DocumentCode
566136
Title
Robust model predictive controller design for a Hypersonic Flight Vehicle
Author
Tao, Xiangyuan ; Hua, Chen ; Li, Ning ; Li, Shaoyuan
Author_Institution
Department of Automation, Shanghai Jiao Tong University, and key laboratory of system control and information processing, ministry of education, 200240, China
fYear
2012
fDate
24-26 June 2012
Firstpage
1299
Lastpage
1304
Abstract
This paper considers the control problem of cruising flight of Hypersonic Flight Vehicle (HFV). The dynamic characteristics of HFV can be addressed as a strong nonlinear, and parameter uncertain multivariable system with hard constraints, which is extremely difficult to design the controller. In this paper, the longitudinal dynamic model of HFV is studied. Subsequently, we propose a robust model predictive control (RMPC) strategy to handle constraints in a systematic manner and overcome the impact of parameter uncertainty on the control effect, and a robust model predictive controller is designed for cruising flight of HFV. Simulation results show that this method can provide sufficient robustness and handle constraints effectively.
Keywords
Hypersonic flight vehicle; longitudinal flight control; robust predictive control;
fLanguage
English
Publisher
ieee
Conference_Titel
Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on
Conference_Location
Wuhan, Hubei, China
Print_ISBN
978-1-4673-1524-1
Type
conf
Filename
6260318
Link To Document