柔軟宇宙構造物ダイナミクスの定式化について
スポンサーリンク
概要
著者
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Yamaguchi Isao
National Aerospace Laboratory
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KIDA Takashi
National Aerospace Laboratory
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YAMADA Katsuhiko
Mitsubishi Electric Corporation
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Ookami Yoshiaki
航空宇宙技術研究所
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Yamaguchi Isao
Japan Aerospace Exploration Agency (jaxa)
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Yamaguchi Isao
Aerospace Research And Development Directorate (ard) Japan Aerospace Exploration Agency (jaxa)
関連論文
- 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
- ON-ORBIT ATTITUDE CONTROL EXPERIMENTS FOR ETS-VI BY I-PD CONTROL
- 柔軟宇宙構造物ダイナミクスの定式化について
- ROBUST ATTITUDE CONTROL USING MU-SYNTHESIS FOR THE LARGE FLEXIBLE SATELLITE ETS-VIII
- Multi-input Multi-output System Identification Using Impulse Responses
- In-orbit Control Experiment on ETS-VIII Spacecraft
- Robust Attitude Control Using Mu-Synthesis for the Large Flexible Satellite ETS-VIII