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Reference and Limit Governors for Limit Protection of Turbofan Engines

Author

Listed:
  • Wenhao Xu

    (Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy & Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

  • Muxuan Pan

    (Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy & Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

  • Jiakun Qin

    (Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy & Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

  • Jinquan Huang

    (Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy & Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

Abstract

This paper proposes a novel architecture of limit protection including the references governors and limit governors and applies this architecture to limit protection in turbofan engines. References governors are designed as add-on schemes to a pre-stability engine control system that modifies reference commands to avoid constraints violation. Limit governors are proposed as an assistant part for references governors adjusting constraints to prevent references from stopping updates. The use of output admissible sets for a class of variable constraints is exploited to form invariant sets. Simulation results based on a turbofan engine model show that references governors with limit governors can effectively enforce the multiple constraints and provide enhanced engine thrust when steady violation occurs.

Suggested Citation

  • Wenhao Xu & Muxuan Pan & Jiakun Qin & Jinquan Huang, 2019. "Reference and Limit Governors for Limit Protection of Turbofan Engines," Energies, MDPI, vol. 12(14), pages 1-18, July.
  • Handle: RePEc:gam:jeners:v:12:y:2019:i:14:p:2803-:d:250299
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    References listed on IDEAS

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    1. Jiakun Qin & Jinquan Huang & Muxuan Pan, 2017. "An Optimal Augmented Monotonic Tracking Controller for Aircraft Engines with Output Constraints," Energies, MDPI, vol. 10(1), pages 1-17, January.
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    Cited by:

    1. Jiakun Qin & Muxuan Pan & Wenhao Xu & Jinquan Huang, 2019. "An Output-Based Limit Protection Strategy for Turbofan Engine Propulsion Control with Output Constraints," Energies, MDPI, vol. 12(21), pages 1-24, October.

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    1. Jiakun Qin & Muxuan Pan & Wenhao Xu & Jinquan Huang, 2019. "An Output-Based Limit Protection Strategy for Turbofan Engine Propulsion Control with Output Constraints," Energies, MDPI, vol. 12(21), pages 1-24, October.

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