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