{"created":"2023-06-20T15:02:14.391602+00:00","id":31327,"links":{},"metadata":{"_buckets":{"deposit":"ebc88341-a65d-4982-92e4-f5c13d19891b"},"_deposit":{"created_by":1,"id":"31327","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31327"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031327","sets":["1887:1890","1896:1898:1899:1991"]},"author_link":["404009","404010","404008","404007"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1988-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"136","bibliographicPageStart":"127","bibliographicVolumeNumber":"6","bibliographic_titles":[{},{"bibliographic_title":"The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1987","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper deals with an influence of the magnetically suspended rotor on the satellite motion; although cross-feedbacks in the magnetic bearing provide stability margin to the rotor gyroscopic motion, they may destabilize the satellite nutation. Stability analyses about the dynamical interaction between the satellite and the magnetically suspended rotor whose controller used three types of (proportional, integral and derivative) cross-feedbacks were performed. The results indicated that they had significant effects on the rotor and the satellite motion.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0033596000","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":"0288-433X","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":"AA10455137","subitem_source_identifier_type":"NCID"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"INOUE, Masao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TSUCHIYA, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAJIMA, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MURAKAMI, Chikara","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0033596.pdf","filesize":[{"value":"453.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0033596.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31327/files/SA0033596.pdf"},"version_id":"43e6ecff-b4b6-404a-95ea-45740bee6573"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Nutational Stability of a Satellite Equipped with an Active Magnetic Momentum Wheel","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Nutational Stability of a Satellite Equipped with an Active Magnetic Momentum Wheel","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1991"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31327","relation_version_is_last":true,"title":["Nutational Stability of a Satellite Equipped with an Active Magnetic Momentum Wheel"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T01:03:20.549390+00:00"}