{"created":"2023-06-20T15:04:04.146899+00:00","id":33277,"links":{},"metadata":{"_buckets":{"deposit":"9a4ba423-a9a7-4d1d-b44d-5245fcefc653"},"_deposit":{"created_by":1,"id":"33277","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"33277"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00033277","sets":["1887:1890","1896:1898:1899:1911"]},"author_link":["416033","416035","416036","416031","416037","416040","416039","416038","416030","416029","416032","416034"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"\"Attitude Control Systems of X-Ray Astronomy-Mission Satellites \"\"ASCA(ASTRO-D)\"\" and \"\"ASTRO-E\"\"\""}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"213","bibliographicPageStart":"1","bibliographicVolumeNumber":"121","bibliographic_titles":[{"bibliographic_title":"宇宙科学研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本報告書では,宇宙科学研究所のX線天文観測科学衛星「あすか」および「ASTRO-E」の姿勢(および軌道)制御系について詳述する．これら二つの科学衛星は,その規模(重量,寸法,有能電力等)に於いてかなり異なるにもかかわらず,両者の姿勢制御系は宇宙科学研究所の天文観測衛星のために開発された,独特の多くの特徴を共有している．本報告では,1)ミッション要求を満たすための姿勢(軌道)制御系の機能構成および設計方針,2)姿勢(軌道)制御系機器の構成と性能の概要,3)各制御機能の動作原理(制御則),4)制御系動作実証試験,および5)「あすか」の姿勢制御系に対する軌道上動作･性能の評価,について報告する．本報告書を纏めるに当たり,筆者等は,本報告書が人工衛星,特に天文観測科学衛星の開発や運用に携わるエンジニアにとって,実際を知るための興味深く有用なテキストとなることを願うものである．","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This is an extensive report on the attitude and orbit control systems of the Japanese X-ray astronomical observatories in space; ASCA and ASTRO-E.. ASCA stands for Advanced Spacecraft for Cosmology and Astrophysics, and was called ASTRO-D before the launch by a M-3SII launch vehicle in February 1993, meaning the 4-th X-ray astronomy mission of the Institute of Space and Astronautical Science(ISAS). The launch of ASTRO-E was unsuccessful due to the failure of the M-V rocket in February 2000 (and the mission is to be resurrected in 2005 as ASTRO-EII). In spite of the differences in the scale in weight, size and available power of the two spacecraft, the attitude control systems of the two shared very much common features that were unique to the X-ray space observatories of ISAS. This report describes the details of 1) the design approach and the configuration of the attitude and orbit control systems, 2) the control schemes or laws of the control functions involved, 3) the relevant hardware and software implementations, 4) the ground verificationtest systems and results, and 5) the in-orbit performances of the ASCA's attitude control system. The authors hope that the report could be a text for engineers who might become involved in the development or operation of spacecraft, especially for those for space-based astronomy missions.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0200050000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0285-2853","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00354474","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"NEC東芝スペースシステム（株）"},{"subitem_text_value":"日本電気航空宇宙システム(株）"},{"subitem_text_value":"日本電気航空宇宙システム(株）"},{"subitem_text_value":"日本電気航空宇宙システム(株）"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science (ISAS)"},{"subitem_text_language":"en","subitem_text_value":"NEC TOSHIBA Space Systems, Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems, Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems, Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems, Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"二宮, 敬虔"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 樹明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"前田, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斎藤, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"秋末, 雅彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"玄葉, 麻美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Keiken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Tatsuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maeda, Ken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saitoh, Tetsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Akisue, Masahiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Genba, Asami","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0200050.pdf","filesize":[{"value":"57.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0200050.pdf","url":"https://jaxa.repo.nii.ac.jp/record/33277/files/SA0200050.pdf"},"version_id":"75eb9a1e-25ff-4f95-a8be-03b730e46c44"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"X線天文観測科学衛星「あすか」および「ASTRO-E」の姿勢制御系","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"X線天文観測科学衛星「あすか」および「ASTRO-E」の姿勢制御系"}]},"item_type_id":"9","owner":"1","path":["1890","1911"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"33277","relation_version_is_last":true,"title":["X線天文観測科学衛星「あすか」および「ASTRO-E」の姿勢制御系"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:11:34.175920+00:00"}