ログイン
言語:

WEKO3

  • トップ
  • コミュニティ
  • ランキング
AND
To
lat lon distance
To

Field does not validate



インデックスリンク

インデックスツリー

メールアドレスを入力してください。

WEKO

One fine body…

WEKO

One fine body…

アイテム

{"_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_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}
  1. B200 工学部/工学研究科
  2. B200e 会議資料
  3. 国際会議

Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data

http://hdl.handle.net/2237/14420
4d7210b7-f56a-4e29-991e-651069dff052
名前 / ファイル ライセンス アクション
SiceAnnualConf.pdf SiceAnnualConf.pdf (299.9 kB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2010-12-21
タイトル
タイトル Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data
著者 Yamato, Yuhei

× Yamato, Yuhei

WEKO 39423

Yamato, Yuhei

Search repository
Sakamoto, Noboru

× Sakamoto, Noboru

WEKO 39424

Sakamoto, Noboru

Search repository
Takahama, Morio

× Takahama, Morio

WEKO 39425

Takahama, Morio

Search repository
権利
権利情報 Copyright © 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’s 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.
キーワード
主題Scheme Other
主題 Nonlinear Control
キーワード
主題Scheme Other
主題 Flight Control
キーワード
主題Scheme Other
主題 High Angle of Attack
抄録
内容記述 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.
内容記述タイプ Abstract
出版者
出版者 Institute of Electrical and Electronics Engineers
言語
言語 eng
資源タイプ
資源タイプresource http://purl.org/coar/resource_type/c_6501
タイプ journal article
ISBN
関連識別子
識別子タイプ ISBN
関連識別子 978-4-907764-34-0
書誌情報 ICCAS-SICE 2009

p. 1806-1811, 発行日 2009-08
著者版フラグ
値 publisher
URI
識別子 http://hdl.handle.net/2237/14420
識別子タイプ HDL
戻る
0
views
See details
Views

Versions

Ver.1 2021-03-01 18:51:22.431220
Show All versions

Share

Mendeley CiteULike Twitter Facebook Print Addthis

Cite as

Export

OAI-PMH
  • OAI-PMH JPCOAR
  • OAI-PMH DublinCore
  • OAI-PMH DDI
Other Formats
  • JSON
  • BIBTEX

Confirm


Powered by CERN Data Centre & Invenio


Powered by CERN Data Centre & Invenio