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人工衛星の高性能姿勢制御の研究
https://jaxa.repo.nii.ac.jp/records/6301
https://jaxa.repo.nii.ac.jp/records/63017aaac710-c161-4266-8cf8-3629c3f4f5fa
名前 / ファイル | ライセンス | アクション |
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49054045.pdf (1.3 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 人工衛星の高性能姿勢制御の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | コントロールモーメントジャイロ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機マヌーバ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角運動量 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 慣性モーメント | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | bang-bang制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | トルク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リアクションホイール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アクチュエータ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control moment gyroscope | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft maneuver | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular momentum | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | moment of inertia | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bang-bang control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | torque | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reaction wheel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | actuator | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | A study of high performance maneuver for artificial satellite | |||||
著者 |
遠藤, 達也
× 遠藤, 達也× 川井, 洋志× 関口, 毅× 鈴木, 秀人× Endo, Tatsuya× Kawai, Hiroshi× Sekiguchi, Takeshi× Suzuki, Hideto |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems 巻 JAXA-SP-05-008, p. 219-224, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This is the report of a study of high performance maneuver for artificial satellite. Especially, CMG (Control Moment Gyro) aiming to agile reorientation maneuver is discussed in this report. The number and the arrangement of the CMG cluster were examined, for Rest-to-Rest maneuvering. The performance presumption parameter to the first design estimate was derived. The CMG assembly design for agile maneuver is determined by requirement of angular momentum and the moment of inertia of satellite. The result of the CMG assembly arrangement should be discussed from the point of electrical energy consumption, precise weight estimation and cost. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049054045 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-05-008 |