{"created":"2023-06-20T14:40:30.691394+00:00","id":7404,"links":{},"metadata":{"_buckets":{"deposit":"b2244dfa-a552-4d44-97bf-77c6f53459e8"},"_deposit":{"created_by":1,"id":"7404","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7404"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007404","sets":["1543:1544:1555","1887:1891"]},"author_link":["39258","39256","39260","39257","39259","39261"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Non-holonomic Analysis and Control of a Thruster Driven Free-Floating Satellite"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"2008","bibliographic_titles":[{"bibliographic_title":"アストロダイナミクスシンポジウム講演後刷り集"},{"bibliographic_title":"Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"方向が固定された3つのスラスターをもつ浮遊衛星について，２次元面内での挙動を考える．この衛星の支配方程式は，スラスターの方向が衛星姿勢角に応じて変化するため，２階の\"非ホロノミック拘束\"となる．まず最初に，スラスターの方向によって衛星の可制御性を分類する．次に2つの制御手法を提案する．1つは衛星のドリフト運動を抑制することができる制御法であり，もう1つはフィードバックにより支配方程式をホロノミック拘束に変換する手法である．2番目の方法を用いることで，衛星の位置と姿勢を同時にかつ正確に目標値に制御できる手法を述べる．","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This study deals with in-plane motion of a free-floating satellite equipped with three thrusters whose directions are fixed to the satellite. The system's governing equations forms a second-order \"nonholonomic\" constraint, because the thruster force directions change according to the satellite attitude. First, controllability of the satellite is categorized according to the directions of the thrusters. Then, this paper proposes two control methods for position and/or attitude control of the satellite; one can suppress the drift of the satellite, and the other transfers the system's nonholonomic governing equations into holonomic ones by a feedback control. Using the second method, this paper explains the procedure to control the satellite's position and attitude simultaneously and precisely.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064733030","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11567475","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"九州大学大学院工学研究院航空宇宙工学部門"},{"subitem_text_value":"九州大学大学院工学研究院航空宇宙工学部門"},{"subitem_text_value":"九州大学大学院工学研究院航空宇宙工学部門"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautics and Astronautics, Kyushu University"},{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautics and Astronautics, Kyushu University"},{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautics and Astronautics, Kyushu University"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"外本, 伸治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩瀬, 正興"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 淳也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hokamoto, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwase, Masaoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Junya","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"スラスター駆動の浮遊衛星に対する非ホロノミック解析と制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スラスター駆動の浮遊衛星に対する非ホロノミック解析と制御"}]},"item_type_id":"5","owner":"1","path":["1555","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7404","relation_version_is_last":true,"title":["スラスター駆動の浮遊衛星に対する非ホロノミック解析と制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:40:02.175318+00:00"}