High-Order Disturbance Observer-Based Attitude Control with Prescribed Performance for Hypersonic Vehicle

被引:0
|
作者
Yang, GuangHui [1 ]
Wang, Xinming [2 ,3 ]
机构
[1] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China
[2] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
[3] Minist Eduact, Key Lab Measurement & Control Complex Syst Engn, Beijing, Peoples R China
关键词
Hypersonic Vehicle; Disturbance Observer; Prescribed Performance Control; Dynamics Surface Control; SLIDING MODE CONTROL; SCHEME;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a high-order disturbance observer-based attitude tracking controller design with prescribed performance for hypersonic vehicle. The lumped disturbances caused by parameters perturbations, external disturbances and unmodelled dynamics are estimated accurately by utilizing high-order disturbance observers. Based on the disturbances estimation, a composite attitude tracking controller with guaranteeing prescribed transient and steady performance is proposed and the stability analysis of the closed-loop system is rigorously analyzed using the Lyapunov technique. The proposed controller not only ensures the tracking errors are within the desired performance envelope but also considering the disturbance rejection. Finally, the effectiveness of the proposed method is verified by simulations.
引用
收藏
页码:7766 / 7771
页数:6
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