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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:CAI Guang-bin,DUAN Guang-ren,HU Chang-hua,TAN Feng.Robust parametric approach for tracking control of an air-breathing hypersonic cruise vehicle[J].Journal of Harbin Institute Of Technology(New Series),2010,17(1):58-64.DOI:10.11916/j.issn.1005-9113.2010.01.011.
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Robust parametric approach for tracking control of an air-breathing hypersonic cruise vehicle
Author NameAffiliation
CAI Guang-bin Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001,China
Unit 302, Xi’an Institute of Hi-Tech, Hongqing Town, Xi’an 710025, China 
DUAN Guang-ren Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001,China 
HU Chang-hua Unit 302, Xi’an Institute of Hi-Tech, Hongqing Town, Xi’an 710025, China 
TAN Feng Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001,China 
Abstract:
To realize the stabilization and the tracking of flight control for an air-breathing hypersonic cruise vehicle, the linearization of the longitudinal model under trimmed cruise condition is processed firstly. Furthermore, the flight control problem is formulated as a robust model tracking control problem. And then, based on the robust parametric approach, eigenstructure assignment and reference model tracking theory, a parametric optimization method for robust controller design is presented. The simulation results show the effectiveness of the proposed approach.
Key words:  hypersonic cruise vehicle  robust parametric approach  tracking control  eigenstructure assignment  parameter optimization
DOI:10.11916/j.issn.1005-9113.2010.01.011
Clc Number:V249.1
Fund:

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