{"created":"2023-06-20T14:39:33.832463+00:00","id":6307,"links":{},"metadata":{"_buckets":{"deposit":"4d2be5b3-ddfb-4016-b913-3ad81885ff68"},"_deposit":{"created_by":1,"id":"6307","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6307"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006307","sets":["1887:1893","9:789:1031:1060"]},"author_link":["31893","31894","31892","31891"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The development of high-reliable Inertial Reference Unit: Project support"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-01-20","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"256","bibliographicPageStart":"253","bibliographicVolumeNumber":"JAXA-SP-05-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術"},{"bibliographic_title":"JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Japan Aerospace Exploration Agency (JAXA), formerly named as National Space Development Agency (NASDA), developed Tuned Dry Gyroscope (TDG), as supreme precision rate sensor for satellite attitude control. JAXA also developed Inertial Reference Unit (IRU) using TDG. This IRU is used on almost every JAXA satellite. It has passed about fifteen years since the development. It is difficult to purchase some kind of electronics parts nowadays. Meanwhile, satellite system requires higher accuracy, more operation flexibility and so on. So, we decided to redesign IRU. Aiming is high-reliability and high-accuracy. The study has started in FY 2001. In FY 2003 IRU redesign was completed and we prepared every document needed. In FY 2004, we built an Engineering Model and qualify its function and performance. In FY 2005, we will complete this study.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049054051","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-05-008","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_3_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 Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"里, 誠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川井, 洋志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawai, Hiroshi","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":"49054051.pdf","filesize":[{"value":"624.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49054051.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6307/files/49054051.pdf"},"version_id":"48df61d7-6423-459e-b79a-0e6cd0350ee5"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"チューンドドライジャイロ","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"部品信頼性","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性基準装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ダイナミックレンジ","subitem_subject_scheme":"Other"},{"subitem_subject":"VFコンバータ","subitem_subject_scheme":"Other"},{"subitem_subject":"高精度","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機電子機器","subitem_subject_scheme":"Other"},{"subitem_subject":"性能試験","subitem_subject_scheme":"Other"},{"subitem_subject":"tuned dry gyro","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"component reliability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial reference unit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic range","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"VF converter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft electronic equipment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance test","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"IRUの高信頼性化の研究:プロジェクトの支援","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"IRUの高信頼性化の研究:プロジェクトの支援"}]},"item_type_id":"3","owner":"1","path":["1060","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6307","relation_version_is_last":true,"title":["IRUの高信頼性化の研究:プロジェクトの支援"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:58:03.516192+00:00"}