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- OpenAccess
Flight Controller Design via Combined Sliding Mode and H(subscript ∞) Techniqueds
順滑模式及H(下標 ∞)技術混合之飛行控制器設計
並列摘要
This paper introduces a controller design based on the combined sliding-mode and H(subscript ∞) techniques. The control objective is to deal with the output tracking problem of linear systems suffering from bounded parameter variation and external disturbance. The proposed method is applied to an aircraft flight controller design. Numerical simulation results are shown to demonstrate its effectiveness and robustness.
被引用紀錄
Fang, L. Y. (2011). 應用小腦控制器於具有時變延遲之 CDMA 無線通訊系統功率控制 [master's thesis, Tamkang University]. Airiti Library. https://doi.org/10.6846/TKU.2011.00456
蘇聖詣（2009）。虛擬根值法之順滑模態控制應用於半主動式懸吊控制系統〔碩士論文，國立臺北科技大學〕。華藝線上圖書館。https://doi.org/10.6841/NTUT.2009.00389
楊千蕙（2009）。水溶液法合成氧化鋅與氧化鎂殼膜奈米結構之特性研究〔碩士論文，國立臺北科技大學〕。華藝線上圖書館。https://doi.org/10.6841/NTUT.2009.00361
延伸閱讀
- 孔健君、楊憲東（2001）。非線性H(下標 ∞)控制理論在飛機控制上的實現。中國航空太空學會學刊，33(1)，23-30。https://doi.org/10.6124/TAASRC.200103_33(1).04
- 潘咨融（2016）。正值系統之 H-infinity 控制器設計〔碩士論文，淡江大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0002-2906201615515300
- Hwang, C. N., Yang, J. M., & Chiang, C. Y. (2001). 輔以H(下標 ∞)－控制操舵系統之模糊避碰系統的設計. Journal of Marine Science and Technology, 9(1), 25-37. https://doi.org/10.6119/JMST.200106_9(1).0004
- Chiang, M. H., Lee, L. W., Kuo, C. F. J., & Chen, Y. N. (2009). 以具H(下標 ∞)追蹤及函式近似法之適應性滑動模式控制器實現氣壓伺服系統之軌跡追蹤控制. 中國機械工程學刊, 30(2), 83-94. https://doi.org/10.29979/JCSME.200904.0002
- Hsieh, Y. R. (1999). 整合型間時雙滑動模式控制器之研製 [master's thesis, National Taiwan Normal University]. Airiti Library. https://www.airitilibrary.com/Article/Detail?DocID=U0021-2603200719094620