{"created":"2023-06-20T14:40:28.309780+00:00","id":7356,"links":{},"metadata":{"_buckets":{"deposit":"6f5aff48-7e19-4e24-b5a0-412012854c6a"},"_deposit":{"created_by":1,"id":"7356","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7356"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007356","sets":["1543:1544:1554","1887:1891"]},"author_link":["38928"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"321","bibliographicPageStart":"314","bibliographicVolumeNumber":"2009","bibliographic_titles":[{"bibliographic_title":"アストロダイナミクスシンポジウム講演後刷り集"},{"bibliographic_title":"Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部))","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The paper presents the Kalman Filter (KF) adaptation of the Tanygin-Shuster (T-S) weighted least-squares algorithm for spin-axis attitude determination. This KF method is suitable for sequential real-time applications. The iteration procedure which led to the unit-vector normalization in the least-squares version of the T-S algorithm has been modified for the sequential approach presented here. This iteration is beneficial for the stability of the attitude determination results. The benefit of the unit-vector normalization has been demonstrated on the basis of real sensor data from the CONTOUR satellite.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064734051","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宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11567475","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"九州大学大学院工学府航空宇宙工学専攻"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyushu University"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"van, der Ha  Jozef C.","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Spinning Satellites","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Attitude Determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalman Filter","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"KALMAN FILTER FOR SPIN-AXIS ATTITUDE ESTIMATION","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"KALMAN FILTER FOR SPIN-AXIS ATTITUDE ESTIMATION","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1554","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7356","relation_version_is_last":true,"title":["KALMAN FILTER FOR SPIN-AXIS ATTITUDE ESTIMATION"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:40:47.153316+00:00"}