{"created":"2023-06-20T14:40:47.494434+00:00","id":7731,"links":{},"metadata":{"_buckets":{"deposit":"46b29cd7-0105-40e3-ae36-0dbdc6eaaf91"},"_deposit":{"created_by":1,"id":"7731","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7731"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007731","sets":["1543:1544:1560","1887:1891"]},"author_link":["41542","41546","41541","41543","41544","41545"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"2つの剛体からなる宇宙機の姿勢制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"191","bibliographicPageStart":"186","bibliographic_titles":[{"bibliographic_title":"平成15年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本研究では、3回転自由度を持つ関節で繋がれた2つの剛体からなる宇宙機の姿勢制御問題を取り扱う。外力が加わらず、系の全角運動量が零に保たれる場合、この宇宙機の姿勢は関節の回転運動によって制御することが可能であり、システムは6状態3入力の非ホロノミックシステムとして定式化される。このシステムに対して、リャプノフ法にもとづく不連続状態フィードバック制御則を提案する。提案則によって、宇宙機の姿勢はほとんどすべての初期姿勢から目標姿勢へと収束する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper deals with an attitude control of a spacecraft which consists of two rigid bodies coupled by a ball and socket joint. When the angular momentum of the spacecraft is zero, the attitude can be controlled by rotation of the joint angles. The system is expressed as a 6-state 3-input nonholonomic system, and a time-invariant discontinuous feedback controller for the system is designed based on Liapunov control. The designed controller makes the attitude of the spacecraft converge to the desired one from almost all initial attitude.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652030","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_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"神戸大学 工学部　情報知能工学科"},{"subitem_text_value":"京都大学 大学院工学研究科"},{"subitem_text_value":"神戸大学 工学部　情報知能工学科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kobe University Department of Computer and Systems Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyoto University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kobe University Department of Computer and Systems Engineering, Faculty of 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":"浦久保, 孝光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"土屋, 和雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"多田, 幸生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Urakubo, Takateru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuchiya, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tada, Yukio","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Liapunov関数","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"剛体構造","subitem_subject_scheme":"Other"},{"subitem_subject":"角運動量","subitem_subject_scheme":"Other"},{"subitem_subject":"フィードバック制御","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"内部運動","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"Liapunov function","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rigid structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular momentum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"feedback control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical 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":"Attitude control of a spacecraft composed of two rigid bodies using internal motion","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Attitude control of a spacecraft composed of two rigid bodies using internal motion","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1560","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7731","relation_version_is_last":true,"title":["Attitude control of a spacecraft composed of two rigid bodies using internal motion"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:56.024203+00:00"}