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有限整定時間制御における過渡特性の改善
https://jaxa.repo.nii.ac.jp/records/45081
https://jaxa.repo.nii.ac.jp/records/450816cbc0751-6a22-4d80-915a-9d0153108ada
名前 / ファイル | ライセンス | アクション |
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naltr00823.pdf (1.1 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 有限整定時間制御における過渡特性の改善 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Improvement of the Transient Response in the Finite Settling Time Control | |||||
著者 |
佐々, 修一
× 佐々, 修一× 渡辺, 顯× SASA, Shuichi× WATANABE, Akira |
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著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-823 巻 823, p. 13, 発行日 1984-07 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the finite settling-time control or dead-beat control, there are some systems that do not have good transient response. We apply the optimal control theory to the dead-beat control of a single input/single output system to improve the transient response. Two solutions are derived ; one is an open-loop solution, and the other is a state feedback solution. The state feedback solution is obtained by the application of the principle of optimality, and the feedback gains are partly time dependent. The characteristics of the optimal response are shown. Also the effect of the system parameter deviation from the original system and the effect of the state disturbance are examined, and it is found that this control low is robust in both cases. This method is applied to a higher order system, that is a Yaw-Damper of an aircraft. The Yaw-Damper is a control system that damps the yawing motion of an airplane. The response of the actual Yaw-Damper and the response of the Yaw-Damper designed by the method mentioned in this paper are compared. It is verified that the latter is almost the same as the former in transient response and that it has the additional feature of finite time settling. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0823000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-823 |