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 :
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