Paper
10 November 2007 Robust control of hypersonic aircraft
Yong-hua Fan, Jun Yang, Yu-zhuo Zhang
Author Affiliations +
Proceedings Volume 6795, Second International Conference on Space Information Technology; 67955A (2007) https://doi.org/10.1117/12.775194
Event: Second International Conference on Spatial Information Technology, 2007, Wuhan, China
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.
© (2007) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Yong-hua Fan, Jun Yang, and Yu-zhuo Zhang "Robust control of hypersonic aircraft", Proc. SPIE 6795, Second International Conference on Space Information Technology, 67955A (10 November 2007); https://doi.org/10.1117/12.775194
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