An adaptive H∞ controller design for bank-to-turn missiles using ridge Gaussian neural networks

被引:27
|
作者
Lin, CK [1 ]
Wang, SD
机构
[1] Chinese Naval Acad, Dept Elect Engn, Kaohsiung 813, Taiwan
[2] Natl Taiwan Univ, Dept Elect Engn, Taipei 106, Taiwan
来源
IEEE TRANSACTIONS ON NEURAL NETWORKS | 2004年 / 15卷 / 06期
关键词
bank-to-turn (BTT) missiles; Gaussian neural networks; H-infinity control theory; ridge functions;
D O I
10.1109/TNN.2004.824418
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
A new autopilot design for bank-to-turn (BTT) missiles is presented. In the design of autopilot, a ridge Gaussian neural network with local learning capability and fewer tuning parameters than Gaussian neural networks is proposed to model the controlled nonlinear systems. We prove that the proposed ridge Gaussian neural network, which can be a universal approximator, equals the expansions of rotated and scaled Gaussian functions. Although ridge Gaussian neural networks can approximate the nonlinear and complex systems accurately, the small approximation errors may affect the tracking performance significantly. Therefore, by employing the H-infinity control theory, it is easy to attenuate the effects of the approximation errors of the ridge Gaussian neural networks to a prescribed level. Computer simulation results confirm the effectiveness of the proposed ridge Gaussian neural networks-based autopilot with H-infinity stabilization.
引用
收藏
页码:1507 / 1516
页数:10
相关论文
共 50 条
  • [21] Disturbance Observer Based Model Predictive Control for Autopilot Design of Bank-to-Turn Missiles
    Yang, Jun
    Li, Shihua
    PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2012, : 2099 - 2104
  • [22] Design of adaptive sliding mode controller for missiles based on neural networks
    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
    Xitong Fangzhen Xuebao, 2008, 20 (5589-5592): : 5589 - 5592
  • [23] The autopilot design of bank-to-turn missile using mixed sensitivity H∞ optimization
    Luo, Delin
    Chen, Ben M.
    2013 IEEE 3RD ANNUAL INTERNATIONAL CONFERENCE ON CYBER TECHNOLOGY IN AUTOMATION, CONTROL AND INTELLIGENT SYSTEMS (CYBER), 2013, : 241 - +
  • [24] Finite-time tracking control of bank-to-turn missiles using terminalsliding mode
    Wang, Zhao
    Li, Shihua
    Fei, Shumin
    ICIC Express Letters, 2009, 3 (04): : 1373 - 1380
  • [25] Distributed composite autopilot design for bank-to-turn missiles with optimized tracking based on disturbance observers
    Yang, Jun
    Wu, Chao
    Li, Shihua
    TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2017, 39 (08) : 1123 - 1138
  • [26] New autopilot design method for bank-to-turn missiles based on the variable structure control theory
    Zhou, Jun
    Zhou, Fengqi
    Chen, Xinhai
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 1993, 11 (03): : 325 - 330
  • [27] Control of Bank-to-turn Missiles using a Combination of First Order and Dynamic Sliding Mode Control
    Sebastian, Treasa
    Jacob, Jeevamma
    2014 INTERNATIONAL CONFERENCE ON ADVANCED COMMUNICATION CONTROL AND COMPUTING TECHNOLOGIES (ICACCCT), 2014, : 104 - 110
  • [28] Design adaptive controller using neural networks
    Shanghai Jiaotong Daxue Xuebao, 4 (109-113):
  • [29] BANK-TO-TURN MISSILE AUTOPILOT DESIGN USING LOOP TRANSFER RECOVERY
    WISE, KA
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1990, 13 (01) : 145 - 152
  • [30] Adaptive Controller Design Using Gamma Neural Networks
    Tahersima, Hanif
    Saleh, Mohammadjafar
    Hamedi, Navid
    Hasanov, Vagif
    2012 2ND AUSTRALIAN CONTROL CONFERENCE (AUCC), 2012, : 425 - 430