%0 Journal Article
%T Variable structure attitude control of flexible satellite<br>挠性卫星的变结构姿态控制
%A GUAN Ping
%A LIU Xiao-he
%A LIU Xiang-jie
%A <br>管萍
%A 刘小河
%A 刘向杰
%J 控制理论与应用
%D 2007
%I 
%X The input-output linearization control is combined with the adaptive fuzzy sliding mode control,and is applied to the attitude maneuver control of the flexible satellite.Firstly,the basic control structure is presented.The adaptive fuzzy control is then utilized to approach the nonlinear control part of sliding mode control,and the adaptive law is also derived.Morever,the parameter of the adaptive fuzzy control is adjusted on-line to deal with the satellite uncertainty,thus the robustness of system is obtained.Finally,simulation results show that precise attitude control is accomplished in spite of the uncertainty in the system.
%K adaptive fuzzy control
%K input-output linearization
%K sliding mode control
%K flexible satellite<br>自适应模糊控制
%K 输入输出线性化
%K 滑模控制
%K 挠性卫星
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=5B3AB970F71A803DEACDC0559115BFCF0A068CD97DD29835&cid=8240383F08CE46C8B05036380D75B607&jid=970898A57DFC021F93AB51667BAED7F7&aid=79D48AF13175E3FC9164A5F35679B7E3&yid=A732AF04DDA03BB3&vid=B91E8C6D6FE990DB&iid=38B194292C032A66&sid=03436AC72A659ACA&eid=D8B37A0210DB6B9D&journal_id=1000-8152&journal_name=控制理论与应用&referenced_num=0&reference_num=7