Progress in control approaches for hypersonic vehicle

查看全文 作　　者：DUAN [1,2]HaiBin;LI [1]Pei

机构地区：[1]Science and Technology on Aircraft Control Laboratory,School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China;[2]State Key Laboratory of Virtual Reality Technology and Systems,Beihang University,Beijing 100191,China

出　　处：《Science China(Technological Sciences)》索引2012年第55卷第10期,共6页

基　　金：supported by the National Natural Science Foundation of China (Grant Nos. 61273054,60975072,60604009);the Program for New Century Excellent Talents in University of China (Grant No. NCET-10-0021);the Aeronautical Foundation of China (Grant No. 20115151019);the Open Fund of the State Key Laboratory of Virtual Reality Technology and Systems (Grant No. VR-2011-ZZ-01) 摘　　要：The controller design for hypersonic vehicle is critical and challenging because of the inherent couplings between the propulsion system and the airframe dynamics,as well as the presence of strong flexibility effects.Many researchers have investigated various strategies to mitigate the coupling by means of robust design methods.This paper reviews the recent research efforts to promote the capability of control design for hypersonic vehicle.Methodologies such as robust control,adaptive control,sliding mode control and other hybrid methods have made significant progresses in hypersonic control.Then,the main challenges of control approaches for hypersonic vehicle are systematically analyzed in detail. 关键词：高超声速飞行器控制器设计推进系统自适应控制研究人员设计方法控制设计鲁棒控制

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Progress in control approaches for hypersonic vehicle

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耦合文献(178)

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