A Control Method of Hypersonic Vehicle Based on the Structured Singular Value Theory
Firstly, the conception of hypersonic flight and its flight characteristics are introduced in the article. Secondly, a control method based on the structured singular value theory is proposed, and the necessity of this method whether can be applied to design the hypersonic vehicle controller is discussed. And then taking a model for example, the robust controller of hypersonic vehicle is designed. At last, the control effect of this controller is proved better through the simulation result. It also turned out that the controller has excellent command track performance.
hypersonic robust control u analysis and synthesis model
Li gang Xu lin-wei He hao An xing
Missile Institute of Air Force Engineering University, Shaanxi, sanyuan, China, 713800
国际会议
三亚
英文
761-764
2012-01-06（万方平台首次上网日期，不代表论文的发表时间）