Advances in aircraft and spacecraft science

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Modified algorithmic LMI design with applications in aerospace vehicles

  • Chen, Tim (Faculty of Information Technology, Ton Duc Thang University) ;
  • Gu, Anzaldi (Department of Control Engineering, Technical University of Bari) ;
  • Hsieh, Chiayen (Education College, National Kaohsiung Normal University, Taiwan, Hwa-Shih Education College) ;
  • Xu, Giustolisi (Department of Control Engineering, Technical University of Bari) ;
  • Wang, Cheng (Department of Control Engineering, Technical University of Bari) ;
  • Chen, C.Y.J. (Key Lab Measurement & Control Complex System Engineering, Barcelona Digital Technology Centre)
  • Received : 2019.12.05
  • Accepted : 2020.11.23
  • Published : 2021.01.25
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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.

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References

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