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Proceedings Paper

Robust control of hypersonic aircraft
Author(s): Yong-hua Fan; Jun Yang; Yu-zhuo Zhang
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Paper Abstract

Design of a robust controller for the longitudinal dynamics of a hypersonic aircraft by using parameter space method is present. The desirable poles are mapped to the parameter space of the controller using pole placement approach in this method. The intersection of the parameter space is the common controller for the multiple mode system. This controller can meet the need of the different phases of aircraft. It has been proved by simulation that the controller has highly performance of precision and robustness for the disturbance caused by separation, cowl open, fuel on and fuel off and perturbation caused by unknown dynamics.

Paper Details

Date Published: 10 November 2007
PDF: 6 pages
Proc. SPIE 6795, Second International Conference on Space Information Technology, 67955A (10 November 2007); doi: 10.1117/12.775194
Show Author Affiliations
Yong-hua Fan, Northwestern Polytechnical Univ. (China)
Jun Yang, Northwestern Polytechnical Univ. (China)
Yu-zhuo Zhang, Northwestern Polytechnical Univ. (China)

Published in SPIE Proceedings Vol. 6795:
Second International Conference on Space Information Technology
Cheng Wang; Shan Zhong; Jiaolong Wei, Editor(s)

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