Aerodynamic numerical analysis with linear matrix inequality theorem of intelligent control

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	Advances in Aircraft and Spacecraft Science Volume 10, Number 2, March 2023 , pages 159-177 DOI: https://doi.org/10.12989/aas.2023.10.2.159
	Full Text PDF Aerodynamic numerical analysis with linear matrix inequality theorem of intelligent control
	C.C. Hung and T. Nguyễn
Abstract
	In this paper we proposed the aerodynamic numerical analysis with linear matrix inequality theorem of intelligent control, which is believed to be applicable in the application not only a function of the block size and reduced wind speed but itself depends on both the size and the aspect ratio of the structure, not on the total scruton number. In order to improve the accuracy of the results, the optimization curve was optimized for the test to evaluate the response in the time of achieving the results and we focus on the results that found a significant influence from the assumptions used for damage propagation for aircraft structural analysis of composite materials. Finally, the numerical simulations confirmed the effectiveness of the method.
Key Words
	aerospace vehicles; LMI; nonlinear systems; smart control; stability analysis
Address
	C.C. Hung: Faculty of National Hsin Hua Senior High School, Tainan, Taiwan T. Nguyễn: Ha Tinh University, Dai Nai Campus: No. 447, Street 26/3, Dai Nai Ward, Ha Tinh City, Vietnam