{"_buckets": {"deposit": "0bbe6558-c331-45ad-affa-2e4811b7548b"}, "_deposit": {"id": "12536", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "12536"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00012536"}, "item_10_biblio_info_6": {"attribute_name": "\u66f8\u8a8c\u60c5\u5831", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2009-08", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "1811", "bibliographicPageStart": "1806", "bibliographic_titles": [{"bibliographic_title": "ICCAS-SICE 2009"}]}]}, "item_10_description_4": {"attribute_name": "\u6284\u9332", "attribute_value_mlt": [{"subitem_description": "In this paper, a stabilization problem for an aircraft at a high angle of attack is considered. Though aircrafts obtain large lift force over the high angle of attack regime, nonlinearities of aerodynamics over the regime are considerably high. Using aerodynamic coeffients data given as a table, we design a nonlinear optimal control law to stabilize an existing aircraft at a high angle of attack by a new method based on stable manifold theory. As a result, the nonlinear optimal control law stabilizes attitudes of the aircraft in a larger region than the linear optimal control does.", "subitem_description_type": "Abstract"}]}, "item_10_identifier_60": {"attribute_name": "URI", "attribute_value_mlt": [{"subitem_identifier_type": "HDL", "subitem_identifier_uri": "http://hdl.handle.net/2237/14420"}]}, "item_10_publisher_32": {"attribute_name": "\u51fa\u7248\u8005", "attribute_value_mlt": [{"subitem_publisher": "Institute of Electrical and Electronics Engineers"}]}, "item_10_relation_8": {"attribute_name": "ISBN", "attribute_value_mlt": [{"subitem_relation_type_id": {"subitem_relation_type_id_text": "978-4-907764-34-0", "subitem_relation_type_select": "ISBN"}}]}, "item_10_rights_12": {"attribute_name": "\u6a29\u5229", "attribute_value_mlt": [{"subitem_rights": "Copyright \u00a9 2009 IEEE. Reprinted from (relevant publication info). This material is posted here with permission of the IEEE. Such permission of the IEEE does not in any way imply IEEE endorsement of any of Nagoya University\u2019s products or services. Internal or personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution must be obtained from the IEEE by writing to pubs-permissions@ieee.org."}]}, "item_10_select_15": {"attribute_name": "\u8457\u8005\u7248\u30d5\u30e9\u30b0", "attribute_value_mlt": [{"subitem_select_item": "publisher"}]}, "item_creator": {"attribute_name": "\u8457\u8005", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "Yamato, Yuhei"}], "nameIdentifiers": [{"nameIdentifier": "39423", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sakamoto, Noboru"}], "nameIdentifiers": [{"nameIdentifier": "39424", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Takahama, Morio"}], "nameIdentifiers": [{"nameIdentifier": "39425", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "\u30d5\u30a1\u30a4\u30eb\u60c5\u5831", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2018-02-20"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "SiceAnnualConf.pdf", "filesize": [{"value": "299.9 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 299900.0, "url": {"label": "SiceAnnualConf.pdf", "url": "https://nagoya.repo.nii.ac.jp/record/12536/files/SiceAnnualConf.pdf"}, "version_id": "4a14d52b-ff6e-4517-8868-d10375353a11"}]}, "item_keyword": {"attribute_name": "\u30ad\u30fc\u30ef\u30fc\u30c9", "attribute_value_mlt": [{"subitem_subject": "Nonlinear Control", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Flight Control", "subitem_subject_scheme": "Other"}, {"subitem_subject": "High Angle of Attack", "subitem_subject_scheme": "Other"}]}, "item_language": {"attribute_name": "\u8a00\u8a9e", "attribute_value_mlt": [{"subitem_language": "eng"}]}, "item_resource_type": {"attribute_name": "\u8cc7\u6e90\u30bf\u30a4\u30d7", "attribute_value_mlt": [{"resourcetype": "journal article", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data", "item_titles": {"attribute_name": "\u30bf\u30a4\u30c8\u30eb", "attribute_value_mlt": [{"subitem_title": "Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data"}]}, "item_type_id": "10", "owner": "1", "path": ["320/502/503"], "permalink_uri": "http://hdl.handle.net/2237/14420", "pubdate": {"attribute_name": "\u516c\u958b\u65e5", "attribute_name_i18n": "\u516c\u958b\u65e5", "attribute_value": "2010-12-21"}, "publish_date": "2010-12-21", "publish_status": "0", "recid": "12536", "relation": {}, "relation_version_is_last": true, "title": ["Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data"], "weko_shared_id": null}