Robust parametric approach for tracking control of an air-breathing hypersonic cruise vehicle
CAI Guang-bin1,2, DUAN Guang-ren1, HU Chang-hua2, TAN Feng1
1.Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001,China;2.Unit 302, Xi’an Institute of Hi-Tech, Hongqing Town, Xi’an 710025, 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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Robust parametric approach for tracking control of an air-breathing hypersonic cruise vehicle
本站小编 哈尔滨工业大学/2019-10-23
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