Integrated guidance and control with impact angle constraint

被引：0
作者：
Liu, Wangkui [2 ]
Wei, Yiyin [2 ]
Duan, Guangren [1 ,2 ]
机构：
[1] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin, Heilongjiang, Peoples R China
[2] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin, Heilongjiang, Peoples R China
来源：
2017 CHINESE AUTOMATION CONGRESS (CAC) | 2017年
基金：
中国国家自然科学基金; 国家自然科学基金重大项目;
关键词：
Adaptive; Integrated guidance and control(IGC); Impact angle constraint; Dynamic surface control; DYNAMIC SURFACE CONTROL; MISSILE GUIDANCE; CONTROL DESIGN; PHASE;
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：
In this paper, an adaptive integrated guidance and control(IGC) law is proposed for the missile intercepting the maneuvering target with impact angle constraint. Considering the parameter uncertainties, a new IGC model is established. Subsequently, the dynamic surface control and adaptive technique are combined to design the adaptive IGC law. Finally, the simulation results are provided to verify the effectiveness of the presented IGC law.
引用
收藏
页码：866 / 871
页数：6
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