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Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data
http://hdl.handle.net/2237/14420
http://hdl.handle.net/2237/144204d7210b7-f56a-4e29-991e-651069dff052
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SiceAnnualConf.pdf (299.9 kB)
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| 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 | |||||
| 言語 | en | |||||
| 著者 |
Yamato, Yuhei
× Yamato, Yuhei× Sakamoto, Noboru× Takahama, Morio |
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| アクセス権 | ||||||
| アクセス権 | open access | |||||
| アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||
| 権利 | ||||||
| 言語 | en | |||||
| 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 | ||||||
| 内容記述タイプ | Abstract | |||||
| 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. | |||||
| 言語 | en | |||||
| 出版者 | ||||||
| 出版者 | Institute of Electrical and Electronics Engineers | |||||
| 言語 | en | |||||
| 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 | |||||
| 出版タイプ | ||||||
| 出版タイプ | VoR | |||||
| 出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
| ISBN | ||||||
| 関連タイプ | isPartOf | |||||
| 識別子タイプ | ISBN | |||||
| 関連識別子 | 978-4-907764-34-0 | |||||
| 書誌情報 |
en : ICCAS-SICE 2009 p. 1806-1811, 発行日 2009-08 |
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| 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 | |||||
