Volume 34 Issue 10
Oct.  2019
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QIAN Qiumeng, DAN Zhihong, ZHANG Song. Linear active disturbance rejection control method for intake pressure control in aero-engine transient test[J]. Journal of Aerospace Power, 2019, 34(10): 2271-2279. doi: 10.13224/j.cnki.jasp.2019.10.021
Citation: QIAN Qiumeng, DAN Zhihong, ZHANG Song. Linear active disturbance rejection control method for intake pressure control in aero-engine transient test[J]. Journal of Aerospace Power, 2019, 34(10): 2271-2279. doi: 10.13224/j.cnki.jasp.2019.10.021
shu

Linear active disturbance rejection control method for intake pressure control in aero-engine transient test

doi: 10.13224/j.cnki.jasp.2019.10.021
  • 1.

    Sichuan Gas Turbine Establishment,Aero Engine Corporation of China,Mianyang Sichuan 621000,China

  • 2.

    Science and Technology on Altitude Simulation Laboratory,Sichuan Gas Turbine Establishment,Aero Engine Corporation of China,Mianyang Sichuan 621000,China

  • 3.

    Science and Technology on Altitude Simulation Laboratory,Sichuan Gas Turbine Establishment,Aero Engine Corporation of China,Mianyang Sichuan 621001,China

  • Received Date: 2019-01-19
  • Publish Date: 2019-10-28
    Abstract
  • When aero-engine received transient test in altitude test facility, the intake control system was abnormally affected and the quality of intake pressure control couldn’t be improved by conventional control methods, so an intake pressure control method based on linear active disturbance rejection was proposed. The high-intensity intake control system simulation platform was built through mechanism simulation and system identification, and the linear active disturbance rejection law was designed to estimate and compensate engine disturbance in real-time manner. An intake pressure control method with active rejection mechanism was formed. Meanwhile, considering the switching problem between manual and automatic control or between different control laws in actual use, an practical bumpless transfer method was designed. Simulation results compared with PID showed that the intake pressure can be quickly converged and stabilized, meanwhile, the maximum deviation was reduced from 7.69kPa to 0.9kPa. So this method achieves good control effect without engine information and can greatly improve intake pressure control quality in transient test.

     

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