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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.
Yong-hua Fan,Jun Yang, andYu-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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Yong-hua Fan, Jun Yang, 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