{"created":"2023-06-20T14:40:46.485760+00:00","id":7708,"links":{},"metadata":{"_buckets":{"deposit":"05978baf-56f0-4f43-800d-9e3f6fe3c2ef"},"_deposit":{"created_by":1,"id":"7708","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7708"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007708","sets":["1543:1544:1560","1887:1891"]},"author_link":["41383","41391","41395","41390","41396","41389","41392","41394","41384","41385","41387","41398","41397","41393","41386","41388"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"のぞみSwing-by軌道運用"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"47","bibliographicPageStart":"35","bibliographic_titles":[{"bibliographic_title":"平成15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 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"「のぞみ」探査機は、1998年に打ち上げられ、その地球出発時に推進系のトラブルから火星到着までの飛行を大幅に延長・変更した新たなシーケンスにしたがって、現在飛行している。昨年12月と、本年6月の2度の地球Swing-byは、その遂行上、非常に重大な軌道操作であった。本論文では、これらの軌道計画と運用報告、および火星周回軌道投入(MOI)を含めた燃料消費量の最小化についての検討結果について報告する。同時に、ΔVLBIにより行われた航法・軌道推定実験結果についても、その結果を紹介する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"'Nozomi' spacecraft that was launched in 1998 has continued its flight to the Mars. Last December and this June, it successfully performed the double consecutive Earth swingbys. This tactical orbit sequence alleviates the delta-V amount for the spacecraft to be captured around the Mars, and enables the scientific observation as planned originally. The paper reports how the guidance and navigation were carried out as for the swingbys. The paper especially refers to the delta-VLBI technique attempted and introduced. The contents of the paper are all based on the actual operation results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652007","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":"日本電気航空宇宙システム"},{"subitem_text_value":"日本電気航空宇宙システム"},{"subitem_text_value":"富士通"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"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":"Fujitsu Ltd."},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"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":"木村, 雅文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"日高, 智成"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大西, 隆史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山川, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中谷, 一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"早川, 基"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉川, 真"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川口, 淳一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kimura, Masafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hidaka, Tomonari","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onishi, Takafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamakawa, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakatani, Ichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hayakawa, Hajime","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"のぞみ宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"火星","subitem_subject_scheme":"Other"},{"subitem_subject":"地球スウィングバイ","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導","subitem_subject_scheme":"Other"},{"subitem_subject":"航法","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機回収","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道挿入","subitem_subject_scheme":"Other"},{"subitem_subject":"地球重力","subitem_subject_scheme":"Other"},{"subitem_subject":"Nozomi spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Earth swingby","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft recovery","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit insertion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Earth gravitation","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":"NOZOMI consecutive double earth swingbys flight to Mars: Guidance and navigation report","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"NOZOMI consecutive double earth swingbys flight to Mars: Guidance and navigation report","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1560","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7708","relation_version_is_last":true,"title":["NOZOMI consecutive double earth swingbys flight to Mars: Guidance and navigation report"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:35:18.581915+00:00"}