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Constrained Model Predictive Control for Generation Power Distribution on Aircraft Engines

Author

Listed:
  • Lingfei Xiao

    (College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

  • Yushuo Tan

    (College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

  • Robert R. Sattarov

    (Institute of Digital Systems, Automation and Energy, Ufa State Petroleum Technological University, 450064 Ufa, Russia)

  • Ye Wei

    (College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

Abstract

Aiming at the increasing demand for electric energy in aircraft in the future, a multi-objective optimization aircraft engine constrained model predictive control method based on generation power distribution is proposed. Firstly, based on the aircraft engine component level model and the equilibrium manifold theory, the aircraft engine equilibrium manifold expansion model is established. Secondly, the influence of the power generation is modeled, and the influence of the low- and high-pressure shaft generators on the normal operation of the aircraft engine is studied and compared. The control variables such as fuel flow and total generation power are taken as the constraint conditions to design the constraint model predictive controller. Furthermore, the multi-objective grey wolf optimization algorithm is introduced to intelligently optimize the parameters of the designed controller. At last, the simulation based on the component level model shows that the high-pressure shaft generator has less influence on the state quantity, including engine thrust, than the low-pressure shaft generator. The proposed control method using the multi-objective gray wolf optimization (MOGWO) algorithm has rapid response and no steady-state error.

Suggested Citation

  • Lingfei Xiao & Yushuo Tan & Robert R. Sattarov & Ye Wei, 2024. "Constrained Model Predictive Control for Generation Power Distribution on Aircraft Engines," Energies, MDPI, vol. 17(18), pages 1-16, September.
    • Handle: RePEc:gam:jeners:v:17:y:2024:i:18:p:4533-:d:1474759
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    References listed on IDEAS

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    1. Chengkun Lv & Ziao Wang & Lei Dai & Hao Liu & Juntao Chang & Daren Yu, 2021. "Control-Oriented Modeling for Nonlinear MIMO Turbofan Engine Based on Equilibrium Manifold Expansion Model," Energies, MDPI, vol. 14(19), pages 1-24, October.
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