{"created":"2023-06-20T14:40:32.865148+00:00","id":7450,"links":{},"metadata":{"_buckets":{"deposit":"362cb172-2713-4ae7-9ca0-70bcd51fa54f"},"_deposit":{"created_by":1,"id":"7450","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7450"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007450","sets":["1543:1544:1556","1887:1891"]},"author_link":["39668"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"83","bibliographicPageStart":"69","bibliographic_titles":[{"bibliographic_title":"第17回アストロダイナミクスシンポジウム講演後刷り集　2007"},{"bibliographic_title":"Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Patched conics is the standard tool for designing fly-by or gravity assist maneuvers performed by a spacecraft about a planet. In this procedure, the trajectory of the spacecraft about the planet is taken as a perfect hyperbola once the spacecraft is in the sphere of influence of the planet. All other perturbations are neglected. As a consequence the outgoing V infinity is identical to the incoming V infinity. In reality, the spacecraft spends a finite time in the sphere of influence of the planet. A typical time is a week. The small perturbations caused by the Sun will affect the ideal hyperbolic trajectory. When the fly-by planet is the Earth, the Moon and J2 cause also small changes in the hyperbola. The small changes in V infinity are the subject of this paper. The perturbation of the Sun can be modeled as a restricted three body problem or analyzed with the standard averaging technique applied to an hyperbolic orbit. We compare our results to the real data of the fly-by past the Earth on March 4, 2005 by the Rosetta spacecraft on his way to the comet Churymov-Gerasimenko (2014).","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063718013","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_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":"Janssens, Frank","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"3体問題","subitem_subject_scheme":"Other"},{"subitem_subject":"2体問題","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道解析","subitem_subject_scheme":"Other"},{"subitem_subject":"エネルギー交換","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道力学","subitem_subject_scheme":"Other"},{"subitem_subject":"数学的解析","subitem_subject_scheme":"Other"},{"subitem_subject":"フライバイ","subitem_subject_scheme":"Other"},{"subitem_subject":"マヌーバ","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"円錐曲線貼り合わせ","subitem_subject_scheme":"Other"},{"subitem_subject":"影響球","subitem_subject_scheme":"Other"},{"subitem_subject":"SOI","subitem_subject_scheme":"Other"},{"subitem_subject":"three body problem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two body problem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"energy exchange","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital mechanics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mathematical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flyby","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"maneuver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equation of motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"patched conic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sphere of influence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SOI","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":"Influence of the finite duration on a fly-by","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Influence of the finite duration on a fly-by","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1556","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7450","relation_version_is_last":true,"title":["Influence of the finite duration on a fly-by"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:39:20.770439+00:00"}