{"created":"2023-06-20T14:40:48.947628+00:00","id":7764,"links":{},"metadata":{"_buckets":{"deposit":"6283528d-ecb9-46e5-8278-542bcf3d43e0"},"_deposit":{"created_by":1,"id":"7764","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7764"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007764","sets":["1543:1544:1561","1887:1891"]},"author_link":["41749","41750","41752","41751","41753","41754"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"スラスタの推力変動を考慮した軌道制御"},{"subitem_alternative_title":"インパルス的な速度変更によるフライアラウンド軌道の設計と制御"}]},"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Control in consideration of a change in the thrust"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"15","bibliographicPageStart":"8","bibliographic_titles":[{"bibliographic_title":"平成14年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"Hillの方程式を用いて、真円の衛星軌道上で故障衛星(ターゲット)の周りを周期的に飛行する宇宙ロボット(チェイサ)の動力学を考える。これまで、インパルス的な速度変更による3次元フライアラウンド軌道と制御手法を提案した。本論文では、スラスタの推力に変動が生じることを考慮した軌道の制御手法に関して議論する。軌道の安定化をシミュレーションによって検証する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Based on the Hill's equation, orbital dynamics of a space robot (chaser) flying periodically around a trouble satellite (target) on a circular orbit around the earth is considered. Three-dimensional flyaround trajectories by impulsive thrust and control methods were proposed. This paper discusses a control in consideration of a change in the thrust. The stabilization of the orbit is verified by the simulation.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045497002","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"大阪大学 大学院基礎工学研究科"},{"subitem_text_value":"大阪大学 大学院基礎工学研究科"},{"subitem_text_value":"大阪大学 大学院基礎工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Osaka University Graduate School of Engineering Science"},{"subitem_text_language":"en","subitem_text_value":"Osaka University Graduate School of Engineering Science"},{"subitem_text_language":"en","subitem_text_value":"Osaka University Graduate School of Engineering Science"}]},"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":"菅原, 正行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"升谷, 保博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮崎, 文夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugahara, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masutani, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazaki, Fumio","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星捕捉","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星制御","subitem_subject_scheme":"Other"},{"subitem_subject":"フライアラウンド軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機推進","subitem_subject_scheme":"Other"},{"subitem_subject":"インパルス的速度変更","subitem_subject_scheme":"Other"},{"subitem_subject":"Hill方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙力学","subitem_subject_scheme":"Other"},{"subitem_subject":"円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"ロボットダイナミクス","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite capture","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flyaround trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"impulsive velocity change","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hill equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"astrodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"circular orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robot dynamics","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":"Design and control of flyaround trajectory by impulsive velocity change","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Design and control of flyaround trajectory by impulsive velocity change","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1561","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7764","relation_version_is_last":true,"title":["Design and control of flyaround trajectory by impulsive velocity change"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:26.249728+00:00"}