Aircraft and spacecraft structural analysis with hybrid criterion of smart control

C.C. Hung , T. Nguyễn

Abstract

In this article, we propose a criterion for ensuring the asymptotic stability of large multiple delays, based on the direct Lyapunov method. Based on this criterion and distributed control scheme, the controllers are synthesized by the PDC to stabilize these large-scale systems with multiple delays. And we focus on the results which shows the high effective by the proposed theory utilized 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 — Department of Mechanical Engineering, National Taiwan University, Taiwan; 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

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