The design of the high-precision attitude control system of the LEO

Ting Song; Tianwei Hao; Yongjiang Xia; Xueqin Chen

doi:10.1109/ISSCAA.2010.5633147

The design of the high-precision attitude control system of the LEO

Ting Song^*
, Tianwei Hao
, Yongjiang Xia
, Xueqin Chen

^*Corresponding author for this work

School of Astronautics

Shanghai Aerospace Control Engineering Institute

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

1 Scopus citations

Abstract

This paper designs the H_∞ state feedback controller of the low-orbit satellite to achieve the high precision attitude control. Based on the analysis of the system uncertainty and environment disturbance of the low-orbit satellite, H_∞ method is adopted and the LMI arithmetic is used to make the computation easier. The results of the system simulation prove that the algorithm is useful and can make the attitude control system achieve the high precision requirements.

Original language	English
Title of host publication	ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
Pages	339-342
Number of pages	4
DOIs	https://doi.org/10.1109/ISSCAA.2010.5633147
State	Published - 2010
Event	3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 - Harbin, China Duration: 8 Jun 2010 → 10 Jun 2010

Publication series

Name	ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

Conference

Conference	3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Country/Territory	China
City	Harbin
Period	8/06/10 → 10/06/10

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10.1109/ISSCAA.2010.5633147

Cite this

Song, T., Hao, T., Xia, Y., & Chen, X. (2010). The design of the high-precision attitude control system of the LEO. In ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (pp. 339-342). Article 5633147 (ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics). https://doi.org/10.1109/ISSCAA.2010.5633147

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title = "The design of the high-precision attitude control system of the LEO",

abstract = "This paper designs the H∞ state feedback controller of the low-orbit satellite to achieve the high precision attitude control. Based on the analysis of the system uncertainty and environment disturbance of the low-orbit satellite, H∞ method is adopted and the LMI arithmetic is used to make the computation easier. The results of the system simulation prove that the algorithm is useful and can make the attitude control system achieve the high precision requirements.",

author = "Ting Song and Tianwei Hao and Yongjiang Xia and Xueqin Chen",

year = "2010",

doi = "10.1109/ISSCAA.2010.5633147",

language = "英语",

isbn = "9781424460441",

series = "ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics",

pages = "339--342",

booktitle = "ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics",

note = "3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 ; Conference date: 08-06-2010 Through 10-06-2010",

}

Song, T, Hao, T, Xia, Y & Chen, X 2010, The design of the high-precision attitude control system of the LEO. in ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics., 5633147, ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, pp. 339-342, 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010, Harbin, China, 8/06/10. https://doi.org/10.1109/ISSCAA.2010.5633147

The design of the high-precision attitude control system of the LEO. / Song, Ting; Hao, Tianwei; Xia, Yongjiang et al.
ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. 2010. p. 339-342 5633147 (ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics).

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

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AU - Song, Ting

AU - Hao, Tianwei

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N2 - This paper designs the H∞ state feedback controller of the low-orbit satellite to achieve the high precision attitude control. Based on the analysis of the system uncertainty and environment disturbance of the low-orbit satellite, H∞ method is adopted and the LMI arithmetic is used to make the computation easier. The results of the system simulation prove that the algorithm is useful and can make the attitude control system achieve the high precision requirements.

AB - This paper designs the H∞ state feedback controller of the low-orbit satellite to achieve the high precision attitude control. Based on the analysis of the system uncertainty and environment disturbance of the low-orbit satellite, H∞ method is adopted and the LMI arithmetic is used to make the computation easier. The results of the system simulation prove that the algorithm is useful and can make the attitude control system achieve the high precision requirements.

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M3 - 会议稿件

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SN - 9781424460441

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BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics

T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010

Y2 - 8 June 2010 through 10 June 2010

ER -

The design of the high-precision attitude control system of the LEO

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