Adaptive fuzzy attitude control of satellite based on linearization

P. Guan; X. J. Liu; F. Lara-Rosano; J. B. Chen

doi:10.23919/acc.2004.1386717

Adaptive fuzzy attitude control of satellite based on linearization

P. Guan^*, X. J. Liu, F. Lara-Rosano, J. B. Chen

^*Corresponding author for this work

School of Automation

Research output: Contribution to journal › Conference article › peer-review

5 Citations (Scopus)

Abstract

Input-output (I/O) linearization is a typical control method in the nonlinear multi-input multi-output (MIMO) system. In this paper, adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The proposed control method is applied to the attitude maneuver control of the flexible satellite, which is a complex nonlinear system. The basic control structure is presented. The selection of the controller parameter, which guarantee the attitude stabilization of the satellite with parameter uncertainties, has been analyzed. The adaptive fuzzy control compensates for the plant uncertainties to increase the robustness of the controller. Simulation results show that precise attitude control is accomplished in spite of the uncertainty in the system.

Original language	English
Pages (from-to)	1091-1096
Number of pages	6
Journal	Proceedings of the American Control Conference
Volume	2
DOIs	https://doi.org/10.23919/acc.2004.1386717
Publication status	Published - 2004
Event	Proceedings of the 2004 American Control Conference (AAC) - Boston, MA, United States Duration: 30 Jun 2004 → 2 Jul 2004

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title = "Adaptive fuzzy attitude control of satellite based on linearization",

abstract = "Input-output (I/O) linearization is a typical control method in the nonlinear multi-input multi-output (MIMO) system. In this paper, adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The proposed control method is applied to the attitude maneuver control of the flexible satellite, which is a complex nonlinear system. The basic control structure is presented. The selection of the controller parameter, which guarantee the attitude stabilization of the satellite with parameter uncertainties, has been analyzed. The adaptive fuzzy control compensates for the plant uncertainties to increase the robustness of the controller. Simulation results show that precise attitude control is accomplished in spite of the uncertainty in the system.",

author = "P. Guan and Liu, {X. J.} and F. Lara-Rosano and Chen, {J. B.}",

year = "2004",

doi = "10.23919/acc.2004.1386717",

language = "English",

volume = "2",

pages = "1091--1096",

journal = "Proceedings of the American Control Conference",

issn = "0743-1619",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

note = "Proceedings of the 2004 American Control Conference (AAC) ; Conference date: 30-06-2004 Through 02-07-2004",

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TY - JOUR

T1 - Adaptive fuzzy attitude control of satellite based on linearization

AU - Guan, P.

AU - Liu, X. J.

AU - Lara-Rosano, F.

AU - Chen, J. B.

PY - 2004

Y1 - 2004

N2 - Input-output (I/O) linearization is a typical control method in the nonlinear multi-input multi-output (MIMO) system. In this paper, adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The proposed control method is applied to the attitude maneuver control of the flexible satellite, which is a complex nonlinear system. The basic control structure is presented. The selection of the controller parameter, which guarantee the attitude stabilization of the satellite with parameter uncertainties, has been analyzed. The adaptive fuzzy control compensates for the plant uncertainties to increase the robustness of the controller. Simulation results show that precise attitude control is accomplished in spite of the uncertainty in the system.

AB - Input-output (I/O) linearization is a typical control method in the nonlinear multi-input multi-output (MIMO) system. In this paper, adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The proposed control method is applied to the attitude maneuver control of the flexible satellite, which is a complex nonlinear system. The basic control structure is presented. The selection of the controller parameter, which guarantee the attitude stabilization of the satellite with parameter uncertainties, has been analyzed. The adaptive fuzzy control compensates for the plant uncertainties to increase the robustness of the controller. Simulation results show that precise attitude control is accomplished in spite of the uncertainty in the system.

UR - http://www.scopus.com/inward/record.url?scp=8744312539&partnerID=8YFLogxK

U2 - 10.23919/acc.2004.1386717

DO - 10.23919/acc.2004.1386717

M3 - Conference article

AN - SCOPUS:8744312539

SN - 0743-1619

VL - 2

SP - 1091

EP - 1096

JO - Proceedings of the American Control Conference

JF - Proceedings of the American Control Conference

T2 - Proceedings of the 2004 American Control Conference (AAC)

Y2 - 30 June 2004 through 2 July 2004

ER -

Adaptive fuzzy attitude control of satellite based on linearization

Abstract

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