Design of Overload Control for Target Missiles Based on Robust Adaptive Terminal Sliding-mode Control

被引:0
作者
Bi Kai-bo [1 ]
Zhang Yi-fei [1 ]
Sui Xian-hui [1 ]
机构
[1] Dalian Naval Acad, Dept Missile, Dalian 116018, Peoples R China
来源
PROCEEDINGS OF THE 2015 2ND INTERNATIONAL WORKSHOP ON MATERIALS ENGINEERING AND COMPUTER SCIENCES (IWMECS 2015) | 2015年 / 33卷
关键词
robust adaptive control; terminal sliding-mode control; neural network; overload control;
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
Backstepping design, neural network technology, robust adaptive control and terminal sliding-mode control is combined. Firstly, neural networks are used to estimate the virtual control laws of the controlled system. Secondly, terminal sliding-mode control is utilized to improve the convergence speed and robustness of the controlled plant. Thirdly, robust adaptive control method is employed to estimate the unknown upper boundary of uncertainties. Lastly, backstepping design is incorporated to design the virtual control laws and actual control law of the controlled system. Based on Lyapunov stability theorem, all of error signals are bounded and exponentially converge to a bound neighbor of the origin. Simulation results show the effectiveness of the proposed control method.
引用
收藏
页码:120 / 127
页数:8
相关论文
共 5 条
  • [1] Chen Zhi-xiang, 2007, Systems Engineering and Electronics, V29, P2097
  • [2] Autopilot design for highly maneuvering STT missiles via singular perturbation-like technique
    Lee, JI
    Ha, IJ
    [J]. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 1999, 7 (05) : 527 - 541
  • [3] Universal Approximation Using Radial-Basis-Function Networks
    Park, J.
    Sandberg, I. W.
    [J]. NEURAL COMPUTATION, 1991, 3 (02) : 246 - 257
  • [4] Qian Xingfang, 2000, MISSILE FLIGHT AEROD
  • [5] [杨志峰 Yang Zhifeng], 2010, [宇航学报, Journal of Chinese Society of Astronautics], V31, P2295