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	Control-oriented Modeling for Hypersonic Vehicle Control
	Wei Qingkai ; Huang Xun
	2010
关键词	hypersonic vehicle control-oriented modeling oblique-shock theory flight control
英文摘要	Hypersonic vehicles have great promising in civil and military application. The physics related to hypersonic flight is quite different from traditional aircraft, such as strong nonlinear, strong aerodynamic coupling and so on. In this work, we apply oblique-shock theory and Prandtl-Meyer flow to obtain a control-oriented model for a hypersonic flight. The results compare well with results of computational fluid dynamics, but can be achieved much quicker. which is preferred for control investigation. As an example, a complete feedback control system for the flight model is demonstrated in the end of this paper.; Engineering, Aerospace; Astronomy & Astrophysics; CPCI-S(ISTP); 0
语种	英语
内容类型	会议论文
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/316462]
专题	工学院
推荐引用方式 GB/T 7714	Wei Qingkai,Huang Xun. Control-oriented Modeling for Hypersonic Vehicle Control[C]. 见:.

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