Volume 21 Issue 2
Apr.  2006
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Article Navigation >  Journal of Aerospace Power  > 2006  >  21(2): 421-426
ZHU Yu-bin, FAN Si-qi, LI Hua-cong, YANG Chui-bai. Research of Hybrid Optimization Method for Aeroengine Performance Seeking Control[J]. Journal of Aerospace Power, 2006, 21(2): 421-426.
Citation: ZHU Yu-bin, FAN Si-qi, LI Hua-cong, YANG Chui-bai. Research of Hybrid Optimization Method for Aeroengine Performance Seeking Control[J]. Journal of Aerospace Power, 2006, 21(2): 421-426.
shu

Research of Hybrid Optimization Method for Aeroengine Performance Seeking Control

  • 1.

    School of Engine and Energy, Northwestern Polytechnical University, Xi'an710072, China

  • 2.

    Center for Space Science & Applied Research, Chinese Academy of Sciences, Beijing 100080, China

  • Received Date: 2005-05-13
  • Rev Recd Date: 2005-11-16
  • Publish Date: 2006-04-28
    Abstract
  • According to the optimization control modes of aeroengine Performance Seeking Control(PSC),the aeroengine performance optimization problems which were described as a linear programming problem were studied.In respect that the linear programming may converge to a local minimum and nonlinear method is much more time comsuming,a hybrid algorithm based on Linear Programming(LP) and Model-Assisted Pattern Search(MAPS) was proposed in this paper.The hybrid optimization method was used for aeroengine control.Digital simulations were conducted at maximum thrust mode and minimum fuel consumption mode.Simulation results demonstrate that the engine performance can be improved further and calculation time can be reduced by using hybrid algorithm.

     

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    • References(6)
  • [1]
    Glenn B Gilyard,John S Orme.Performance Seeking Control:Program Overview and Future Directions[R].NASA TM-4531,1993.
    [2]
    Nobbs S G,Jacobs S W,Donahue D J.Development of the Full-Envelop Performance Seeking Control Algorithm[R].AIAA-92-3748,1992.
    [3]
    John S Orme,Glenn B Gilyard.Subsonic Flight Test Evaluation of A Propulsion System Parameter Estmation Process for The F100 Engine[R].AIAA-92-3745.
    [4]
    John S Orme,Glenn B Gilyard.Preliminary Supersonic Flight Test Evaluation of Performance Seeking Control[R].AIAA -93-1821.
    [5]
    Christopher M Siefert,Virginia Torczon,Michael W Trosset.Model-Assisted Pattern Search Methods for Optimizing Expensive Computer Simulations[R].JSM,2002.
    [6]
    Michael James Sasena,Flexibility and Efficiency Enhancements for Constrained Global Design Optimization with Kriging Approximations[D].Ph.D Dissertation,University of Michigan,2002.
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