| Author Name | Affiliation | | 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 |
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| 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: |
