Longitudinal Control of Morphing Aircraft Based on Fixed Time Constraint Backstepping Method

Ruichen Ming, Xiaoxiong Liu, Yu Li, Wei Huang, Weiguo Zhang

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

In this paper, a fixed-time controller is proposed in view of the characteristics of force and moment changes of the variable sweep aircraft during the morphing process. The characteristic of the controller is that it can ensure that the stability of the system in a fixed time, and can estimate the aerodynamic derivatives of the variable sweep through the least squares estimation method. In addition, according to the characteristics that the controller easily leads to system input saturation, a processing method of constraint control is proposed to ensure the stability of the system under the condition of limited input. Finally, the variable-sweep-wing aircraft is used to simulate the angle of attack and pitch angular velocity, and the simulation results verify the effectiveness of the control law.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
编辑Liang Yan, Haibin Duan, Yimin Deng, Liang Yan
出版商Springer Science and Business Media Deutschland GmbH
3688-3697
页数10
ISBN(印刷版)9789811966125
DOI
出版状态已出版 - 2023
活动International Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, 中国
期限: 5 8月 20227 8月 2022

出版系列

姓名Lecture Notes in Electrical Engineering
845 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Guidance, Navigation and Control, ICGNC 2022
国家/地区中国
Harbin
时期5/08/227/08/22

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