{"created":"2023-06-20T14:39:12.264770+00:00","id":5900,"links":{},"metadata":{"_buckets":{"deposit":"93e0fb97-f44b-4685-a5a1-ae515054c75d"},"_deposit":{"created_by":1,"id":"5900","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5900"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005900","sets":["1887:1891","9:789:998:1019"]},"author_link":["29153","29167","29168","29162","29157","29155","29158","29154","29165","29161","29163","29159","29160","29156","29166","29164"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Orbit determination of earth orbiter using 4-way tracking data and application to lunar orbiter"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"96","bibliographicPageStart":"91","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":"宇宙航空研究開発機構(JAXA)は、データ中継技術衛星DRTS経由で計測した衛星間測距データ(4-way追跡データ)を用いて、軌道決定技術の実証実験を行っている。本論文では、4way追跡データを用いた地球周回衛星の軌道決定実験の主要な成果を報告する。また、2007年打ち上げ予定の月周回衛星(SELENE)では、月を周回する小型衛星経由で月裏側の4-wayドップラを取得する計画である。4-wayドップラがSELENE軌道決定・予報精度に与える影響についても紹介する。","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 been studying the feasibility of orbit determination technology with satellite-to-satellite (four-way) tracking data using the DRTS (Date Relay Test Satellite) which was launched in 2002. The orbit determination was performed in batch processing mode, and showed that the accuracy level is equivalent to the results by tracking data from ground network stations. This paper presents the overview of JAXA's experiments on orbit determination using four-way tracking data of the DRTS user satellites such as the ADEOS (Advance Earth Observing Satellite)-2 and the ALOS (Advanced Land Observing Satellite). The application of this technologies to the SELENE (SELenological and Engineering Explorer) orbiting the moon is also presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063223014","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 宇宙基幹システム本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙基幹システム本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙基幹システム本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙基幹システム本部"},{"subitem_text_value":"富士通"},{"subitem_text_value":"富士通"},{"subitem_text_value":"大興電子通信"},{"subitem_text_value":"国立天文台"}]},"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 Office of Space Flight and Operations"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Office of Space Flight and Operations"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Office of Space Flight and Operations"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Office of Space Flight and Operations"},{"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":"Daiko Denshi Tsushin Ltd."},{"subitem_text_language":"en","subitem_text_value":"National Astronomical Observatory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小川, 美奈"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷口, 正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩名, 泰典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斉藤, 正敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"片桐, 征治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青島, 千晶"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小井沼, 久哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SELENE RSAT/VRADミッショングループ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Mina","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Taniguchi, Sho","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwana, Yasunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Masatoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Katagiri, Seiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoshima, Chiaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koinuma, Hisaya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SELENE RSAT/VRAD Mission Group","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":"63223014.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63223014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5900/files/63223014.pdf"},"version_id":"8111a3b4-ef46-40da-a11c-574a4d5cbd62"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"位置誤差","subitem_subject_scheme":"Other"},{"subitem_subject":"技術試験衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"予測","subitem_subject_scheme":"Other"},{"subitem_subject":"精度","subitem_subject_scheme":"Other"},{"subitem_subject":"データ中継技術衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星間追跡データ","subitem_subject_scheme":"Other"},{"subitem_subject":"4-way追跡データ","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星間通信","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星追跡","subitem_subject_scheme":"Other"},{"subitem_subject":"ドップラー効果","subitem_subject_scheme":"Other"},{"subitem_subject":"月周回衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"月の裏側","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position error","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Engineering Test Satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"prediction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"data relay test satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite-to-satellite tracking data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"4-way tracking data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"intersatellite communication","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite tracking","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Doppler effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar orbiter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar far side","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4-way軌道決定の現状と、月周回衛星への応用","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"地球周回衛星の4-way軌道決定の現状と、月周回衛星への応用"}]},"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":"5900","relation_version_is_last":true,"title":["地球周回衛星の4-way軌道決定の現状と、月周回衛星への応用"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:42:13.965944+00:00"}