WEKO3
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小型衛星μ-LabSatによる月トラッキング姿勢制御実験
https://jaxa.repo.nii.ac.jp/records/2248
https://jaxa.repo.nii.ac.jp/records/2248d4bdf5f0-e7bf-4145-8293-14c86d46317b
名前 / ファイル | ライセンス | アクション |
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49202000.pdf (6.1 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 | 小型衛星μ-LabSatによる月トラッキング姿勢制御実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | μ-LabSat | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スライディングモード制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月トラッキング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 視線 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ハードウエアインザループシミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 在宇宙実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月トラッキング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御入力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道上実験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | microsatellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | micro-LabSat | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sliding mode control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | moon tracking | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | line of sight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hardware in the loop simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spaceborne experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | moon tracking | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control input | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | on-orbit experiment | |||||
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 | Moon tracking attitude control experiment of a micro satellite micro-LabSat | |||||
著者 |
照井, 冬人
× 照井, 冬人× 木村, 真一× 永井, 康史× 山本, 宏× 吉原, 圭介× 山元, 透× 中須賀, 真一× Terui, Fuyuto× Kimura, Shinichi× Nagai, Yasufumi× Yamamoto, Hiroshi× Yoshihara, Keisuke× Yamamoto, Toru× Nakasuka, Shinichi |
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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 | ||||||
情報通信研究機構 | ||||||
著者所属 | ||||||
情報通信研究機構 | ||||||
著者所属 | ||||||
情報通信研究機構 | ||||||
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 | ||||||
東京大学 大学院工学系研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute of Information and Communications Technology | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute of Information and Communications Technology | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute of Information and Communications Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo School of Engineering | ||||||
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研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-05-038, 発行日 2006-03-31 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 'Micro-LabSat', a micro-piggyback satellite, was launched by an H-2A rocket on December 14, 2002. One of its missions was to release truncated cone-shaped targets with representative dimensions of approximately 10 cm and evaluate the use of machine vision to estimate their position and attitude relative to the satellite. As a follow-on mission using the same camera, an attitude control moon-tracking maneuver was planned comprising the following steps: (1) recognize the moon in captured images and track it continuously, (2) calculate the median point of the moon, (3) control the satellite's attitude to move the moon's position in the image to be near the image center, (4) maintain the moon's position near the center of the image. Micro-LabSat is a bias-momentum micro satellite with two wheels, a configuration that is not normally capable of agile attitude maneuvers. This paper describes an algorithm 'Sliding Mode Controller using the Rodriguez parameter' that has been developed to enable such maneuvers, and presents the results of its evaluation by numerical simulation and an on-orbit moon tracking experiment. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049202000 | |||||
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-RR-05-038 |