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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2008, Vol. 29 ›› Issue (4): 776-780.

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Nonlinear Model Predictive Control for Turboshaft Engine

Yao Wenrong, Sun Jianguo   

  1. College of Energy and Power Engineering, Nanjing University of Aeronautics and  Astronautics
  • Received:2007-06-22 Revised:2008-03-25 Online:2008-07-10 Published:2008-07-10
  • Contact: Sun Jianguo

Abstract:

A controller of a turboshaft engine is designed by the nonlinear model predictive control (NMPC) method. The model predictive control system is mainly comprised of three parts: a predictive model, its online optimization and feedback correction. A neural network model is used to predict the dynamic response of the turboshaft engine and generate the predictive model of the NMPC; the sequential quadratic programming (SQP) optimization algorithm is used to optimize the fuel flow of the turboshaft engine online; the error between the neural network model output and the real engine output is used to correct by feedback, the reference of the controller. Finally, a digital simulation is performed, which shows that compared with the serial PID controller the overshoot of the NMPC controller is reduced from 2.2% to 0.8%, and the response time is reduced from 6 s to 2 s. So the NMPC controller has better control quality.

Key words: turboshaft , engine,  , NMPC,  , SQP,  , neural , network , model,  , feedback , correction

CLC Number: