Abstract—This study focuses on the H-inf control of aircraft during landing, our aim being also to design a robust control law for a wind shear profile using the H-inf control. This method is based on minimizing a closed loop transfer function norm in order to obtain the stability and robust performance of the system. Some of the design objectives are suggested in other works, but the numerical case study and the numerical implementation of the design procedure are performed and presented in this paper for the first time.
Index Terms—Landing, H-inf, control law, wind shear.
Serena Cristian Voicu and Florentin Alin Buţu are with Faculty of Aerospace Engineering, University “Politehnica” of Bucharest, Bucharest, Romania (e-mail: voicuserena@yahoo.com, florentinalin@yahoo.com).
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Cite: Serena Cristiana Voicu and Florentin Alin Buţu, "H-Infinity Design for Automatic Landing System," International Journal of Modeling and Optimization vol. 7, no. 3, pp. 173-178, 2017.
