DocumentCode
589415
Title
Control of Hypersonic Vehicle Based on Improved QFT
Author
Shi Zhen ; Wang Fei ; Ma Wen-qiao
Author_Institution
Coll. of Autom., Harbin Eng. Univ., Harbin, China
Volume
1
fYear
2012
fDate
28-29 Oct. 2012
Firstpage
227
Lastpage
230
Abstract
Hypersonic vehicle has high military value in terms of real-time reconnaissance, remote rapid deployment and precision strike, especially the implementation of real-time reconnaissance mission has unique advantages. Efficient thrust, the aircraft must be flying high dynamic pressure conditions, in order to control the resulting aerodynamic heating and aerodynamic drag for the hypersonic vehicle angle of attack for precise control, at the same time, the dynamic characteristics of the hypersonic vehicle conventional aircraft are very different, the most critical aerodynamic characteristics are good enough stability of the pre-degree in terms of the control system must have a very strong robust feedback system. the QFT method, using an improved design of hypersonic flight longitudinal channel controller. Simulation results show that the robust controller design meets the system requirements.
Keywords
aerodynamics; aircraft control; control system synthesis; drag; feedback; heating; military aircraft; robust control; QFT; aerodynamic drag control; aerodynamic heating control; dynamic characteristics; hypersonic flight longitudinal channel controller design; hypersonic vehicle control; hypersonic vehicle conventional aircraft; military value; precision strike; real-time reconnaissance mission; remote rapid deployment; robust controller design; robust feedback system; Aerodynamics; Aerospace control; Aircraft; Control systems; Robustness; Vehicle dynamics; Vehicles; QFT; control system; hepersonic; nonlinear;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Intelligence and Design (ISCID), 2012 Fifth International Symposium on
Conference_Location
Hangzhou
Print_ISBN
978-1-4673-2646-9
Type
conf
DOI
10.1109/ISCID.2012.64
Filename
6406959
Link To Document