{"created":"2023-06-20T14:40:46.130928+00:00","id":7700,"links":{},"metadata":{"_buckets":{"deposit":"41a328c1-f9d0-4202-9bba-52f429208af4"},"_deposit":{"created_by":1,"id":"7700","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7700"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007700","sets":["1543:1544:1559","1887:1891"]},"author_link":["41318","41324","41319","41321","41317","41315","41322","41323","41316","41320"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"小惑星探査機はやぶさの軌道計画とΔV運用"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"392","bibliographicPageStart":"387","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":"小惑星探査機はやぶさは、2003年5月9日に打上げられ、イオンエンジンによる低推力ΔVにより継続的な軌道変更を行った後、2004年5月19日の地球Swing Byによって、小惑星ITOKAWAに向かう軌道へと移った。Swing By後も、2005年8月末のITOKAWAランデブーに向け、引き続き、軌道計画→イオンエンジン運用→軌道決定→軌道計画のサイクルを回していく。本論文では、1)イオンエンジンによる低推力飛行の軌道計画手法、2)軌道計画から運用手順作成までの手法、3)はやぶさΔV運用／軌道実績、4)低推力飛行における軌道運用のポイント、について報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Asteroid Sample Return Spacecraft HAYABUSA was launched in May 9th, 2003. After the launch, it continuously changed its orbit by Ion Engine and swung by earth in May 19th, 2004. Now it heads in the direction of ITOKAWA (Asteroid 25143). HAYABUSA will rendezvous with ITOKAWA at the end of August 2005. The operation team designs the orbit, operates Ion Engine, determines the orbit with the ranging data and then designs the next orbit. This cycle will be performed continuously until the earth return. This paper describes 1) the orbit design method for low thrust delta-V performed by Ion Engine, 2) the method to create the operation sequence from the delta-V plan, 3) the results of HAYABUSA delta-V operation and the realized orbit, and 4) the important issues for the orbit design with low thrust continuous delta-V.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897067","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":"NEC東芝スペースシステム"},{"subitem_text_value":"NEC東芝スペースシステム"},{"subitem_text_value":"NEC航空宇宙システム"},{"subitem_text_value":"NEC航空宇宙システム"},{"subitem_text_value":"NEC航空宇宙システム"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"NEC TOSHIBA Space Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC TOSHIBA Space Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."}]},"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":"大島, 武"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"萩野, 慎二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木村, 雅文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松岡, 正敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小湊, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oshima, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hagino, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kimura, Masafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuoka, Masatoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kominato, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"はやぶさ宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"小惑星いとかわ","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":"イオンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙ランデブー","subitem_subject_scheme":"Other"},{"subitem_subject":"低推力推進","subitem_subject_scheme":"Other"},{"subitem_subject":"地球スウィングバイ","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道設計","subitem_subject_scheme":"Other"},{"subitem_subject":"HAYABUSA spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Asteroid ITOKAWA","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sample return mission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ion engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space rendezvous","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low thrust propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Earth swingby","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit design","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":"Orbit design & delta-V operation of asteroid sample return spacecraft HAYABUSA","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Orbit design & delta-V operation of asteroid sample return spacecraft HAYABUSA","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":"7700","relation_version_is_last":true,"title":["Orbit design & delta-V operation of asteroid sample return spacecraft HAYABUSA"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:35:25.149911+00:00"}