Position and attitude control of an underactuated satellite with constant thrust

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

6 引用 (Scopus)

抜粋

This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.

元の言語英語
ホスト出版物のタイトルAIAA Guidance, Navigation, and Control Conference 2011
出版者American Institute of Aeronautics and Astronautics Inc.
ISBN(印刷物)9781600869525
DOI
出版物ステータス出版済み - 1 1 2011
イベントAIAA Guidance, Navigation and Control Conference 2011 - Portland, OR, 米国
継続期間: 8 8 20118 11 2011

出版物シリーズ

名前AIAA Guidance, Navigation, and Control Conference 2011

その他

その他AIAA Guidance, Navigation and Control Conference 2011
米国
Portland, OR
期間8/8/118/11/11

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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  • これを引用

    Yoshimura, Y., Matsuno, T., & Hokamoto, S. (2011). Position and attitude control of an underactuated satellite with constant thrust. : AIAA Guidance, Navigation, and Control Conference 2011 (AIAA Guidance, Navigation, and Control Conference 2011). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2011-6352