{"created":"2023-06-20T14:39:12.073529+00:00","id":5896,"links":{},"metadata":{"_buckets":{"deposit":"790e53d7-32e9-4a12-bc79-b636d2c62ac3"},"_deposit":{"created_by":1,"id":"5896","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5896"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005896","sets":["1887:1891","9:789:998:1019"]},"author_link":["29133","29127","29130","29123","29129","29134","29132","29124","29125","29128","29126","29131"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The Real Time Trajectory Estimation Program (RTEP): Overview and experience results"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"68","bibliographicPageStart":"59","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_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Real Time Trajectory Estimation Program (RTEP) is JAXA's system for estimating a satellite's trajectory and thrust acceleration based on the Kalman filter during the Apogee Engine Firing (AEF). RTEP has been used during the AEFs of, ETS (Engineering Test Satellite)-6 (1994), COMETS (Communications and broadcasting Engineering Test Satellite) (1998), DRTS (Data Relay Test Satellite) (2002), OICETS (Optical Inter-orbit Communications Engineering Test Satellite) (2005) and ALOS (Advanced Land Observing Satellite) (2006). This paper presents the overview of RTEP, the results of the estimation using Space network data.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063223010","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":"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":"宇宙航空研究開発機構"},{"subitem_text_value":"三菱スペース・ソフトウエア"},{"subitem_text_value":"三菱スペース・ソフトウエア"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"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"},{"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":"Mitsubishi Space Software Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小川, 美奈"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩名, 泰典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷口, 正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中嶋, 憲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"堀田, 学"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"広田, 正夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Mina","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwana, Yasunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Taniguchi, Sho","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakajima, Ken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hotta, Manabu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirota, Masao","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":"63223010.pdf","filesize":[{"value":"3.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63223010.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5896/files/63223010.pdf"},"version_id":"fe476baf-407d-4c46-9833-2b8da556042a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道解析","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道位置推定","subitem_subject_scheme":"Other"},{"subitem_subject":"カルマンフィルタ","subitem_subject_scheme":"Other"},{"subitem_subject":"推定","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"実時間軌道推定","subitem_subject_scheme":"Other"},{"subitem_subject":"RTEP","subitem_subject_scheme":"Other"},{"subitem_subject":"アポジーエンジン点火","subitem_subject_scheme":"Other"},{"subitem_subject":"AEF","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星追跡","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"ペリジー","subitem_subject_scheme":"Other"},{"subitem_subject":"位置誤差","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital position estimation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalman filter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"estimating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real time trajectory estimation program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RTEP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"apogee engine firing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AEF","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite tracking","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"perigee","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position error","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":"地球周回衛星の実時間軌道推定:概要と成果","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"地球周回衛星の実時間軌道推定:概要と成果"}]},"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":"5896","relation_version_is_last":true,"title":["地球周回衛星の実時間軌道推定:概要と成果"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:06:25.225907+00:00"}