Hypersonic Vehicle Longitudinal Control Based on Sliding Mode Observer and Dynamic Surface Control

被引：0
作者：
Guo Yuyan [1 ]
Wang Shixing [2 ]
Xu Bin [3 ]
Hu Xiaoxiang [4 ]
Yuan Yuan [5 ]
机构：
[1] Northwestern Polytech Univ, Sch Automat, Xian 710000, Peoples R China
[2] Naval Aeronaut & Astronaut Univ, Dept Control Engn, Yantai 264000, Peoples R China
[3] Northwestern Polytech Univ, Sch Automat, Xian 710000, Peoples R China
[4] Xian Res Inst Hightech, Unit 1302, Xian 710025, Peoples R China
[5] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
来源：
PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016 | 2016年
基金：
中国国家自然科学基金;
关键词：
Hypersonic Flight Vehicle; Sliding Mode Observer; Dynamic Surface Control; Back-stepping Control; FLIGHT VEHICLE; NEURAL-CONTROL; 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：
In this paper, a class of sliding mode observer and a dynamic surface control law are proposed for the longitudinal dynamics of hypersonic flight vehicle. The sliding mode observer is designed to estimate the angle of attack and flight path angle which are usually difficult to measure. Using the estimation results, the back-stepping-based dynamic surface control law is designed to avoid the explosion of complexity caused by continuous integration, and the control method is applied on the hypersonic vehicle longitudinal model to make the aircraft track the reference trajectory precisely. Simulation results have shown that the proposed methods perform well on the control and state estimation of hypersonic vehicle.
引用
收藏
页码：10926 / 10931
页数：6
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