書誌事項
- タイトル別名
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- H.INF. Tracking Control for Minimum Time Slewing of Flexible Space Structure
- ジュウナン ウチュウ コウゾウブツ ノ サイタン ジカン スルーマヌーバ ニ タイスル H トラッキング セイギョ
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This paper presents experimental results of H infinity tracking control for slewing flexible space structures. The model of flexible space structure employed in the experiment consists of a rigid body rotating around a shaft and a flexible beam attached to the rigid body. The minimum time optimal control for flexible structure, which is a multi bang-bang control, is used to obtain a reference optimal trajectory. Two full-bridge strain gauges are located at the root of the beam in order to sense the bending-moment of the flexible beam and a tachometer is located at the rotary shaft of the torque motor in order to measure the angular velocity of the rigid main body. The angular velocity and bending-moment are utilized to calculate the control torque provided to the main body. The effectiveness of the H infinity feedback tracking control on suppression of residual vibration and achieving the goal attitude is studied for two types of flexible beams experimentally.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 53 (621), 482-489, 2005
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204469178368
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- NII論文ID
- 10020377897
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 7699739
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可