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基于自适应反演的导弹滑模控制
引用本文:施建洪,晋玉强,肖支才.基于自适应反演的导弹滑模控制[J].海军航空工程学院学报,2004,19(6):607-610.
作者姓名:施建洪  晋玉强  肖支才
作者单位:海军航空工程学院控制工程系,烟台,264001
摘    要:阐述了在导弹系统存在不确定性情况下,基于自适应反演控制技术和模糊神经网络理论,提出了一种导弹滑模控制系统设计方法。设计过程中将不确定性对系统的影响合成为一项,然后应用模糊神经逼近器来逼近系统的不确定项;考虑了已知信息,利用自适应模糊神经控制理论和滑模控制设计了控制器,应用Lypunov稳定性理论保证了闭环系统的稳定性,并推导出模糊神经逼近器各参数的自适应调节律。

关 键 词:非线性系统  滑模控制  模糊神经逼近器  不确定性
修稿时间:2004年7月1日

Sliding Mode Control of Missile Based on Adaptive Backstepping
SHI Jian-hong,JIN Yu-qiang,XIAO Zhi-cai.Sliding Mode Control of Missile Based on Adaptive Backstepping[J].Journal of Naval Aeronautical Engineering Institute,2004,19(6):607-610.
Authors:SHI Jian-hong  JIN Yu-qiang  XIAO Zhi-cai
Abstract:Based on adaptive backstepping control techniques and fuzzy-neural theory,a sliding mode control scheme is proposed for missile control systems with uncertainties.Firstly,the effect of the uncertainties is synthesized one term in the design procedure.Then fuzzy-neural approximators are designed to approximate the uncertainty function.Considering the known information,the controller is designed using adaptive fuzzy-neural control theory and sliding mode control theory.The Lyapunov stability theory is used to guarantee the closed-loop stability and derive adaptive tuning rules for updateing the parameters of the fuzzy-neural approximator.
Keywords:nonlinear system  sliding mode control  fuzzy-neural approximator  uncertainty
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