{"created":"2023-06-20T14:40:40.711821+00:00","id":7597,"links":{},"metadata":{"_buckets":{"deposit":"a2292401-fd56-4f58-8fd7-13ad66144b0b"},"_deposit":{"created_by":1,"id":"7597","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7597"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007597","sets":["1543:1544:1558","1887:1891"]},"author_link":["40675","40678","40679","40674","40677","40676"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"20kg級超小型衛星の迅速姿勢制御用CMGシステムの設計と試作"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"209","bibliographicPageStart":"204","bibliographic_titles":[{"bibliographic_title":"第15回アストロダイナミクスシンポジウム講演後刷り集　2005"},{"bibliographic_title":"Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"小型衛星が持つ迅速姿勢制御の可能性をさらに強化するための姿勢制御装置として、コントロールモーメントジャイロ(CMG: Control Moment Gyro)を採用し、小型化に関する定量的な検討、および駆動則の設計を行った。20kg級超小型衛星による突発的な天文現象観測ミッションへの応用を目指し、ピラミッド型CMGクラスタの試験モデルを開発し、3次元姿勢動力学シミュレータを用いて地上実験を行った。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For the agile maneuver missions of micro-satellites, Control Moment Gyros (CMGs) will meet the necessary requirements because a small gimbal torque input produces a large torque output. However, CMG has some difficulties in designing and control algorithm. Here, a simplified method to calculate appropriate output torque for 20 kg class astronomy satellite is introduced and experimentally evaluated using a test model of pyramid cluster of 4 CMGs and a 3-DOF (Degree Of Freedom) attitude dynamics simulator.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480032","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/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"},{"subitem_text_value":"東京工業大学 大学院理工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School of Science and Engineering"}]},"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":"尾曲, 邦之"}],"nameIdentifiers":[{"nameIdentifier":"40674","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"臼田, 武史"}],"nameIdentifiers":[{"nameIdentifier":"40675","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"松永, 三郎"}],"nameIdentifiers":[{"nameIdentifier":"40676","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Omagari, Kuniyuki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"40677","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Usuda, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"40678","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Matsunaga, Saburo","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"40679","nameIdentifierScheme":"WEKO"}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"コントロールモーメントジャイロ","subitem_subject_scheme":"Other"},{"subitem_subject":"CMG","subitem_subject_scheme":"Other"},{"subitem_subject":"可変速度CMG","subitem_subject_scheme":"Other"},{"subitem_subject":"VS-CMG","subitem_subject_scheme":"Other"},{"subitem_subject":"小型化","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"超小型衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"ジャイロスコープ","subitem_subject_scheme":"Other"},{"subitem_subject":"リアクションホイール","subitem_subject_scheme":"Other"},{"subitem_subject":"ジンバル","subitem_subject_scheme":"Other"},{"subitem_subject":"制御系設計","subitem_subject_scheme":"Other"},{"subitem_subject":"光ファイバジャイロ","subitem_subject_scheme":"Other"},{"subitem_subject":"地上実験","subitem_subject_scheme":"Other"},{"subitem_subject":"制御シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"control moment gyro","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CMG","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Variable Speed CMG","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"VS-CMG","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"miniaturization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microsatellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gyroscope","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction wheel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gimbal","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control system design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fiber optic gyro","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control simulation","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":"Design and functional model of CMG system for agile attitude maneuver of 20 kg-class microsatellite","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Design and functional model of CMG system for agile attitude maneuver of 20 kg-class microsatellite","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1558","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7597","relation_version_is_last":true,"title":["Design and functional model of CMG system for agile attitude maneuver of 20 kg-class microsatellite"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:37:02.456798+00:00"}