Robust controller design for uncertain delayed systems and its applications to hypersonic vehicles

被引：12

作者：

Liu, Hao ^{[1
,2
]}

Zhang, Jiansong ^{[1
]}

Xi, Jianxiang ^{[3
]}

Yu, Yao ^{[4
]}

机构：

[1] Beihang Univ, Sch Astronaut, Beijing, Peoples R China

[2] Univ Texas Arlington, Res Inst, Arlington, TX 76019 USA

[3] High Tech Inst Xian, Xian, Peoples R China

[4] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing, Peoples R China

来源：

ASIAN JOURNAL OF CONTROL | 2020年 / 22卷 / 04期

基金：

中国国家自然科学基金;

关键词：

hypersonic vehicle; nonlinear system; robust control; time delay; SLIDING MODE CONTROL; TRACKING-CONTROL; NONLINEAR CONTROL; ADAPTIVE-CONTROL; TIME-DELAY; AIRCRAFT;

D O I：

10.1002/asjc.2045

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The longitudinal dynamics of hypersonic flight vehicles involves strong nonlinearity and coupling, uncertainties including parametric uncertainties, unmodeled uncertainties, external disturbances, and time-varying input and state time delays. In this paper, a robust controller design method is proposed for the longitudinal stabilization of these vehicles by the signal-compensation-based control idea. Theoretical analysis is given to prove the robustness properties of the designed closed-loop control system subject to multiple time-varying uncertainties and time-varying input and state delays. Simulation results are performed to show the validness and advantages of the proposed robust control approach.

引用

页码：1579 / 1588

页数：10

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