DocumentCode :
1794848
Title :
On coupling use control technology for hypersonic aircraft
Author :
Wang, A. Jinshuo ; Zhang, B. Qingzhen ; Man, C. Yiming
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
376
Lastpage :
381
Abstract :
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.
Keywords :
aircraft control; control system synthesis; multivariable control systems; stability; controller parameter design; coupling control technology; hypersonic aircraft; multivariate coupling characteristics; stability; Aerospace control; Aircraft; Control systems; Couplings; Educational institutions; Indexes; Stability analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007258
Filename :
7007258
Link To Document :
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