Periodic time-varying controller design of a satellite using magnetorquers

Guangfu Ma; Chuanjiang Li; Zhihong Yang

Periodic time-varying controller design of a satellite using magnetorquers

Guangfu Ma^*
, Chuanjiang Li
, Zhihong Yang

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Contribution to conference › Paper › peer-review

Abstract

Satellite attitude control that utilizing momentum bias and magnetic control is a class of complicated linear quasi-periodic system. According to asymptotical stability theorem of linear time-varying system, a new approach to magnetic controller design is presented in this paper. Simulation result is given. It is shown that high pointing accuracy of roll/yaw is achieved.

Original language	English
Pages	5454-5457
Number of pages	4
State	Published - 2004
Event	WCICA 2004 - Fifth World Congress on Intelligent Control and Automation, Conference Proceedings - Hangzhou, China Duration: 15 Jun 2004 → 19 Jun 2004

Conference

Conference	WCICA 2004 - Fifth World Congress on Intelligent Control and Automation, Conference Proceedings
Country/Territory	China
City	Hangzhou
Period	15/06/04 → 19/06/04

Keywords

Attitude control system
Linear quasi-periodic system
Magnetic control
Momentum bias

Cite this

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title = "Periodic time-varying controller design of a satellite using magnetorquers",

abstract = "Satellite attitude control that utilizing momentum bias and magnetic control is a class of complicated linear quasi-periodic system. According to asymptotical stability theorem of linear time-varying system, a new approach to magnetic controller design is presented in this paper. Simulation result is given. It is shown that high pointing accuracy of roll/yaw is achieved.",

keywords = "Attitude control system, Linear quasi-periodic system, Magnetic control, Momentum bias",

author = "Guangfu Ma and Chuanjiang Li and Zhihong Yang",

year = "2004",

language = "英语",

pages = "5454--5457",

note = "WCICA 2004 - Fifth World Congress on Intelligent Control and Automation, Conference Proceedings ; Conference date: 15-06-2004 Through 19-06-2004",

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TY - CONF

T1 - Periodic time-varying controller design of a satellite using magnetorquers

AU - Ma, Guangfu

AU - Li, Chuanjiang

AU - Yang, Zhihong

PY - 2004

Y1 - 2004

N2 - Satellite attitude control that utilizing momentum bias and magnetic control is a class of complicated linear quasi-periodic system. According to asymptotical stability theorem of linear time-varying system, a new approach to magnetic controller design is presented in this paper. Simulation result is given. It is shown that high pointing accuracy of roll/yaw is achieved.

AB - Satellite attitude control that utilizing momentum bias and magnetic control is a class of complicated linear quasi-periodic system. According to asymptotical stability theorem of linear time-varying system, a new approach to magnetic controller design is presented in this paper. Simulation result is given. It is shown that high pointing accuracy of roll/yaw is achieved.

KW - Attitude control system

KW - Linear quasi-periodic system

KW - Magnetic control

KW - Momentum bias

UR - https://www.scopus.com/pages/publications/4444325915

M3 - 论文

AN - SCOPUS:4444325915

SP - 5454

EP - 5457

T2 - WCICA 2004 - Fifth World Congress on Intelligent Control and Automation, Conference Proceedings

Y2 - 15 June 2004 through 19 June 2004

ER -

Periodic time-varying controller design of a satellite using magnetorquers

Abstract

Conference

Keywords

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Cite this