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Interaction between a Fault-tolerant Flight Control System using Simple Adaptive Control and Pilot's Pitch Control
http://hdl.handle.net/2261/00075007
http://hdl.handle.net/2261/0007500771ca0701-9b74-4ecc-a134-617739714c37
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
Takase-Entzinger-Suzuki_ASCC_2017.pdf (2.0 MB)
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| Item type | 会議発表論文 / Conference Paper(1) | |||||
|---|---|---|---|---|---|---|
| 公開日 | 2018-08-28 | |||||
| タイトル | ||||||
| タイトル | Interaction between a Fault-tolerant Flight Control System using Simple Adaptive Control and Pilot's Pitch Control | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Simple Adaptive Control | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Fault-tolerant Flight Control | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Human Pilot | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Manual Control | |||||
| 資源タイプ | ||||||
| 資源 | http://purl.org/coar/resource_type/c_5794 | |||||
| タイプ | conference paper | |||||
| 著者 |
Takase, Ryoichi
× Takase, Ryoichi× Entzinger, Jorg Onno× Suzuki, Shinji |
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| 著者別名 | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 148073 | |||||
| 姓名 | 高瀬, 諒一 | |||||
| 著者別名 | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 148074 | |||||
| 姓名 | エントジンガー, ヨルグ オノ | |||||
| 著者別名 | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 148075 | |||||
| 姓名 | 鈴木, 真二 | |||||
| 著者所属 | ||||||
| 著者所属 | Department of Aeronautics and Astronautics, The University of Tokyo | |||||
| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | This paper deals with a fault-tolerant flight control system where the aircraft is manually controlled by pilots. Our previous research demonstrated that Simple Adaptive Control (SAC) with a PID compensator could automatically control an aircraft even after the dynamic characteristics change due to aircraft damage only under predetermined desired value. Now we focus on the interaction between the pilot’s input and the adaptive controller. In this paper, we installed the adaptive controller in the flight simulator in order to check the basic performance of the developed system and the interaction in landing phases between the pilot’s control input and the adaptive controller. | |||||
| 内容記述 | ||||||
| 内容記述タイプ | Other | |||||
| 内容記述 | 2017 11th Asian Control Conference (ASCC), Gold Coast Convention Centre, Australia, 17-20 December 2017 | |||||
| 書誌情報 | 発行日 2017 | |||||
| DOI | ||||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | info:doi/10.1109/ASCC.2017.8287222 | |||||
| 権利 | ||||||
| 権利情報 | © © 2017 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. | |||||
| 著者版フラグ | ||||||
| 値 | author | |||||
| 出版者 | ||||||
| 出版者 | IEEE | |||||
| 異版である | ||||||
| 関連タイプ | isVersionOf | |||||
| 識別子タイプ | URI | |||||
| 関連識別子 | https://doi.org/10.1109/ASCC.2017.8287222 | |||||
