{"created":"2023-05-15T08:43:51.042349+00:00","id":8972,"links":{},"metadata":{"_buckets":{"deposit":"1d7adcd1-9e81-4aa6-8251-a2e5ada6e049"},"_deposit":{"created_by":13,"id":"8972","owners":[13],"pid":{"revision_id":0,"type":"depid","value":"8972"},"status":"published"},"_oai":{"id":"oai:uec.repo.nii.ac.jp:00008972","sets":["6"]},"author_link":["24456","24457","24455"],"item_10001_biblio_info_7":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2019-06","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"6","bibliographicPageEnd":"1297","bibliographicPageStart":"1291","bibliographicVolumeNumber":"49","bibliographic_titles":[{},{"bibliographic_title":"IEEE Transactions on Systems, Man, and Cybernetics: Systems","bibliographic_titleLang":"en"}]}]},"item_10001_description_5":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"This correspondence paper presents a framework for practical model construction and stable altitude control of an unmanned aerial vehicle with a parafoil-type wing (UAV-PW). To design a stable controller, we first construct a dynamical longitudinal model of the UAV-PW. Since there exist no aerodynamics data of the parafoil shape in our UAV-PW, aerodynamics coefficients balanced at the trimmed equilibrium are employed. The model accuracy is investigated by comparing the model outputs with the real test flight experimental data. Next, stable controller design conditions for the UAV-PW model with uncertainties are derived in terms of linear matrix inequalities (LMIs). By solving the LMI conditions, we design a stable controller that asymptotically stabilizes the UAV-PW model with the uncertainties on a considered operation domain. The experimental results demonstrate the viability of the model construction and the stable altitude control.","subitem_description_type":"Abstract"}]},"item_10001_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"IEEE"}]},"item_10001_relation_14":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_type":"isVersionOf","subitem_relation_type_id":{"subitem_relation_type_id_text":"10.1109/TSMC.2017.2707393","subitem_relation_type_select":"DOI"}}]},"item_10001_relation_17":{"attribute_name":"関連サイト","attribute_value_mlt":[{"subitem_relation_type_id":{"subitem_relation_type_id_text":"https://doi.org/10.1109/TSMC.2017.2707393","subitem_relation_type_select":"DOI"}}]},"item_10001_rights_15":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"© 2019 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. This is not the published version. Please cite only the published version."}]},"item_10001_source_id_9":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"2168-2216","subitem_source_identifier_type":"ISSN"}]},"item_10001_version_type_20":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_ab4af688f83e57aa","subitem_version_type":"AM"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Tanaka, Motoyasu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wang, Hua O.","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2019-02-18"}],"displaytype":"detail","filename":"Practical Model Construction and Stable Control of an Unmanned Aerial Vehicle With a Parafoil-Type Wing.pdf","filesize":[{"value":"1.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"Practical Model Construction and Stable Control of an Unmanned Aerial Vehicle With a Parafoil-Type Wing","url":"https://uec.repo.nii.ac.jp/record/8972/files/Practical Model Construction and Stable Control of an Unmanned Aerial Vehicle With a Parafoil-Type Wing.pdf"},"version_id":"f69dbd71-37f2-4f23-8159-4468279ff47f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Linear matrix inequality (LMI)","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model construction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stable control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unmanned aerial vehicle with parafoil-type wing (UAV-PW)","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Practical Model Construction and Stable Control of an Unmanned Aerial Vehicle With a Parafoil-Type Wing","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Practical Model Construction and Stable Control of an Unmanned Aerial Vehicle With a Parafoil-Type Wing","subitem_title_language":"en"}]},"item_type_id":"10001","owner":"13","path":["6"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-02-18"},"publish_date":"2019-02-18","publish_status":"0","recid":"8972","relation_version_is_last":true,"title":["Practical Model Construction and Stable Control of an Unmanned Aerial Vehicle With a Parafoil-Type Wing"],"weko_creator_id":"13","weko_shared_id":-1},"updated":"2023-05-15T10:13:26.964890+00:00"}