{"created":"2023-06-20T14:40:42.311090+00:00","id":7621,"links":{},"metadata":{"_buckets":{"deposit":"d40147be-795d-4d12-8049-d3b466cb9505"},"_deposit":{"created_by":1,"id":"7621","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7621"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007621","sets":["1543:1544:1558","1887:1891"]},"author_link":["40829","40830","40827","40831","40825","40826","40828","40832"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"人工衛星の捕捉および結合時の安定化非線形制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"363","bibliographicPageStart":"358","bibliographic_titles":[{"bibliographic_title":"第15回アストロダイナミクスシンポジウム講演後刷り集　2005"},{"bibliographic_title":"Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"将来の宇宙インフラストラクチャ構想において、衛星への燃料補給や故障衛星を回収するミッションが考えられている。それらを遂行するためにはターゲットに対し、チェイサーの接近、結合、捕捉が必要になるが、宇宙機の運動は回転と並進が干渉した非線形システムで表され、それを考慮した制御系を設計する必要がある。そこで本研究では人工衛星の捕捉および結合時における結合前後の安定条件を満たす非線形制御系の設計法を検討する。そして数値例によりその有効性を確認する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the future space infra-structure plan, the missions of spacecraft capturing and docking are considered. The motion of the spacecraft is described as the nonlinear system interfered of the rotation and translation dynamics. We derive the condition of the stabilizing controller for the nonlinear spacecraft system before and after docking and capturing. Then, its capability is investigated by numerical simulations.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480056","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/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"電気通信大学 大学院"},{"subitem_text_value":"電気通信大学 大学院"},{"subitem_text_value":"電気通信大学"},{"subitem_text_value":"電気通信大学"}]},"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 Graduate School"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications Graduate School"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications"}]},"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":"伊藤, 玲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"池田, 裕一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長塩, 知之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木田, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ikeda, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagashio, Tomoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kida, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星制御","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星追跡","subitem_subject_scheme":"Other"},{"subitem_subject":"タンブリング運動","subitem_subject_scheme":"Other"},{"subitem_subject":"制御則","subitem_subject_scheme":"Other"},{"subitem_subject":"非線形制御","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機捕捉","subitem_subject_scheme":"Other"},{"subitem_subject":"PD型制御","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機ドッキング","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機回収","subitem_subject_scheme":"Other"},{"subitem_subject":"制御系設計","subitem_subject_scheme":"Other"},{"subitem_subject":"安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"制御理論","subitem_subject_scheme":"Other"},{"subitem_subject":"制御シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"リアプノフ関数","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite tracking","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tumbling motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonlinear control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft capturing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"PD-type control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft docking","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft recovery","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control system design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stabilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Lyapunov function","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"Stabilizing nonlinear control of spacecraft at capturing and docking phase","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Stabilizing nonlinear control of spacecraft at capturing and docking phase","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1558","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7621","relation_version_is_last":true,"title":["Stabilizing nonlinear control of spacecraft at capturing and docking phase"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:39.412770+00:00"}