{"created":"2024-05-13T05:25:01.108016+00:00","id":2000168,"links":{},"metadata":{"_buckets":{"deposit":"5a79df07-9307-4779-9645-f38e1833af97"},"_deposit":{"created_by":14,"id":"2000168","owner":"14","owners":[14],"pid":{"revision_id":0,"type":"depid","value":"2000168"},"status":"published"},"_oai":{"id":"oai:shonan-it.repo.nii.ac.jp:02000168","sets":["1711090862268:1713407023043"]},"author_link":["1873","1874"],"item_10002_biblio_info_7":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-03-31","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1","bibliographicPageEnd":"24","bibliographicPageStart":"19","bibliographicVolumeNumber":"51","bibliographic_titles":[{"bibliographic_title":"湘南工科大学紀要","bibliographic_titleLang":"ja"},{"bibliographic_title":"SHONAN INSTITUTE OF  TECHNOLOGY JOURNAL","bibliographic_titleLang":"en"}]}]},"item_10002_description_5":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論文では宇宙機の離散時間非線形姿勢制御問題について考える．はじめに，制御器設計のための宇宙機の離散時間モデル(Euler近似モデル)を導出する．次に，Euler近似システムの閉ループ系が漸近安定となる離散時間非線形姿勢制御器を設計する．最後に，数値シミュレーションにより提案手法の有効性を検証する．\n\nThis paper considers discrete-time nonlinear control for attitude control problem of spacecraft. To this end, the Euler approximation system is first derived. Then, a discrete-time nonlinear attitude controller so that the closed-loop system of the Euler approximation system is asymptotically stabilized is designed. Finally, the effectiveness of proposed control method is verified by numerical simulations.","subitem_description_type":"Abstract"}]},"item_10002_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"湘南工科大学","subitem_publisher_language":"ja"}]},"item_10002_source_id_11":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10400308","subitem_source_identifier_type":"NCID"}]},"item_10002_source_id_9":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"09192549","subitem_source_identifier_type":"PISSN"}]},"item_10002_version_type_20":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"池田, 裕一","creatorNameLang":"ja"},{"creatorName":"イケダ, ユウイチ","creatorNameLang":"ja-Kana"}],"familyNames":[{"familyName":"池田","familyNameLang":"ja"},{"familyName":"イケダ","familyNameLang":"ja-Kana"}],"givenNames":[{"givenName":"裕一","givenNameLang":"ja"},{"givenName":"ユウイチ","givenNameLang":"ja-Kana"}],"nameIdentifiers":[{"nameIdentifier":"1873","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"IKEDA, Yuichi","creatorNameLang":"en"}],"familyNames":[{"familyName":"IKEDA","familyNameLang":"en"}],"givenNames":[{"givenName":"Yuichi","givenNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"1874","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2024-05-13"}],"displaytype":"detail","filename":"019-024_池田 裕一_宇宙機の離散時間非線形姿勢制御.pdf","filesize":[{"value":"634 KB"}],"format":"application/pdf","licensetype":"license_11","url":{"label":"宇宙機の離散時間非線形姿勢制御","url":"https://shonan-it.repo.nii.ac.jp/record/2000168/files/019-024_池田 裕一_宇宙機の離散時間非線形姿勢制御.pdf"},"version_id":"c4277869-62f8-46ed-9108-d50e60450902"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙機","subitem_subject_language":"ja","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_language":"ja","subitem_subject_scheme":"Other"},{"subitem_subject":"離散時間非線形制御","subitem_subject_language":"ja","subitem_subject_scheme":"Other"},{"subitem_subject":"Spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Discrete-time nonlinear control","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"宇宙機の離散時間非線形姿勢制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"宇宙機の離散時間非線形姿勢制御","subitem_title_language":"ja"},{"subitem_title":"Discrete-time nonlinear attitude control of spacecraft","subitem_title_language":"en"}]},"item_type_id":"10002","owner":"14","path":["1713407023043"],"pubdate":{"attribute_name":"公開日","attribute_value":"2024-05-13"},"publish_date":"2024-05-13","publish_status":"0","recid":"2000168","relation_version_is_last":true,"title":["宇宙機の離散時間非線形姿勢制御"],"weko_creator_id":"14","weko_shared_id":-1},"updated":"2024-05-21T07:03:11.222192+00:00"}