A self-organizing fuzzy control approach for bank-to-turn missiles

被引:10
|
作者
Lin, CK [1 ]
Wang, SD [1 ]
机构
[1] Natl Taiwan Univ, Dept Elect Engn, Taipei 106, Taiwan
关键词
fuzzy basis function; neural networks; engineering; terminal attractor;
D O I
10.1016/S0165-0114(96)00320-X
中图分类号
TP301 [理论、方法];
学科分类号
081202 ;
摘要
In this paper, an adaptive fuzzy autopilot is developed for bank-to-turn (BTT) missiles. We propose a self-organizing rotated fuzzy basis function control system that is more flexible than fuzzy basis function expansion in that not only the output weights but also the shapes of fuzzy basis functions can be tuned. Another characteristic of this autopilot is to incorporate the terminal attractor controller into the autopilot to speed up the convergence rate. The global stability analysis established in the Lyapunov sense shows that the states and tracking errors of the BTT missile are uniformly bounded. Finally, there are two simulation examples to demonstrate the effectiveness of the proposed autopilot. The purpose of the first example is to indicate the better performance including faster convergence speed and lower steady-state error obtained by autopilots with terminal attractors as compared with that autopilot without terminal attractor. Another simulation result proves that BTT missile can manipulate under various flight conditions in our scenarios and shows the superior tracking performance. (C) 1998 Elsevier Science B.V. All rights reserved.
引用
收藏
页码:281 / 306
页数:26
相关论文
共 50 条
  • [31] Performance enhancement methods for unstable bank-to-turn (BTT) missiles with saturating actuators
    Rodriguez, AA
    Wang, YZ
    INTERNATIONAL JOURNAL OF CONTROL, 1996, 63 (04) : 641 - 678
  • [32] Performance enhancement methods for unstable bank-to-turn (BTT) missiles with saturating actuators
    Arizona State Univ, Tempe, United States
    Int J Control, 4 (641-678):
  • [33] Guaranteed cost decoupling control of bank-to-turn vehicle
    Deng, Z.
    Wang, Y.
    Liu, L.
    Zhu, Q.
    IET CONTROL THEORY AND APPLICATIONS, 2010, 4 (09): : 1594 - 1604
  • [34] Mixed H2/H∞ autopilot design of bank-to-turn missiles using fuzzy basis function networks
    Lin, Chuan-Kai
    FUZZY SETS AND SYSTEMS, 2007, 158 (20) : 2268 - 2287
  • [35] Robust autopilot design for bank-to-turn missiles using adaptive dual-layer sliding mode control
    Guo, Zongyi
    Zhou, Jun
    Guo, Jianguo
    OPTIK, 2017, 131 : 383 - 398
  • [36] Decentralized Fuzzy Guaranteed Cost Tracking Control with Poles Assignment for Bank-to-Turn Missile
    Shi Kun
    Liang Xiao-geng
    26TH CHINESE CONTROL AND DECISION CONFERENCE (2014 CCDC), 2014, : 1260 - 1265
  • [37] Nonlinear autopilot design and simulation for bank-to-turn missiles using dynamic inversion method
    Zhang, Y
    Duan, CY
    Zhang, P
    SYSTEM SIMULATION AND SCIENTIFIC COMPUTING, VOLS 1 AND 2, PROCEEDINGS, 2005, : 1144 - 1148
  • [38] GUIDANCE OF A BANK-TO-TURN MISSILE WITH ALTITUDE CONTROL REQUIREMENTS
    CUNNINGHAM, EP
    JOURNAL OF SPACECRAFT AND ROCKETS, 1974, 11 (05) : 340 - 342
  • [39] SELF-ORGANIZING CONTROL USING FUZZY NEURAL NETWORKS
    YAMAGUCHI, T
    TAKAGI, T
    MITA, T
    INTERNATIONAL JOURNAL OF CONTROL, 1992, 56 (02) : 415 - 439
  • [40] A self-organizing fuzzy CMAC for sliding mode control
    Hwang, KS
    Lin, CS
    1996 IEEE INTERNATIONAL WORKSHOP ON VARIABLE STRUCTURE SYSTEMS - VSS '96, PROCEEDINGS, 1996, : 133 - 138