Robust control synthesis method for the satellite

Zhi Hong Yang; Guang Fu Ma; Chuan Jiang Li

Robust control synthesis method for the satellite

Zhi Hong Yang^*
, Guang Fu Ma
, Chuan Jiang Li

^*Corresponding author for this work

School of Astronautics, Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Scopus citations

Abstract

This paper presents a robust H^∞ control synthesis method for the satellite. The method is applied to the robust stabilization problem of the satellite in the face of parameter uncertainties and external disturbances. Observer-based robust H^∞ state feedback controller is adopted and the controller parameters can be derived from corresponding LMIs. A numerical simulation for a satellite's attitude control system shows that the closed loop system has both the satisfactory robust stability and the excellent ability of rejecting exogenous noise.

Original language	English
Title of host publication	2003 International Conference on Machine Learning and Cybernetics, ICMLC 2003
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	726-730
Number of pages	5
ISBN (Print)	0780378652, 9780780378650
State	Published - 2003
Externally published	Yes
Event	2nd International Conference on Machine Learning and Cybernetics, ICMLC 2003 - Xi'an, China Duration: 2 Nov 2003 → 5 Nov 2003

Publication series

Name	International Conference on Machine Learning and Cybernetics
Volume	2

Conference

Conference	2nd International Conference on Machine Learning and Cybernetics, ICMLC 2003
Country/Territory	China
City	Xi'an
Period	2/11/03 → 5/11/03

Keywords

H state feedback
LMI
Observer
Satellite attitude control

Cite this

@inproceedings{fb518e1f12204f15b5a9f49f6c50e7d9,

title = "Robust control synthesis method for the satellite",

abstract = "This paper presents a robust H∞ control synthesis method for the satellite. The method is applied to the robust stabilization problem of the satellite in the face of parameter uncertainties and external disturbances. Observer-based robust H∞ state feedback controller is adopted and the controller parameters can be derived from corresponding LMIs. A numerical simulation for a satellite's attitude control system shows that the closed loop system has both the satisfactory robust stability and the excellent ability of rejecting exogenous noise.",

keywords = "H state feedback, LMI, Observer, Satellite attitude control",

author = "Yang, \{Zhi Hong\} and Ma, \{Guang Fu\} and Li, \{Chuan Jiang\}",

year = "2003",

language = "英语",

isbn = "0780378652",

series = "International Conference on Machine Learning and Cybernetics",

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

pages = "726--730",

booktitle = "2003 International Conference on Machine Learning and Cybernetics, ICMLC 2003",

address = "美国",

note = "2nd International Conference on Machine Learning and Cybernetics, ICMLC 2003 ; Conference date: 02-11-2003 Through 05-11-2003",

}

Yang, ZH, Ma, GF & Li, CJ 2003, Robust control synthesis method for the satellite. in 2003 International Conference on Machine Learning and Cybernetics, ICMLC 2003. International Conference on Machine Learning and Cybernetics, vol. 2, Institute of Electrical and Electronics Engineers Inc., pp. 726-730, 2nd International Conference on Machine Learning and Cybernetics, ICMLC 2003, Xi'an, China, 2/11/03.

Robust control synthesis method for the satellite. / Yang, Zhi Hong; Ma, Guang Fu ; Li, Chuan Jiang.
2003 International Conference on Machine Learning and Cybernetics, ICMLC 2003. Institute of Electrical and Electronics Engineers Inc., 2003. p. 726-730 (International Conference on Machine Learning and Cybernetics; Vol. 2).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Robust control synthesis method for the satellite

AU - Yang, Zhi Hong

AU - Ma, Guang Fu

AU - Li, Chuan Jiang

PY - 2003

Y1 - 2003

N2 - This paper presents a robust H∞ control synthesis method for the satellite. The method is applied to the robust stabilization problem of the satellite in the face of parameter uncertainties and external disturbances. Observer-based robust H∞ state feedback controller is adopted and the controller parameters can be derived from corresponding LMIs. A numerical simulation for a satellite's attitude control system shows that the closed loop system has both the satisfactory robust stability and the excellent ability of rejecting exogenous noise.

AB - This paper presents a robust H∞ control synthesis method for the satellite. The method is applied to the robust stabilization problem of the satellite in the face of parameter uncertainties and external disturbances. Observer-based robust H∞ state feedback controller is adopted and the controller parameters can be derived from corresponding LMIs. A numerical simulation for a satellite's attitude control system shows that the closed loop system has both the satisfactory robust stability and the excellent ability of rejecting exogenous noise.

KW - H state feedback

KW - LMI

KW - Observer

KW - Satellite attitude control

UR - https://www.scopus.com/pages/publications/1542346784

M3 - 会议稿件

AN - SCOPUS:1542346784

SN - 0780378652

SN - 9780780378650

T3 - International Conference on Machine Learning and Cybernetics

SP - 726

EP - 730

BT - 2003 International Conference on Machine Learning and Cybernetics, ICMLC 2003

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2nd International Conference on Machine Learning and Cybernetics, ICMLC 2003

Y2 - 2 November 2003 through 5 November 2003

ER -

Robust control synthesis method for the satellite

Abstract

Publication series

Conference

Keywords

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