Tracking control of air-breathing hypersonic vehicles with non-affine dynamics via improved neural back-stepping design

被引:78
作者
Bu, Xiangwei [1 ]
He, Guangjun [1 ]
Wang, Ke [1 ]
机构
[1] Air Force Engn Univ, Air & Missile Def Coll, 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 (AHV); Non-affine dynamics; Improved back-stepping; Neural approximation; OUTPUT-FEEDBACK; FLIGHT VEHICLE; ADAPTIVE-CONTROL; CONTROL SCHEME; UNCERTAINTY;
D O I
10.1016/j.isatra.2018.02.010
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This study considers the design of a new back-stepping control approach for air-breathing hypersonic vehicle (AHV) non-affine models via neural approximation. The AHV's non-affine dynamics is decomposed into velocity subsystem and altitude subsystem to be controlled separately, and robust adaptive tracking control laws are developed using improved back-stepping designs. Neural networks are applied to estimate the unknown non-affine dynamics, which guarantees the addressed controllers with satisfactory robustness against uncertainties. In comparison with the existing control methodologies, the special contributions are that the non-affine issue is handled by constructing two low-pass filters based on model transformations, and virtual controllers are treated as intermediate variables such that they aren't needed for back-stepping designs any more. Lyapunov techniques are employed to show the uniformly ultimately boundedness of all closed-loop signals. Finally, simulation results are presented to verify the tracking performance and superiorities of the investigated control strategy. (C) 2018 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:88 / 100
页数:13
相关论文
共 33 条
  • [1] Approximate Back-Stepping Fault-Tolerant Control of the Flexible Air-Breathing Hypersonic Vehicle
    An, Hao
    Liu, Jianxing
    Wang, Changhong
    Wu, Ligang
    [J]. IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2016, 21 (03) : 1680 - 1691
  • [2] [Anonymous], AIAA GUID NAV CONTR
  • [3] Fifty years of hypersonics: where we've been, where we're going
    Bertin, JJ
    Cummings, RM
    [J]. PROGRESS IN AEROSPACE SCIENCES, 2003, 39 (6-7) : 511 - 536
  • [4] Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle
    Bolender, Michael A.
    Doman, David B.
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 2007, 44 (02) : 374 - 387
  • [5] Guaranteeing prescribed output tracking performance for air-breathing hypersonic vehicles via non-affine back-stepping control design
    Bu, Xiangwei
    [J]. NONLINEAR DYNAMICS, 2018, 91 (01) : 525 - 538
  • [6] Neural-approximation-based robust adaptive control of flexible air-breathing hypersonic vehicles with parametric uncertainties and control input constraints
    Bu, Xiangwei
    Wu, Xiaoyan
    Wei, Daozhi
    Huang, Jiaqi
    [J]. INFORMATION SCIENCES, 2016, 346 : 29 - 43
  • [7] A guaranteed transient performance-based adaptive neural control scheme with low-complexity computation for flexible air-breathing hypersonic vehicles
    Bu, Xiangwei
    Wu, Xiaoyan
    Huang, Jiaqi
    Wei, Daozhi
    [J]. NONLINEAR DYNAMICS, 2016, 84 (04) : 2175 - 2194
  • [8] A neural approximation-based novel back-stepping control scheme for air-breathing hypersonic vehicles with uncertain parameters
    Bu, Xiangwei
    Wu, Xiaoyan
    Zhang, Rui
    Ma, Zhen
    Huang, Jiaqi
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2016, 230 (03) : 231 - 243
  • [9] Novel adaptive neural control of flexible air-breathing hypersonic vehicles based on sliding mode differentiator
    Bu Xiangwei
    Wu Xiaoyan
    Ma Zhen
    Zhang Rui
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2015, 28 (04) : 1209 - 1216
  • [10] Tracking differentiator design for the robust backstepping control of a flexible air-breathing hypersonic vehicle
    Bu, Xiangwei
    Wu, Xiaoyan
    Zhang, Rui
    Ma, Zhen
    Huang, Jiaqi
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2015, 352 (04): : 1739 - 1765