{"created":"2023-06-20T14:40:45.323589+00:00","id":7682,"links":{},"metadata":{"_buckets":{"deposit":"c9d176f7-0551-4a09-91aa-a30514c4205f"},"_deposit":{"created_by":1,"id":"7682","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7682"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007682","sets":["1543:1544:1559","1887:1891"]},"author_link":["41195","41196"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"アクチュエータの方向に制約をもつ宇宙機の位置制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"287","bibliographicPageStart":"284","bibliographic_titles":[{"bibliographic_title":"平成16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 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本稿では宇宙機の位置制御を対象として、スラスタに制約をもつ場合の制御方法について考察する。スラスタが宇宙機のある方向に力を発生できない場合には、宇宙機の姿勢変化を利用して位置制御を行う必要が生じる。ここではこのような場合の宇宙機の位置制御方法について検討を行う。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Position control of spacecraft in the case where thrusters cannot generate forces in a certain direction of the spacecraft is considered in this paper. In this case, the spacecraft attitude change is utilized to change the control force direction in the inertial space. The control method is proposed by using the spacecraft attitude change and its performance is analyzed by the method of averaging. Numerical studies are executed in order to verify the control algorithm of the spacecraft.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897049","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":"三菱電機"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"}]},"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":"山田, 克彦"}],"nameIdentifiers":[{"nameIdentifier":"41195","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yamada, Katsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"41196","nameIdentifierScheme":"WEKO"}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙機制御","subitem_subject_scheme":"Other"},{"subitem_subject":"位置制御","subitem_subject_scheme":"Other"},{"subitem_subject":"制御アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"アクチュエータ","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢変化","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control algorithm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"actuator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude change","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equation of motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"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":"Position control of spacecraft with direction restriction in actuator","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Position control of spacecraft with direction restriction in actuator","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1559","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7682","relation_version_is_last":true,"title":["Position control of spacecraft with direction restriction in actuator"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:35:42.392821+00:00"}