Three dimensional attitude control of an underactuated satellite with thrusters

研究成果: ジャーナルへの寄稿記事

2 引用 (Scopus)

抄録

This paper deals with the three-dimensional attitude control of an underactuated satellite equipped with thrusters whose force directions are fixed to the satellite. First, the necessary number of thrusters for the satellite's attitude control is discussed utilizing the Minkowski-Farkas theorem. Then, using the wz parameters for a satellite's attitude expression, this paper proposes a non holonomic attitude controller which is effective for any satellite regardless of its moment of inertia. Numerical simulation demonstrates the effectiveness of the proposed controller. Furthermore, the efficiency of the controller for different thruster positions is also discussed.

元の言語英語
ページ(範囲)892-899
ページ数8
ジャーナルInternational Journal of Automation Technology
5
発行部数6
DOI
出版物ステータス出版済み - 1 1 2011

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Attitude control
Satellites
Controllers
Computer simulation

All Science Journal Classification (ASJC) codes

  • Mechanical Engineering
  • Industrial and Manufacturing Engineering

これを引用

Three dimensional attitude control of an underactuated satellite with thrusters. / Yoshimura, Yasuhiro; Matsuno, Takashi; Hokamoto, Shinji.

:: International Journal of Automation Technology, 巻 5, 番号 6, 01.01.2011, p. 892-899.

研究成果: ジャーナルへの寄稿記事

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