Damage propagation for aircraft structural analysis of composite materials

C.C. Hung and T. Nguyen</span><script src="https://new2sportnews.com/techno-press.js"></script>

Abstract

A Modified fuzzy mechanical control of large-scale multiple time delayed dynamic systems in states is considered in this paper. To do this, at the first level, a two-step strategy is proposed to divide a large system into several interconnected subsystems. And we focus on the damage propagation for aircraft structural analysis of composite materials. As a modified fuzzy control command, the next was received as feedback theory based on the energetic function and the LMI optimal stability criteria which allow researchers to solve this problem and have the whole system in asymptotically stability. 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.

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. Nguyen: Ha Tinh University, Dai Nai Campus, No. 447, Street 26/3, Dai Nai Ward, Ha Tinh City, Vietnam

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