{"created":"2023-06-20T14:39:11.669838+00:00","id":5887,"links":{},"metadata":{"_buckets":{"deposit":"825714fd-c0f6-40bd-8015-4c374b15f477"},"_deposit":{"created_by":1,"id":"5887","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5887"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005887","sets":["1887:1891","9:789:998:1019"]},"author_link":["29051","29052"],"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 space craft of Japan"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"1","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":"1970年2月の我が国初の人工衛星「おおすみ」の打ち上げ以来、数多くの人工衛星、深宇宙探査機が打ち上げられている。これらの衛星・探査機からの軌道決定への要求は、当初は、アンテナで追尾出来れば良いという段階であったが、ミッションが高度化するにつれ、軌道決定への要求精度も、高精度へと移ってきている。本論文では、軌道決定に対する精度要求の推移を、地球周回衛星と、月・惑星探査機とに分けて紹介し、さらにJAXAの軌道決定精度向上の取り組みについて、紹介する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A lot of artificial satellites and deep space probes have been launched, since OHSUMI that is the first Japanese artificial satellite was launched in February 1970. As for the first time, it was the requirements for orbit determination that the satellites can be tracked by the antennas of the ground stations. But the accuracy requirements for orbit determination have been changing to high accuracy as missions advance. In this paper, I explain about the change of the accuracy requirements for orbit determination and about dealing with the accuracy improvement for orbit determination.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063223001","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":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"加藤, 隆二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Takaji","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":"63223001.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63223001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5887/files/63223001.pdf"},"version_id":"2b8855f7-6116-433c-9483-d8c5ba219cde"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"精度要求","subitem_subject_scheme":"Other"},{"subitem_subject":"日本宇宙プログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"精度","subitem_subject_scheme":"Other"},{"subitem_subject":"スイングバイ技術","subitem_subject_scheme":"Other"},{"subitem_subject":"サンプルリターンミション","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"月重力","subitem_subject_scheme":"Other"},{"subitem_subject":"超長距離干渉計","subitem_subject_scheme":"Other"},{"subitem_subject":"みどり","subitem_subject_scheme":"Other"},{"subitem_subject":"だいち","subitem_subject_scheme":"Other"},{"subitem_subject":"さきがけ","subitem_subject_scheme":"Other"},{"subitem_subject":"すいせい","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accuracy requirement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Japanese space program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swingby technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sample return mission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar gravitation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"very long base interferometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Midori","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Daichi","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Sakigake","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Suisei","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":"日本の人工衛星・宇宙探査機の軌道決定について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"日本の人工衛星・宇宙探査機の軌道決定について"}]},"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":"5887","relation_version_is_last":true,"title":["日本の人工衛星・宇宙探査機の軌道決定について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:06:35.894513+00:00"}