{"created":"2023-06-20T14:40:45.640428+00:00","id":7689,"links":{},"metadata":{"_buckets":{"deposit":"c23cb1c8-16ff-4752-8e1b-02e608e88aae"},"_deposit":{"created_by":1,"id":"7689","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7689"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007689","sets":["1543:1544:1559","1887:1891"]},"author_link":["41219","41221","41220","41222"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"長楕円軌道におけるランデブ方式の提案"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"329","bibliographicPageStart":"324","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":"地球周回軌道上の衛星(ターゲット)に対するサービスの1つとして操作可能な宇宙ロボット(チェイサ)がターゲットに接近し、外観の観察や修理などを行なうことが考えられている。本論文では非協力なターゲットに対するランデブ軌道制御の方法を提案する。提案する制御方法は、長楕円軌道上での運動解析をもとに周期的な状態遷移則を求めて、できるだけ簡単で最適な軌道制御が実現できるようにした。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents considerations of formulation and design for spacecraft rendezvous control on elliptic orbits around the earth. Spacecraft rendezvous is a key technique for orbital services to the target spacecraft such as resupply, review, assembling or mend. In order to formulate, it is needed to derive a linearized equation of relative motion between two spacecrafts (target and chaser) on an elliptic orbit. The solution of this equation is generally composed of periodic term and secular term (which is called drift motion in this paper). Based on this fact, a discrete state transition law of relative motion can be obtained, which enables realization of simple rendezvous control of the chaser.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897056","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":"京都大学 大学院工学研究科"},{"subitem_text_value":"京都大学 工学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyoto University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyoto University Faculty of Engineering"}]},"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":"林, 一樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"土屋, 和雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hayashi, Kazuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuchiya, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙ランデブー","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機制御","subitem_subject_scheme":"Other"},{"subitem_subject":"楕円軌道","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":"相対運動","subitem_subject_scheme":"Other"},{"subitem_subject":"永年変動","subitem_subject_scheme":"Other"},{"subitem_subject":"周期変動","subitem_subject_scheme":"Other"},{"subitem_subject":"space rendezvous","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elliptical orbit","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":"relative motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"secular variation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"periodic variation","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":"A new approach for spacecraft rendezvous control on elliptic orbits","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A new approach for spacecraft rendezvous control on elliptic orbits","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":"7689","relation_version_is_last":true,"title":["A new approach for spacecraft rendezvous control on elliptic orbits"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:35:35.770361+00:00"}