摘要
This paper presents adaptive control architecture for the safe flight of a transport aircraft under adverse operating conditions and uncertainties. This architecture combines a nominal controller based on an LQR with integral action, and an adaptive controller that accommodates for actuator saturation and disturbances. In this paper, we consider the control of the C-5 transport aircraft, which is similar to the Generic Transport Model. We delineate the underlying nonlinear dynamic model and introduce various upsets, damages, and failures by representing these various adverse conditions in the form of uncertainties.
源语言 | 英语 |
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主期刊名 | Mechatronics and Intelligent Materials II |
页 | 105-109 |
页数 | 5 |
DOI | |
出版状态 | 已出版 - 2012 |
活动 | 2nd International Conference on Mechatronics and Intelligent Materials 2012, MIM 2012 - GuiLin, 中国 期限: 18 5月 2012 → 19 5月 2012 |
出版系列
姓名 | Advanced Materials Research |
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卷 | 490-495 |
ISSN(印刷版) | 1022-6680 |
会议
会议 | 2nd International Conference on Mechatronics and Intelligent Materials 2012, MIM 2012 |
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国家/地区 | 中国 |
市 | GuiLin |
时期 | 18/05/12 → 19/05/12 |
指纹
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Zhang, B., & Wang, S. (2012). An aircraft adaptive control architecture based on nominal controller. 在 Mechatronics and Intelligent Materials II (页码 105-109). (Advanced Materials Research; 卷 490-495). https://doi.org/10.4028/www.scientific.net/AMR.490-495.105