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- KIDA Takashi
- 航空宇宙技術研究所
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- YAMAGUCHI Isao
- 航空宇宙技術研究所
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- OKAMOTO Osamu
- 航空宇宙技術研究所
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- OHKAMI Yoshiaki
- 航空宇宙技術研究所
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- ICHIKAWA Shinichiro
- 宇宙開発事業団
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- TANAKA Shunsuke
- 宇宙開発事業団
Bibliographic Information
- Other Title
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- 大型柔軟衛星の三軸制御に関する実験的検討
- オオガタ ジュウナン エイセイ ノ 3ジク セイギョ ニ カンスル ジッケンテ
Search this article
Abstract
This paper studies three-axis attitude control problems of a class of flexible spacecraft having elastic appendages. A Linear Quadratic Regulator (LQR) associated with a state estimator is designed to control its attitude and the appendage vibration, simultaneously. In order to evaluate and demonstrate the controller performance, ground-based control experiments are conducted, using a ETS (Engineering Test Satellite)-VI laboratory model supported on a single-axis air-table. The evaluation is made concerning mainly with (a) LQR realization by using a thruster and a reaction wheel, and (b) stability robustness against the truncated vibration modes of flexible appendages.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 35 (407), 569-576, 1987
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
- 1390001204505751936
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- NII Article ID
- 130003958708
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL BIB ID
- 3154455
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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