L1 adaptive control law design for Aircraft considering actuator influence

Xiaoxiong Liu, Hui Zhao, Qingyuan Ma, Jian Shen

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

Considering the impact of the actuator on the aircraft flight performance, this paper proposes a design method for longitudinal damping control law of aircraft based on Ll adaptive control. Firstly, the aircraft adaptive control model is built according to modeling error and external disturbance of flight control system. And then the actuator model was augmented to the system state vector for accurate pitch rate feedback control. Finally, the Ll adaptive law and observer are designed based on the system structure. The Simulation results show that the Ll adaptive control can perform the longitudinal damping control of the aircraft well, and can still effectively control when the actuator failure.

源语言英语
主期刊名2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
出版商Institute of Electrical and Electronics Engineers Inc.
ISBN(电子版)9781538611715
DOI
出版状态已出版 - 8月 2018
活动2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 - Xiamen, 中国
期限: 10 8月 201812 8月 2018

出版系列

姓名2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

会议

会议2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
国家/地区中国
Xiamen
时期10/08/1812/08/18

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