{"created":"2023-06-20T14:40:28.661786+00:00","id":7364,"links":{},"metadata":{"_buckets":{"deposit":"67c5bb64-4fc1-4d7a-af07-8c3bc64fa7f7"},"_deposit":{"created_by":1,"id":"7364","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7364"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007364","sets":["1543:1544:1554","1887:1891"]},"author_link":["38981","38983","38980","38982"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"画像運動推定を活用した非協力ターゲットへの宇宙機の位置追従マニューバ制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"2009","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 19th 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":"アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部))","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":"Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), 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":"小惑星や故障衛星などの非協力target に対する自律ロボット衛星(\"pursuer\")の位置・姿勢追従マニューバストラテジについて検討する．本ストラテジは最適フィードフォワード制御フェイズとフィードバック制御フェイズを組み合わせて構成されており，最適フィードフォワード制御フェイズにおいては，targetの運動推定結果より予測されるtargetの未来位置・姿勢情報を用いてpursuerをtargetの運動に同期した軌道に投入する．本稿ではtargetとして地球低軌道上の機能不全衛星を想定し，target同期軌道へpursuer を投入する最適マニューバ制御法について検討する．","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this research, a control strategy for a spacecraft(\"Pursuer\") to rendezvous with an uncooperative object (\"Target\") is dealt with. This strategy consists of a feedforward optimal control phase and feedback control phases. In the feedforward optimal control phase, the pursuer is injected into trajectory synchronized with the target's motion using the future position and velocity of the target obtained by motion estimation. In this paper, designing the optimal control maneuver to the trajectory synchronized with the target motion assuming a space debris removal mission in LEO is investigated.","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: AA0064734059","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":"電気通信大学"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications (UEC)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"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":"今泉, 継男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"照井, 冬人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Imaizumi, Tsuguo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Terui, Fuyuto","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":"Relative Motion Estimation and Control Strategy for a Spacecraft to an Uncooperative Object","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Relative Motion Estimation and Control Strategy for a Spacecraft to an Uncooperative Object","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1554","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7364","relation_version_is_last":true,"title":["Relative Motion Estimation and Control Strategy for a Spacecraft to an Uncooperative Object"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:40:39.833577+00:00"}