{"created":"2023-06-20T14:40:31.023645+00:00","id":7409,"links":{},"metadata":{"_buckets":{"deposit":"49134ba2-a276-4e40-9103-544bac676505"},"_deposit":{"created_by":1,"id":"7409","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7409"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007409","sets":["1543:1544:1555","1887:1891"]},"author_link":["39290","39288","39287","39289"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"LOS angle feedback control for formation flying spacecraft"}]},"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":"衛星によるフォーメーションフライトの，軌道維持に用いるフィードバック制御則について述べる．提案する制御則は，定められた軌道を航行する目標衛星のLOS角を基に，各々の衛星の加速度を決定するものである．Hillの方程式に基づくシミュレーションにより，複数衛星が与えられた初期位置から，定められたフォーメーションが形成され，維持できることを示す．","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper, we focus on a feedback control law which leads to formation flight that several spacecraft keep relative position in short distance and move on a prescribed orbit. The proposed control law determines the acceleration of each spacecraft based on the line of sight (LOS) angle measurements to a target satellite moving on the prescribed orbit. Through numerical simulations using Hill ’s equation, we verify that the group of spacecraft moves from a given initial state into a prescribed flying formation by the proposed approach.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064733035","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":"大阪大学"},{"subitem_text_value":"大阪大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Osaka University"},{"subitem_text_language":"en","subitem_text_value":"Osaka 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":"田畑, 哲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮崎, 文夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tabata, Tetsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazaki, Fumio","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":"複数衛星のフォーメーションフライトにおけるLOS 角に基づくフィードバック制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"複数衛星のフォーメーションフライトにおけるLOS 角に基づくフィードバック制御"}]},"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":"7409","relation_version_is_last":true,"title":["複数衛星のフォーメーションフライトにおけるLOS 角に基づくフィードバック制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:39:57.785364+00:00"}