Optimal Static Output Feedback Control for Large Space Structures and Its Application to Local Control

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A static output feedback control having positive definite gains is known to give a certain robust stability to a class of collocated space structures. This paper studies an optimal design for static output feedback gains which minimize the <I>H</I><SUB>∞</SUB> norm so that the closed-loop system has the prescribed disturbance attenuation capability. For this purpose, two synthesis methods via linear matrix inequalities are proposed. Then, considering structural robustness, the construction of a local feedback control system is investigated. System features include a set of local controllers with a simple structure and the high fault tolerance for preserving closed-loop stability. The validity is numerically shown using a simple uniform beam model.

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 47(155), 1-8, 2004-05-04

    THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

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各種コード

  • NII論文ID(NAID)
    10012934681
  • NII書誌ID(NCID)
    AA0086707X
  • 本文言語コード
    ENG
  • 資料種別
    ART
  • ISSN
    05493811
  • NDL 記事登録ID
    6945486
  • NDL 雑誌分類
    ZN25(科学技術--運輸工学--航空機・ロケット)
  • NDL 請求記号
    Z53-M236
  • データ提供元
    CJP書誌  NDL  J-STAGE 
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