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Bi-index Constraints-Based Output Feedback Fault-Tolerant Control for Aero-Engine Distributed Control Systems

  • Research Article - Systems Engineering
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Abstract

With a focus on the aero-engine distributed control system (DCS) with parameter perturbation, Markov time delay, data packet dropout and external disturbance, a research has been carried out on DCS fault-tolerant control on condition of partial failure of actuator. First, a quantitative description of the system parameters is given, and the augmented model of the entire closed-loop system is established. Then the stability of the closed-loop system constrained by \(H_\infty \) and cost performance index is analyzed, and the method of designing optimal guaranteed cost fault-tolerant controller is proposed based on dynamic output feedback. Finally, the consistency theory of bi-index constraints is introduced, based on which the fault-tolerant controller is designed. The simulation results show that the designed controller can effectively reduce the controlling cost of the system while guaranteeing its \(H_\infty \) performance.

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Authors and Affiliations

  1. Aeronautics and Astronautics Engineering Institute, Air Force Engineering University, Xi’an, 710038, China

    Ledi Zhang, Litong Ren, Shousheng Xie, Yu Zhang & Lei Wang

  2. Aircraft and Power Engineering Institute, Aviation University of Air Force, Changchun, 130022, China

    Xianyu Zhang

Authors
  1. Ledi Zhang
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  2. Litong Ren
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  3. Shousheng Xie
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  4. Yu Zhang
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  5. Lei Wang
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  6. Xianyu Zhang
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Correspondence to Ledi Zhang.

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Zhang, L., Ren, L., Xie, S. et al. Bi-index Constraints-Based Output Feedback Fault-Tolerant Control for Aero-Engine Distributed Control Systems. Arab J Sci Eng 42, 2937–2946 (2017). https://doi.org/10.1007/s13369-016-2384-z

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  • DOI: https://doi.org/10.1007/s13369-016-2384-z

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