{"created":"2023-06-20T14:40:25.137971+00:00","id":7297,"links":{},"metadata":{"_buckets":{"deposit":"2f9f854e-2b06-4395-aa3f-2f95c5dc9ad3"},"_deposit":{"created_by":1,"id":"7297","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7297"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007297","sets":["1543:1544:1553","1887:1891"]},"author_link":["38559","38558","38556","38557"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"超小型衛星用リアクションホイールの擾乱抑制に関する研究"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"311","bibliographicPageStart":"307","bibliographicVolumeNumber":"20","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":"The 20th 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":"第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県　","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":"The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"摘要: かつて教育目的で開発されてきた超小型衛星にも現在では高精度な姿勢制御が要求されるミッションが提案され始めている．一般に高精度な安定度を要求する衛星にはアクチュエータとしてリアクションホイールが搭載されるが，リアクションホイール自身が衛星の主要な内部擾乱源となることも知られている．そのため，リアクションホイールには姿勢制御トルクを発生させつつ，擾乱の発生を抑制することが求められている．本研究の目的はリアクションホイールが自身で発生する擾乱を抑制するホイール制御則の提案である．本講演ではリアクションホイールが発生する擾乱のモデル化を行い，リアクションホイールの擾乱測定結果と比較し，モデルが妥当であるかについて述べる．","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Development of microsatellites by universities and organizations advances so increasingly that the higher attitude control such as pointing accuracy and stability is getting required for even their microsatellites being engaged in complicated space missions. Reaction wheel is widely used as an actuator in the space missions, however, it causes serious disturbance against the attitude control. It indicates that reaction wheel should also suppress generation of the disturbance for achieving precise attitude control. The purpose of this study is to analyze reaction wheel disturbance and to propose a new control rule for reaction wheel in consideration of the disturbance suppression on attitude control of microsatellite.","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: AA0065115050","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所 (JAXA)(ISAS)"}]},"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)(ISAS)"}]},"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":"首都大学東京"},{"subitem_text_value":"首都大学東京"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan 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":"寅谷, 敬紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐原, 宏典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Toraya, Takanori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sahara, Hironori","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Attitude Stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Disturbance Suppression","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reaction Wheel","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":"A Study on Disturbance Suppression of Reaction Wheel for Microsatellite","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A Study on Disturbance Suppression of Reaction Wheel for Microsatellite","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1553","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7297","relation_version_is_last":true,"title":["A Study on Disturbance Suppression of Reaction Wheel for Microsatellite"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:41:41.382968+00:00"}