{"created":"2023-06-20T14:39:12.177772+00:00","id":5898,"links":{},"metadata":{"_buckets":{"deposit":"26c98163-19f6-48e7-9a7d-424a1a759ce2"},"_deposit":{"created_by":1,"id":"5898","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5898"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005898","sets":["1887:1891","9:789:998:1019"]},"author_link":["29142","29141","29143","29144","29140","29139"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Orbit determination method using radio interferometry of small-diameter antennas for LEO satellites"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"84","bibliographicPageStart":"77","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":"本研究では、2台のアンテナで構成する小口径電波干渉計を用いて、到達時刻差に起因する到来電波の「位相差」を観測し、軌道決定のアルゴリズム、および必要な機器構成を検討すると共に、その軌道決定能力を評価した。事例研究として、鹿児島大学理学部が所有する1.4m口径のパラボラアンテナ2台で構成する電波干渉計(基線長76m)を用いて、低高度地球周回群衛星であるGlobalstarの一部の衛星を対象として実観測を実施した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper, using the radio interferometry of two small-dish antennas, the phase difference of arrival radio caused by the arrival time delay was observed. The algorithm of orbit determination and the required facilities are considered and the performance of method was verified. There is the 76-m baseline radio interferometry of two 1.4-m parabola antennas in the Faculty of Science, Kagoshima University. In the case study, using this facility, the one of Globalstar satellites, which is LEO (Low Earth Orbit) clustered satellite system, was observed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063223012","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":"東北大学"},{"subitem_text_value":"鹿児島大学"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Kagoshima University"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"坂本, 祐二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西尾, 正則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高野, 忠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakamoto, Yuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishio, Masanori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takano, Tadashi","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":"63223012.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63223012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5898/files/63223012.pdf"},"version_id":"ee2b6d1e-4ab9-4fc0-b024-b973c8f4af33"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"電波干渉計","subitem_subject_scheme":"Other"},{"subitem_subject":"超長距離干渉計","subitem_subject_scheme":"Other"},{"subitem_subject":"低高度地球軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"Globalstar衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"群衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"位相差変化率","subitem_subject_scheme":"Other"},{"subitem_subject":"移相","subitem_subject_scheme":"Other"},{"subitem_subject":"状態推定","subitem_subject_scheme":"Other"},{"subitem_subject":"アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"radio interferometer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"very long base interferometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low Earth orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Globalstar satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"clustered satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"phase difference rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"phase shift","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"state estimation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"algorithm","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":"小口径電波干渉計による低高度地球周回衛星の軌道決定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小口径電波干渉計による低高度地球周回衛星の軌道決定"}]},"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":"5898","relation_version_is_last":true,"title":["小口径電波干渉計による低高度地球周回衛星の軌道決定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:06:23.176068+00:00"}