On Coupling Use Control Technology for Hypersonic aircraft

被引：0
|
作者：
Wang, Jinshuo [1 ]
Zhang, Qingzhen [1 ]
Man, Yiming [2 ]
机构：
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] China Acad Launch Vehicle Technol, Reasearch Ctr, Beijing 100076, Peoples R China
来源：
2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2014年
关键词：
SYSTEMS;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
the multivariate coupling characteristics is studied, as well as the characteristics of the coupled mode and its stability. Some available coupling control strategy is put forward, and the parameter of controller is designed. The purpose of this paper is to solve the problem of increasing stability and improving mobility, by the method of decoupling and coupling use.
引用
收藏
页码：376 / 381
页数：6
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