{"created":"2023-06-20T14:39:11.805432+00:00","id":5890,"links":{},"metadata":{"_buckets":{"deposit":"d3293b85-cdf5-4467-ade0-bc1465ad95f1"},"_deposit":{"created_by":1,"id":"5890","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5890"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005890","sets":["1887:1891","9:789:998:1019"]},"author_link":["29068","29064","29067","29066","29061","29062","29065","29063"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Precise orbit and clock estimation software for High Accuracy Positioning Experiment System using Quasi Zenith Satellite System"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"26","bibliographicPageStart":"19","bibliographicVolumeNumber":"JAXA-SP-06-015","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 先進的軌道計測・決定技術に関する研究会論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Advanced Orbit Measurement and Orbit Calculation Technologies","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"現在、宇宙航空研究開発機構(JAXA)および関連機関において、準天頂衛星システムを利用した高精度測位実験システムの開発を行っている。高精度測位実験システムの構成要素の1つであるマスターコントロール実験局は、測位モニタ実験局で受信した準天頂衛星の測位信号をリアルタイムに収集し、軌道時刻推定を行い、その推定結果に基づくエフェメリスやクロックパラメータを含むGPS(Global Positioning System)補完航法メッセージを生成する。本稿では、マスターコントロール実験局で動作する軌道時刻推定ソフトウェアの概要、軌道時刻推定シミュレーションの結果ならびにGPS補完を実現するために必要となるGPS時系との接続方法についての概要を紹介する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Japan Aerospace Exploration Agency (JAXA) has started the development of High Accuracy Positioning Experiment System using Quasi-Zenith Satellite System (QZSS). The Master Control Station (MCS) which is one of the components of High Accuracy Positioning Experiment System performs precise orbit and clock estimation using QZSS and GPS (Global Positioning System) positioning signals and generates navigation messages for QZSS users. This paper presents an overview of the precise orbit and clock estimation software, simulation results of orbit and clock estimation by prototype software, and connection method between GPS time and QZSS time.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063223004","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-06-015","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"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"富士通"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"NEC東芝スペースシステム"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fujitsu Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"NEC TOSHIBA Space Systems Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 洋介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沢辺, 幹夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小暮, 聡"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"卯尾, 匡史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yosuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sawabe, Mikio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kogure, Satoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uo, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-16"}],"displaytype":"detail","filename":"63223004.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63223004.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5890/files/63223004.pdf"},"version_id":"a1da2f53-8d00-4d60-a65c-45f3b6723f0f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道時刻推定ソフトウエア","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"時刻同期","subitem_subject_scheme":"Other"},{"subitem_subject":"測位","subitem_subject_scheme":"Other"},{"subitem_subject":"全地球測位システム","subitem_subject_scheme":"Other"},{"subitem_subject":"時計","subitem_subject_scheme":"Other"},{"subitem_subject":"準天頂衛星システム","subitem_subject_scheme":"Other"},{"subitem_subject":"QZSS","subitem_subject_scheme":"Other"},{"subitem_subject":"マスターコントロール実験局","subitem_subject_scheme":"Other"},{"subitem_subject":"MCS","subitem_subject_scheme":"Other"},{"subitem_subject":"エフェメリス","subitem_subject_scheme":"Other"},{"subitem_subject":"時間測定","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星レーザ測距","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit and clock estimation software","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"time synchronization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"positioning","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Global Positioning System","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"clock","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"quasi-zenith satellite system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"QZSS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"master control station","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MCS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ephemeris","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"time measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite laser ranging","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"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":"準天頂衛星システムを利用した高精度測位実験システムにおける高精度軌道時刻推定について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"準天頂衛星システムを利用した高精度測位実験システムにおける高精度軌道時刻推定について"}]},"item_type_id":"5","owner":"1","path":["1019","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5890","relation_version_is_last":true,"title":["準天頂衛星システムを利用した高精度測位実験システムにおける高精度軌道時刻推定について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:06:32.354870+00:00"}