Composite predictive flight control for airbreathing hypersonic vehicles

被引:56
|
作者
Yang, Jun [1 ,2 ]
Zhao, Zhenhua [1 ]
Li, Shihua [1 ]
Zheng, Wei Xing [2 ]
机构
[1] Southeast Univ, Sch Automat, Key Lab Measurement & Control CSE, Minist Educ, Nanjing 210096, Jiangsu, Peoples R China
[2] Univ Western Sydney, Sch Comp Engn & Math, Penrith, NSW 2751, Australia
基金
中国博士后科学基金; 中国国家自然科学基金; 澳大利亚研究理事会;
关键词
airbreathing hypersonic vehicle; nonlinear model predictive control; optimised tracking; mismatched disturbance rejection; nominal performance recovery; SLIDING MODE CONTROL; NONLINEAR-DISTURBANCE-OBSERVER; TRACKING CONTROL; CONTROL-SYSTEMS; CONTROL DESIGN; SPACE-VEHICLE; MPC;
D O I
10.1080/00207179.2014.896477
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 robust optimised tracking control problem for a generic airbreathing hypersonic vehicle (AHV) subject to nonvanishing mismatched disturbances/uncertainties is investigated in this paper. A baseline nonlinear model predictive control (MPC) method is firstly introduced for optimised tracking control of the nominal dynamics. A nonlinear-disturbance-observer-based control law is then developed for robustness enhancement in the presence of both external disturbances and uncertainties. Compared with the existing robust tracking control methods for AHVs, the proposed composite nonlinear MPC method obtains not only promising robustness and disturbance rejection performance but also optimised nominal tracking control performance. The merits of the proposed method are validated by implementing simulation studies on the AHV system.
引用
收藏
页码:1970 / 1984
页数:15
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