished in spite of the uncertainty in the system.",

keywords = "Adaptive fuzzy control, Attitude maneuver, Flexible satellite, Input-output linearization",

author = "Ping Guan and Liu, \{Xiang Dong\} and Chen, \{Jia Bin\} and Liu, \{Xiao He\}",

year = "2005",

month = jun,

language = "English",

volume = "14",

pages = "140--144",

journal = "Journal of Beijing Institute of Technology (English Edition)",

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publisher = "Beijing Institute of Technology",

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T1 - Flexible satellite attitude control via adaptive fuzzy linearization

AU - Guan, Ping

AU - Liu, Xiang Dong

AU - Chen, Jia Bin

AU - Liu, Xiao He

PY - 2005/6

Y1 - 2005/6

N2 - The adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The control method is then applied to the attitude maneuver control of the flexible satellite. The basic control structure is given. The rules of the controller parameter selection, which guarantee the attitude stabilization of the satellite with parameter uncertainties, have been analyzed. Simulation results show that the precise attitude control is accomplished in spite of the uncertainty in the system.

AB - The adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The control method is then applied to the attitude maneuver control of the flexible satellite. The basic control structure is given. The rules of the controller parameter selection, which guarantee the attitude stabilization of the satellite with parameter uncertainties, have been analyzed. Simulation results show that the precise attitude control is accomplished in spite of the uncertainty in the system.

KW - Adaptive fuzzy control

KW - Attitude maneuver

KW - Flexible satellite

KW - Input-output linearization

UR - https://www.scopus.com/pages/publications/22844447870

M3 - Article

AN - SCOPUS:22844447870

SN - 1004-0579

VL - 14

SP - 140

EP - 144

JO - Journal of Beijing Institute of Technology (English Edition)

JF - Journal of Beijing Institute of Technology (English Edition)

IS - 2

ER -

Flexible satellite attitude control via adaptive fuzzy linearization

摘要

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