In-orbit Control Experiment on ETS-VIII Spacecraft
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概要
- 論文の詳細を見る
This paper describes an in-orbit attitude control experiment carried out on ETS (Engineering Test Satellite)-VIII in June 2009 and March 2010.This experiment aims to develop a technical basis for the attitude control of a class of future large flexible spacecraft. Four novel robust control laws were developed and tested through the experiment;DVDFB (Direct Velocity and Displacement FeedBack) control law, DDFB (Dynamic Displacement FeedBack) control law, μ-synthesis based control law, and linearly interpolated gain scheduling law.Experimental resultsofeach control law are presented to show its high control performance compared with a conventional control law.
著者
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KASAI Tokio
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Chofu
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YAMAGUCHI Isao
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Chofu
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MITANI Shinji
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Tsukuba
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IKEDA Masafumi
Space Applications Mission Directorate, Japan Aerospace Exploration Agency
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SUNAGAWA Kei
Space Applications Mission Directorate, Japan Aerospace Exploration Agency
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Kida Takashi
University Of Electro-communications
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Ohtani Takashi
Japan Aerospace Exploration Agency (jaxa)
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Mitani Shinji
Japan Aerospace Exploration Agency (jaxa)
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Ohtani Takashi
Aerospace Research And Development Directorate (ard) Japan Aerospace Exploration Agency (jaxa)
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HAMADA Yoshiro
Aerospace Research and Development Directorate (ARD),Japan Aerospace Exploration Agency (JAXA)
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NAGASHIRO Tomoyuki
University of Electro-Communicatios
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IGAWA Takahiro
Aerospace Research and Development Directorate (ARD),Japan Aerospace Exploration Agency (JAXA)
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Sunagawa Kei
Space Applications Mission Directorate Jaxa
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Mitani Shinji
Aerospace Research And Development Directorate (ard) Japan Aerospace Exploration Agency (jaxa)
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Igawa Takahiro
Aerospace Research And Development Directorate (ard) Japan Aerospace Exploration Agency (jaxa)
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Ikeda Masafumi
Space Applications Mission Directorate Jaxa
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Hamada Yoshiro
Aerospace Research And Development Directorate (ard) Japan Aerospace Exploration Agency (jaxa)
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Yamaguchi Isao
Aerospace Research And Development Directorate (ard) Japan Aerospace Exploration Agency (jaxa)
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KASAI Tokio
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency
関連論文
- On-Orbit System Identification Experiments of the Engineering Test Satellite-VIII
- System Identification Using Impulse Response Including Initial States
- A Preliminary Study on Precise Attitude Switching Maneuver of Flexible Spacecraft Using CMG
- ETS-VI On-Orbit System Identification Experiments
- On-Orbit System Identification and Attitude Control Experiment of ETS-VI
- 柔軟宇宙構造物ダイナミクスの定式化について
- Optimal Static Output Feedback Control for Large Space Structures and Its Application to Local Control
- ROBUST ATTITUDE CONTROL USING MU-SYNTHESIS FOR THE LARGE FLEXIBLE SATELLITE ETS-VIII
- Flight result of SDS-1 and development of SDS-4 in JAXA(Technical Session,ICSANE 2011(International Conference on Space, Aeronautical and Navigational Electronics 2011))
- In-orbit Control Experiment on ETS-VIII Spacecraft
- Application of MPC to Spacecraft Attitude Maneuver using RCS and/or RW
- Robust Attitude Control Using Mu-Synthesis for the Large Flexible Satellite ETS-VIII