Progress in control approaches for hypersonic vehicle  

作　　者：DUAN HaiBin LI 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)》2012年第10期2965-2970,共6页中国科学（技术科学英文版）

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：hypersonic vehicle robust control adaptive control fuzzy control sliding mode control inherent coupling 

分 类 号：TP273[自动化与计算机技术—检测技术与自动化装置] V43[自动化与计算机技术—控制科学与工程]