{"created":"2023-06-20T14:40:23.969947+00:00","id":7279,"links":{},"metadata":{"_buckets":{"deposit":"f40f9f0b-cd3f-4617-9de6-bd86bb51b6b6"},"_deposit":{"created_by":1,"id":"7279","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7279"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007279","sets":["1543:1544:1553","1887:1891"]},"author_link":["38451","38449","38452","38450"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"パルス入力による円軌道上のフォーメーションフライト"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"198","bibliographicPageStart":"193","bibliographicVolumeNumber":"20","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":"The 20th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県　","subitem_description_type":"Other"}]},"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":"The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本講演では､円軌道上の主衛星(Leader)に対する,従衛星(Follower)の相対軌道遷移を考察する.フォーメーション問題は,線形化された相対運動方程式であるHCW方程式の周期解で記述される.一定幅のパルス入力を用いて軌道遷移を行うとき,増速量には下限が存在するが,3回の入力で総速度変化量最小の軌道遷移が達成できる.さらに,最適レギュレータ理論を用いて準最適フィードバック制御を設計し,そのシミュレーション結果を紹介する.","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper considers formation flight along a circular orbit. The relative motion of one space craft (follower) with respect to another (leader) in a circular orbit is described by nonlinear autonomous diferential equations, and their linearized equations are known as Hill-Clohessy-Wiltshire (HCW) equations. Formation problems are formulated by the periodic solutions of HCW equations. Control inputs are assumed to be pulse inputs of a constant width, and their performance index is the total velocity change. It is shown that there exist optimal three pulse strategies. Using the optimal regulator theory, suboptimal feedback controls are designed and simulation results are given.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065115032","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所 (JAXA)(ISAS)"}]},"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)(ISAS)"}]},"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":"東京大学工学部航空宇宙工学科"},{"subitem_text_value":"南山大学情報理工学部システム創成工学科"}]},"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, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Department of Systems Design and Engineering, Faculty of Information Sciences and Engineering, Nanzan 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":"地福, 亮"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"市川, 朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Jifuku, Ryo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ichikawa, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Formation Flight along a Circular Orbit with Pulse Input","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Formation Flight along a Circular Orbit with Pulse Input","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1553","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7279","relation_version_is_last":true,"title":["Formation Flight along a Circular Orbit with Pulse Input"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:41:57.630631+00:00"}