Modified algorithmic LMI design with applications in aerospace vehicles

Tim Chen , Anzaldi Gu , Chiayen Hsieh , Giustolisi Xu , Cheng Wang , C.Y.J. Chen

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. 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. Modeling the Fisher equation and the temperature gauge for high-speed aircraft and spacecraft shows that the calculation method is efficient.

Key Words

aerospace vehicles, LMI, smart control, nonlinear systems, stability analysis

Address

Tim Chen — Faculty of Information Technology, Ton Duc Thang University, Ho Chi Minh City, Vietnam
Anzaldi Gu, Giustolisi Xu and Cheng Wang — Department of Control Engineering, Technical University of Bari, Via E. Orabona, 4, 70125 Bari, Italy
Chiayen Hsieh — Education College, National Kaohsiung Normal University, Taiwan, Hwa-Shih Education College, Da Hsueh Rd, Shou-Feng, Hualien, Taiwan
C.Y.J. Chen — Key Lab Measurement & Control Complex System Engineering, Barcelona Digital Technology Centre, Barcelona, Spain

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