Attitude stabilization of averaging magnetic torque

Huang Lin; Jing Wuxing

Attitude stabilization of averaging magnetic torque

Huang Lin^*
, Jing Wuxing

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

4 Scopus citations

Abstract

The stability problems of two magnetic control systems are discussed. One uses a three-axis magnetic actuator only; the other includes an additional momentum-biased wheel. The so-called orbit-averaged magnetic controllers, derived from the orbit-averaged magnetic field, show an ability to ensure the global attitude stabilization. This is supported theoretically by the averaging method and Lyapunov theories, and also illustrated by the simulations executed for orbits of different inclinations. The results show that the second system can achieve considerably high steady-state control accuracy in all cases.

Original language	English
Title of host publication	1st International Symposium on Systems and Control in Aerospace and Astronautics
Pages	627-632
Number of pages	6
State	Published - 2006
Event	1st International Symposium on Systems and Control in Aerospace and Astronautics - Harbin, China Duration: 19 Jan 2006 → 21 Jan 2006

Publication series

Name	1st International Symposium on Systems and Control in Aerospace and Astronautics
Volume	2006

Conference

Conference	1st International Symposium on Systems and Control in Aerospace and Astronautics
Country/Territory	China
City	Harbin
Period	19/01/06 → 21/01/06

Cite this

@inproceedings{172fe2c72f3641a1bd2f07cdf94ec10b,

title = "Attitude stabilization of averaging magnetic torque",

abstract = "The stability problems of two magnetic control systems are discussed. One uses a three-axis magnetic actuator only; the other includes an additional momentum-biased wheel. The so-called orbit-averaged magnetic controllers, derived from the orbit-averaged magnetic field, show an ability to ensure the global attitude stabilization. This is supported theoretically by the averaging method and Lyapunov theories, and also illustrated by the simulations executed for orbits of different inclinations. The results show that the second system can achieve considerably high steady-state control accuracy in all cases.",

author = "Huang Lin and Jing Wuxing",

year = "2006",

language = "英语",

isbn = "0780393953",

series = "1st International Symposium on Systems and Control in Aerospace and Astronautics",

pages = "627--632",

booktitle = "1st International Symposium on Systems and Control in Aerospace and Astronautics",

note = "1st International Symposium on Systems and Control in Aerospace and Astronautics ; Conference date: 19-01-2006 Through 21-01-2006",

}

Lin, H & Wuxing, J 2006, Attitude stabilization of averaging magnetic torque. in 1st International Symposium on Systems and Control in Aerospace and Astronautics., 1627415, 1st International Symposium on Systems and Control in Aerospace and Astronautics, vol. 2006, pp. 627-632, 1st International Symposium on Systems and Control in Aerospace and Astronautics, Harbin, China, 19/01/06.

Attitude stabilization of averaging magnetic torque. / Lin, Huang; Wuxing, Jing.
1st International Symposium on Systems and Control in Aerospace and Astronautics. 2006. p. 627-632 1627415 (1st International Symposium on Systems and Control in Aerospace and Astronautics; Vol. 2006).

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

TY - GEN

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AU - Lin, Huang

AU - Wuxing, Jing

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N2 - The stability problems of two magnetic control systems are discussed. One uses a three-axis magnetic actuator only; the other includes an additional momentum-biased wheel. The so-called orbit-averaged magnetic controllers, derived from the orbit-averaged magnetic field, show an ability to ensure the global attitude stabilization. This is supported theoretically by the averaging method and Lyapunov theories, and also illustrated by the simulations executed for orbits of different inclinations. The results show that the second system can achieve considerably high steady-state control accuracy in all cases.

AB - The stability problems of two magnetic control systems are discussed. One uses a three-axis magnetic actuator only; the other includes an additional momentum-biased wheel. The so-called orbit-averaged magnetic controllers, derived from the orbit-averaged magnetic field, show an ability to ensure the global attitude stabilization. This is supported theoretically by the averaging method and Lyapunov theories, and also illustrated by the simulations executed for orbits of different inclinations. The results show that the second system can achieve considerably high steady-state control accuracy in all cases.

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M3 - 会议稿件

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SN - 0780393953

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T3 - 1st International Symposium on Systems and Control in Aerospace and Astronautics

SP - 627

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BT - 1st International Symposium on Systems and Control in Aerospace and Astronautics

T2 - 1st International Symposium on Systems and Control in Aerospace and Astronautics

Y2 - 19 January 2006 through 21 January 2006

ER -

Attitude stabilization of averaging magnetic torque

Abstract

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