{"created":"2023-06-20T14:40:40.211035+00:00","id":7587,"links":{},"metadata":{"_buckets":{"deposit":"fb9f1de8-e620-477b-a1d6-31da269b5993"},"_deposit":{"created_by":1,"id":"7587","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7587"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007587","sets":["1543:1544:1558","1887:1891"]},"author_link":["40615","40616","40613","40612","40614","40617"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"次期小惑星探査ミッションの軌道計画の検討状況"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"140","bibliographicPageStart":"135","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":"本発表では、次期小惑星探査ミッションの検討の中で進めている軌道計画の検討状況を報告する。昨年度のシンポジウムでは、対象天体と探査シーケンスを絞り込むための予備検討として、弾道飛行とスウィングバイを組み合わせた探査シーケンスの検討結果を報告した。今回は、その結果を元に選定したミッション候補に対し、電気推進を主推進として地球スウィングバイを組み合わせたE-ΔVEGAの使用を想定した軌道計画を検討したので、その結果を報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Reported in this paper is the status of the trajectory analysis of the asteroid explorer mission now under study in JAXA/ISAS. In the previous symposium, we have reported the results of the preliminary analysis to select the candidates of the target asteroids and the exploration sequence. The global search of the targets and sequences in the space of the combinations of the ballistic trajectories and planetary swing-bys successfully made clear the mission candidates suited our objective. Following the preliminary analysis, more detailed trajectory analysis is performed assuming the usage of the electric propulsion, and the results of which are reported in this paper.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480022","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":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical 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":"川勝, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山川, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安部, 正真"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawakatsu, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamakawa, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Abe, Masanao","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道解析","subitem_subject_scheme":"Other"},{"subitem_subject":"スイングバイ技術","subitem_subject_scheme":"Other"},{"subitem_subject":"電気推進","subitem_subject_scheme":"Other"},{"subitem_subject":"小惑星ミッション","subitem_subject_scheme":"Other"},{"subitem_subject":"サンプルリターンミッション","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"M-V打上げ機","subitem_subject_scheme":"Other"},{"subitem_subject":"逐次2次計画法","subitem_subject_scheme":"Other"},{"subitem_subject":"SQP法","subitem_subject_scheme":"Other"},{"subitem_subject":"EDVEGA","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"マヌーバ","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swingby technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"asteroid mission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sample return mission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"M-V launcher","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sequential quadratic programming method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SQP method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"EDVEGA","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equation of motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"maneuver","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":"Trajectory analysis of post-Hayabusa asteroid explorer mission","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Trajectory analysis of post-Hayabusa asteroid explorer mission","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":"7587","relation_version_is_last":true,"title":["Trajectory analysis of post-Hayabusa asteroid explorer mission"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:37:12.040402+00:00"}