Energy equality based detumbling control for Pico-satellites

Fucheng Liu; Haifeng Zhu; Yong Liu; Qian Feng; Quan Pan

doi:10.1109/ChiCC.2014.6896725

Energy equality based detumbling control for Pico-satellites

Fucheng Liu, Haifeng Zhu, Yong Liu, Qian Feng, Quan Pan

School of Automation

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

Abstract

Pico-satellite, which quality is under 10Kg, is a popular research direction in space field. In this paper, because of the characteristics of the Pico-satellite's attitude determination and attitude control systems, which has no momentum wheel, long share time, constant magnetic moment, we put forward a new Pico-satellite attitude control algorithm named Energy equivalent damping control algorithm. This algorithm use the principle of Magnetic torque work equivalent with the B-dot algorithm, then the kinetic energy of the Pico-satellite decreases gradually and makes the system stable in the desired angular velocity. The algorithm has good engineering application background, and it can meet the requirement of Pico-satellite's low power consumption, low cost, light weight etc. A large number of simulation results show that this algorithm has good control precision and control convergence.

Original language	English
Title of host publication	Proceedings of the 33rd Chinese Control Conference, CCC 2014
Editors	Shengyuan Xu, Qianchuan Zhao
Publisher	IEEE Computer Society
Pages	776-781
Number of pages	6
ISBN (Electronic)	9789881563842
DOIs	https://doi.org/10.1109/ChiCC.2014.6896725
State	Published - 11 Sep 2014
Event	Proceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China Duration: 28 Jul 2014 → 30 Jul 2014

Publication series

Name	Proceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	Proceedings of the 33rd Chinese Control Conference, CCC 2014
Country/Territory	China
City	Nanjing
Period	28/07/14 → 30/07/14

Keywords

Active Magnetic Control
Energy Equivalent
Long Time-sharing control
Pico Satellite

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10.1109/ChiCC.2014.6896725

Cite this

@inproceedings{d15058dc79974c4d8deb8ddd1c1756bf,

title = "Energy equality based detumbling control for Pico-satellites",

abstract = "Pico-satellite, which quality is under 10Kg, is a popular research direction in space field. In this paper, because of the characteristics of the Pico-satellite's attitude determination and attitude control systems, which has no momentum wheel, long share time, constant magnetic moment, we put forward a new Pico-satellite attitude control algorithm named Energy equivalent damping control algorithm. This algorithm use the principle of Magnetic torque work equivalent with the B-dot algorithm, then the kinetic energy of the Pico-satellite decreases gradually and makes the system stable in the desired angular velocity. The algorithm has good engineering application background, and it can meet the requirement of Pico-satellite's low power consumption, low cost, light weight etc. A large number of simulation results show that this algorithm has good control precision and control convergence.",

keywords = "Active Magnetic Control, Energy Equivalent, Long Time-sharing control, Pico Satellite",

author = "Fucheng Liu and Haifeng Zhu and Yong Liu and Qian Feng and Quan Pan",

note = "Publisher Copyright: {\textcopyright} 2014 TCCT, CAA.; Proceedings of the 33rd Chinese Control Conference, CCC 2014 ; Conference date: 28-07-2014 Through 30-07-2014",

year = "2014",

month = sep,

day = "11",

doi = "10.1109/ChiCC.2014.6896725",

language = "英语",

series = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",

publisher = "IEEE Computer Society",

pages = "776--781",

editor = "Shengyuan Xu and Qianchuan Zhao",

booktitle = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",

}

Liu, F, Zhu, H, Liu, Y, Feng, Q & Pan, Q 2014, Energy equality based detumbling control for Pico-satellites. in S Xu & Q Zhao (eds), Proceedings of the 33rd Chinese Control Conference, CCC 2014., 6896725, Proceedings of the 33rd Chinese Control Conference, CCC 2014, IEEE Computer Society, pp. 776-781, Proceedings of the 33rd Chinese Control Conference, CCC 2014, Nanjing, China, 28/07/14. https://doi.org/10.1109/ChiCC.2014.6896725

Energy equality based detumbling control for Pico-satellites. / Liu, Fucheng; Zhu, Haifeng; Liu, Yong et al.
Proceedings of the 33rd Chinese Control Conference, CCC 2014. ed. / Shengyuan Xu; Qianchuan Zhao. IEEE Computer Society, 2014. p. 776-781 6896725 (Proceedings of the 33rd Chinese Control Conference, CCC 2014).

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

TY - GEN

T1 - Energy equality based detumbling control for Pico-satellites

AU - Liu, Fucheng

AU - Zhu, Haifeng

AU - Liu, Yong

AU - Feng, Qian

AU - Pan, Quan

PY - 2014/9/11

Y1 - 2014/9/11

N2 - Pico-satellite, which quality is under 10Kg, is a popular research direction in space field. In this paper, because of the characteristics of the Pico-satellite's attitude determination and attitude control systems, which has no momentum wheel, long share time, constant magnetic moment, we put forward a new Pico-satellite attitude control algorithm named Energy equivalent damping control algorithm. This algorithm use the principle of Magnetic torque work equivalent with the B-dot algorithm, then the kinetic energy of the Pico-satellite decreases gradually and makes the system stable in the desired angular velocity. The algorithm has good engineering application background, and it can meet the requirement of Pico-satellite's low power consumption, low cost, light weight etc. A large number of simulation results show that this algorithm has good control precision and control convergence.

AB - Pico-satellite, which quality is under 10Kg, is a popular research direction in space field. In this paper, because of the characteristics of the Pico-satellite's attitude determination and attitude control systems, which has no momentum wheel, long share time, constant magnetic moment, we put forward a new Pico-satellite attitude control algorithm named Energy equivalent damping control algorithm. This algorithm use the principle of Magnetic torque work equivalent with the B-dot algorithm, then the kinetic energy of the Pico-satellite decreases gradually and makes the system stable in the desired angular velocity. The algorithm has good engineering application background, and it can meet the requirement of Pico-satellite's low power consumption, low cost, light weight etc. A large number of simulation results show that this algorithm has good control precision and control convergence.

KW - Active Magnetic Control

KW - Energy Equivalent

KW - Long Time-sharing control

KW - Pico Satellite

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M3 - 会议稿件

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BT - Proceedings of the 33rd Chinese Control Conference, CCC 2014

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T2 - Proceedings of the 33rd Chinese Control Conference, CCC 2014

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ER -

Energy equality based detumbling control for Pico-satellites

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