{"created":"2023-06-20T14:40:45.684328+00:00","id":7690,"links":{},"metadata":{"_buckets":{"deposit":"15f75008-a916-4931-a818-07880d502123"},"_deposit":{"created_by":1,"id":"7690","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7690"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007690","sets":["1543:1544:1559","1887:1891"]},"author_link":["41230","41226","41223","41228","41227","41224","41229","41225"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"宇宙機の近傍飛行制御のための人工ポテンシャル法の適用について"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"333","bibliographicPageStart":"330","bibliographic_titles":[{"bibliographic_title":"平成16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 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本研究では、軌道上を飛翔する宇宙ステーションの回りに補給船を周回飛行させるための制御手法として、人工ポテンシャル法の適用を検討する。人工ポテンシャル法は、目標位置で最小値をとるポテンシャル関数を作業空間に設定し、その効果によって発生する仮想的な吸引力、あるいは斥力を制御力として利用する手法である。この手法を適用することにより、低推力の連続スラスタを用いた誘導手法の実現を試みる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Application of artificial potential method is considered for the fly-around of the subsatellite (chaser) around the space station (target). The artificial potential method is the technique of guiding the object to the destination along the slope of the potential function whose minimum corresponds to the destination in the work space, by generating virtual control force. By assuming the availability of the continuous low-thrust actuators, an uniformly asymptotically stabilizing controller is proposed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897057","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_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":"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"},{"subitem_text_value":"電気通信大学 大学院"}]},"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"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications Graduate School"}]},"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":"中島, 健志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木田, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長塩, 知之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青砥, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakajima, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kida, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagashio, Tomoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoto, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"人工ポテンシャル法","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機近傍飛行制御","subitem_subject_scheme":"Other"},{"subitem_subject":"ターゲット","subitem_subject_scheme":"Other"},{"subitem_subject":"チェーサー","subitem_subject_scheme":"Other"},{"subitem_subject":"ランデブー宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"フィードバック制御","subitem_subject_scheme":"Other"},{"subitem_subject":"推力","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"artificial potential method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft fly-around control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"target","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chaser","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rendezvous spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"feedback control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation","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":"Application of artificial potential method to spacecraft fly-around control","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Application of artificial potential method to spacecraft fly-around control","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1559","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7690","relation_version_is_last":true,"title":["Application of artificial potential method to spacecraft fly-around control"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:35:34.945804+00:00"}