Robustness optimization approach for hypersonic vehicle controller based on parallel computing

Abstract

Air-breathing hypersonic vehicle maneuvering in large flight envelope has imposed urgent requirements for performance and robustness enhancement of control system. Considering the characteristics of multi-variables, strong coupling and complex nonlinearity, a nonlinear state feedback structure is developed based on feedback linearization technique, which is… (More)

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@article{Kun2016RobustnessOA, title={Robustness optimization approach for hypersonic vehicle controller based on parallel computing}, author={Ni Kun and Zhang Qingzhen and Cheng Lin}, journal={2016 Chinese Control and Decision Conference (CCDC)}, year={2016}, pages={4072-4078} }