An aircraft adaptive control architecture based on nominal controller

Bo Zhang*, Shushan Wang

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

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
主期刊名Mechatronics and Intelligent Materials II
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 201219 5月 2012

出版系列

姓名Advanced Materials Research
490-495
ISSN(印刷版)1022-6680

会议

会议2nd International Conference on Mechatronics and Intelligent Materials 2012, MIM 2012
国家/地区中国
GuiLin
时期18/05/1219/05/12

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引用此

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