Attitude Control of Spacecraft with Mobile Antenna by a Gain-Scheduled H∞ Controller

• NAGASHIO Tomoyuki

  Graduate School of Electro-Communications, University of Electro-Communications

• KIDA Takashi

  Department of Mechanical Engineering and Intelligent Systems, University of Electro-Communications

書誌事項

タイトル別名

• Attitude Control of Spacecraft with Mobile Antenna by a Gain-Scheduled H.INF. Controller.
• Attitude Control of Spacecraft with Mobile Antenna by a Gain Scheduled H Controller

抄録

This paper studies the attitude control problem of a class of data relay satellite which has a large mobile antenna for tracking target spacecraft in low orbit. The movement of the antenna disturbs the satellite attitude motion through dynamic coupling of the motions of the antenna and the satellite main body. In the operation, control of the spacecraft attitude must be maintained even when the antenna rotates at a high angular velocity. In this paper, we apply robust gain-scheduled controller synthesis to this problem. The controller is designed as a robust stabilizing controller based on the H_∞ controller synthesis of linear parameter varying system. The capability of the method is investigated by a numerical study.

収録刊行物

• TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 43 (139), 16-22, 2000

  一般社団法人 日本航空宇宙学会

キーワード

• Spacecraft
• Linear Parameter Varying System
• Robust Control

詳細情報

• CRID: 1390001204080115328
• NII論文ID: 10004294275
• NII書誌ID: AA0086707X
• DOI: 10.2322/tjsass.43.16
• ISSN: 21894205
• ISSN: 05493811
• NDL書誌ID: 5423301
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I5423301
• Web Site: https://www.jstage.jst.go.jp/article/tjsass/43/139/43_139_16/_pdf
• 本文言語コード: en
• データソース種別:
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  • NDL
  • Crossref
  • CiNii Articles
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