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基于模糊神经网络的导弹最优寻的末制导律
引用本文:董朝阳,景韶光,王青,张明廉. 基于模糊神经网络的导弹最优寻的末制导律[J]. 北京航空航天大学学报, 2002, 28(4): 373-375. DOI: 10.3969/j.issn.1001-5965.2002.04.001
作者姓名:董朝阳  景韶光  王青  张明廉
作者单位:北京航空航天大学自动化科学与电气工程学院
基金项目:航空科研项目;98D51003;
摘    要:提出了一种适用于一类末制导段采用推力矢量控制的新型导弹的模糊神经网络最优寻的末制导律.在制导律设计时不仅要求导弹能量最省,脱靶量最小,同时考虑了推力矢量控制的非线性特点,并且为改善该神经网络系统的学习效果,在学习算法中还引入模糊学习规则.数字仿真表明所提出的模糊神经网络制导律对于机动目标具有较好的攻击能力.

关 键 词:末制导  推力矢量控制  神经网络  模糊规则  数字仿真
文章编号:1001-5965(2002)04-0373-03
收稿时间:2000-10-17
修稿时间:2000-10-17

Optimal Terminal Missile Guidance Law Based on Fuzzy Neural Networks
DONG Chao-yang,JING Shao-guang,WANG Qing,ZHANG Ming. Optimal Terminal Missile Guidance Law Based on Fuzzy Neural Networks[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(4): 373-375. DOI: 10.3969/j.issn.1001-5965.2002.04.001
Authors:DONG Chao-yang  JING Shao-guang  WANG Qing  ZHANG Ming
Affiliation:Beijing University of Aeronautics and Astronautics, School of Automation Science and Electrical Engineering
Abstract:Because fuzzy neural networks technique has the advantages not only strong adaptability to nonlinear systems but also quick learning ability, it has been applied to nonlinear systems successfully. an optimal terminal missile guidance law based on fuzzy neural networks for the advanced missiles with thruster vector control is presented. In the design of optimal guidance law, the minimum of missile energy loss and miss distance is required while the nonlinear character of the thruster vector control is considered. In addition, fuzzy learning rules are presented to improve the learning ability of the neural networks system. Numerical simulation results are given to illustrate that the presented fuzzy neural networks guidance law has good performance to hit maneuvering targets.
Keywords:precise guidance  thrust vector control  neural networks  fuzzy rules  numerical simulation
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