{"created":"2023-06-20T14:40:49.167903+00:00","id":7769,"links":{},"metadata":{"_buckets":{"deposit":"a8ff6535-60ce-4474-9961-1105db1a151d"},"_deposit":{"created_by":1,"id":"7769","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7769"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007769","sets":["1543:1544:1561","1887:1891"]},"author_link":["41784","41795","41793","41796","41792","41799","41800","41790","41791","41788","41797","41789","41798","41786","41785","41787","41783","41794"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"VLBI観測データを用いた軌道決定精度解析"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"44","bibliographicPageStart":"39","bibliographic_titles":[{"bibliographic_title":"平成14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 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"従来の深宇宙探査機の軌道決定では、地上局から衛星を見た視線方向の情報量をもつレンジ・レンジレート観測量を用いるため、これと垂直方向の軌道決定精度には限界がある。一方、VLBI観測データは視線垂直方向に感度をもつため、これら両者のデータを組み合わせて使用すれば、軌道決定精度の向上が期待できる。本論文では、宇宙科学研究所の深宇宙探査機に、VLBI観測データを併用した軌道決定を適用した場合のケーススタディを行い、軌道決定精度の向上効果について述べる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In orbit determination of a deep-space satellite, traditional radiometric data, that is, range and range rate data are used in most cases. Since these data have sensitivity in line of site direction, orbit determination accuracy is good in this direction, but there is less accuracy in perpendicular directions. On the other hand, VLBI data have sensitivity perpendicular to the line of site direction, so the combination of traditional radiometric data and VLBI data are very effective to improve the orbit determination accuracy. In this paper, the orbit determination analysis is carried out by using VLBI observation data, and some typical results for ISAS deep-space satellites are shown.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045497007","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (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":"富士通"},{"subitem_text_value":"富士通"},{"subitem_text_value":"富士通"},{"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":"Fujitsu Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fujitsu Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fujitsu 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":"石橋, 史朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大西, 隆史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"辻本, 滋雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"黒須, 勝利"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉川, 真"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 隆二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"市川, 勉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山川, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川口, 淳一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishibashi, Shiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onishi, Takafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsujimoto, Shigeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kurosu, Katsutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Takaji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ichikawa, Tsutomu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamakawa, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"深宇宙探査","subitem_subject_scheme":"Other"},{"subitem_subject":"超長基線干渉法","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定精度","subitem_subject_scheme":"Other"},{"subitem_subject":"視線方向通信","subitem_subject_scheme":"Other"},{"subitem_subject":"放射計データ","subitem_subject_scheme":"Other"},{"subitem_subject":"地球自転","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deep space exploration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"very long base interferometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"line of sight communication","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"radiometric data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Earth rotation","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 determination analysis using VLBI observation data","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Orbit determination analysis using VLBI observation data","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1561","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7769","relation_version_is_last":true,"title":["Orbit determination analysis using VLBI observation data"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:21.995505+00:00"}