DocumentCode
313111
Title
Modelling and controller design for 2.4 m injector powered transonic wind tunnel
Author
Yu, Wen ; Zhang, Guijun
Author_Institution
Autom. Control Sect., CINVESTAV-IPN, Mexico City, Mexico
Volume
3
fYear
1997
fDate
4-6 Jun 1997
Firstpage
1544
Abstract
This paper presents a new modelling and control method of a 2.4 m transonic wind tunnel by analyzing its special properties. Multivariable linearization models are first used for wind tunnel control, and a dual closed loop controller is then implemented to speed up the starting process
Keywords
aerodynamics; closed loop systems; compensation; computerised control; distributed control; linearisation techniques; multivariable systems; starting; wind tunnels; 2.4 m; aerodynamics; closed loop systems; compensation; distributed control; injector; linearization models; modelling; multivariable systems; starting process; transonic wind tunnel; Aerodynamics; Automatic control; Automation; Circuits; Control systems; Distributed computing; Distributed control; Neural networks; Servomechanisms; Valves;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1997. Proceedings of the 1997
Conference_Location
Albuquerque, NM
ISSN
0743-1619
Print_ISBN
0-7803-3832-4
Type
conf
DOI
10.1109/ACC.1997.610807
Filename
610807
Link To Document