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モデル予測制御による小規模飛行実験機の水平面内誘導: 直線軌道追従ケースでの飛行試験結果
https://jaxa.repo.nii.ac.jp/records/22488
https://jaxa.repo.nii.ac.jp/records/22488aad7dca9-1b0b-4639-8408-391e5495567d
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | モデル予測制御による小規模飛行実験機の水平面内誘導: 直線軌道追従ケースでの飛行試験結果 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | model predictive control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | guidance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight demonstration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | small scale research vehicle (SSRV) | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Lateral Guidance of the Small Scale Research Vehicle by Model Predictive Control: Flight Test Results of Straight Trajectory Tracking | |||||
著者 |
濱田, 吉郎
× 濱田, 吉郎× 塚本, 太郎× 石本, 真二× Hamada, Yoshiro× Tsukamoto, Taro× Ishimoto, Shinji |
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著者所属 | ||||||
宇宙航空研究開発機構航空本部(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙輸送ミッション本部(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 計測自動制御学会(SICE) | |||||
出版者(英) | ||||||
出版者 | The Society of Instrument and Control Engineers (SICE) | |||||
書誌情報 |
計測自動制御学会論文集 en : Transactions of the Society of Instrument and Control Engineers 巻 50, 号 3, p. 236-244, 発行日 2014-03-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper describes the novel lateral guidance law of an unmanned aerial vehicle using model predictive control and shows its flight demonstration results. The guidance law is accompanied with the extended Kalman filter which estimates steady wind velocities in order to follow a pre-specified reference trajectory defined in the ground-fixed coordinate system. The small scale research vehicle, developed by Japan Aerospace Exploration Agency, is used to show the proposed system's high guidance performance in flight demonstrations. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0453-4654 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1883-8189 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00072392 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.9746/sicetr.50.236 | |||||
関連名称 | info:doi/10.9746/sicetr.50.236 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1420039000 |