H.INF. Tracking Control for Minimum Time Slewing of Flexible Space Structure
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- Kojima Hirohisa
- 東京都立科学技術大学
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- Fujiki Takaaki
- 東京都立科学技術大学
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- A. Fujii Hironori
- 東京都立科学技術大学
Bibliographic Information
- Other Title
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- 柔軟宇宙構造物の最短時間スルーマヌーバに対するH∞トラッキング制御
- 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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Abstract
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.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 53 (621), 482-489, 2005
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390001204469178368
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- NII Article ID
- 10020377897
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 7699739
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed