Integrated guidance and control with input saturation

被引：0

作者：

Liu, Wangkui ^{[1
,2
]}

Wei, Yiyin ^{[2
]}

Duan, Guangren ^{[1
,2
]}

机构：

[1] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin 150001, Heilongjiang, Peoples R China

[2] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Heilongjiang, Peoples R China

来源：

PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017) | 2017年

基金：

国家自然科学基金重大项目; 中国国家自然科学基金;

关键词：

Backstepping control; Adaptive; Integrated guidance and control (IGC); Input saturation; MISSILE GUIDANCE; CONSTRAINT; VEHICLE; DESIGN;

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：

Based on backstepping control technique, a novel adaptive integrated guidance and control (IGC) law is presented for missile intercepting maneuvering target with input saturation. To deal with the uncertainties in the IGC system, adaptive control technique is utilized to estimate the upper bounds of the uncertainties. Moreover, an auxiliary system is designed to cope with the input saturation. The state of the auxiliary system is used in the IGC law design and stability analysis. The detailed stability analysis of the closed-loop IGC system is carried out based on the Lyapunov theory. Finally, the effectiveness of the proposed adaptive IGC law is verified by the nonlinear numerical simulation results.

引用

页码：6179 / 6184

页数：6

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