Offset-free trajectory tracking control for hypersonic vehicle under external disturbance and parametric uncertainty

被引:13
作者
Gao, Haiyan [1 ]
Zhang, Ji [1 ]
Tang, Weiqiang [2 ]
机构
[1] Xiamen Univ Technol, Sch Elect Engn & Automat, High Voltage Key Lab Fujian Prov, Xiamen, Peoples R China
[2] Lanzhou Univ Technol, Sch Elect & Informat Engn, Lanzhou, Gansu, Peoples R China
来源
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2018年 / 355卷 / 03期
基金
中国国家自然科学基金;
关键词
SLIDING MODE CONTROL; PREDICTIVE CONTROL; FLIGHT VEHICLE; CHAOTIC SYSTEMS; CONTROL DESIGN; ROBUST-CONTROL; OBSERVER; AIRCRAFT; STATE;
D O I
10.1016/j.jfranklin.2017.12.007
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A novel offset-free trajectory tracking control strategy is proposed for a hypersonic vehicle under external disturbances and parameter uncertainties. In order to realize the real-time control for the hypersonic vehicle, the predictive control law is divided into the on-line design and off-line design. Unlike general nonlinear disturbance observer-based control which involves designing the disturbance compensation strategy, the influences of the disturbances on the velocity and altitude are attenuated by the direct feedback compensation (DFC). Particularly, the offset-free tracking feature is proved for the output reference signal. Simulations show that the real-time control can be realized for the hypersonic vehicle, the controls and angle of attack are all in their given constraint scopes, and the velocity and altitude can track the given references accurately even under mismatched disturbances. (c) 2018 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:997 / 1017
页数:21
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