書誌事項
- タイトル別名
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- タモクテキ サイテキ カ ニ ヨル コントロールモーメントジャイロ トウサイ ウチュウキ ノ タイコショウセイ シセイ セイギョケイ セッケイ
- Fault-Tolerant Attitude Control System using Multi-Objective Optimization for Spacecraft Equipped with Control Moment Gyros
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第58回宇宙科学技術連合講演会(2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県
"Recent years have seen a growing requirement for accurate and agile attitude control of spacecraft. In order to both quickly and accurately control the attitude of a spacecraft, Control Moment Gyros (CMGs) which can generate much higher torque than conventional spacecraft actuators are used as an actuator of spacecraft. Rapid maneuverability is needed for spacecraft with CMGs and it needs drive on motors. It is also said that drive on motors negatively affects lifetime of motors. Moreover, it is also important for attitude control systems to be fault tolerant. In this study, a design method is proposed for the attitude control system, using multi objective optimization of the hardware and software parameters. Pareto solutions are obtained using multi objective optimization of Skew angle and the parameters of the control system. The tendency of the evaluation value with or without optimizing Skew angle and with or without consideration of fault-tolerance is discussed."
資料番号: AC1500049000
レポート番号: JSASS-2014-4449
収録刊行物
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- 第58回宇宙科学技術連合講演会講演集 = Proceedings of 58th Space Sciences and Technology Conference
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第58回宇宙科学技術連合講演会講演集 = Proceedings of 58th Space Sciences and Technology Conference 58 6p-, 2014-11
日本航空宇宙学会(JSASS)
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詳細情報 詳細情報について
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- CRID
- 1050292561247289600
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- NII論文ID
- 40020275948
- 120006839017
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- NII書誌ID
- AA11800503
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- ISSN
- 18841945
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- NDL書誌ID
- 025932993
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- 本文言語コード
- ja
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- 資料種別
- conference paper
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- データソース種別
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