A prescribed performance control approach guaranteeing small overshoot for air-breathing hypersonic vehicles via neural approximation

被引:74
作者
Bu, Xiangwei [1 ]
Xiao, Yu [2 ,3 ]
Wang, Ke [1 ]
机构
[1] Air Force Engn Univ, Air & Missile Def Coll, Xian 710051, Shaanxi, Peoples R China
[2] Northwestern Polytech Univ, Sch Automat, Xian 710072, Shaanxi, Peoples R China
[3] Air Force Engn Univ, Dept Sci Researching, Xian 710051, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
Air-breathing hypersonic vehicle; Prescribed performance control (PPC); Performance function; Neural networks (NNs); Minimal-learning parameter; TRAJECTORY LINEARIZATION CONTROL; ROBUST ADAPTIVE-CONTROL; BACK-STEPPING CONTROL; REENTRY VEHICLE; TRACKING DIFFERENTIATOR; DYNAMIC-SYSTEMS; CONTROL SCHEME; DESIGN; CONSTRAINTS; UNCERTAINTY;
D O I
10.1016/j.ast.2017.10.005
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper investigates a new prescribed performance control (PPC) methodology for the longitudinal dynamic model of an air-breathing hypersonic vehicle via neural approximation. To release the restriction on traditional PPC that the initial tracking errors have to be known in advance for control design, a novel performance function is exploited. Moreover, the devised controller is capable of guaranteeing prescribed performance on the velocity and altitude tracking errors. Neural networks (NNs) are employed to approximate the unknown vehicle dynamics and a minimal-learning parameter scheme is utilized to update the norm of NN's weight vector. Hence, a low computational burden design is achieved without using back-stepping. The semi-globally uniform boundedness of all the closed-loop signals is insured by Lyapunov synthesis. Finally, simulation results are presented to validate the efficacy of the proposed control approach. (C) 2017 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:485 / 498
页数:14
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