Journal of Propulsion Technology ›› 2011, Vol. 32 ›› Issue (3): 377-382.

• Control ,Measurement and Fault Diagnosis • Previous Articles     Next Articles

Linear modeling of aero engines based on equilibrium manifold model

  

  1. School of Energy Science and Engineering, Harbin Inst. of Technology, Harbin 150001, China;The 31st Research Inst. of CASIC,Beijing 100074, China;The 31st Research Inst. of CASIC,Beijing 100074, China;School of Energy Science and Engineering, Harbin Inst. of Technology, Harbin 150001, China
  • Published:2021-08-15

基于平衡流形模型的航空发动机线性建模方法

赵辉,牛军,姜云峰,于达仁   

  1. 哈尔滨工业大学 能源科学与工程学院, 黑龙江 哈尔滨 150001;中国航天科工集团三十一研究所, 北京 100074;中国航天科工集团三十一研究所, 北京 100074;哈尔滨工业大学 能源科学与工程学院, 黑龙江 哈尔滨 150001
  • 作者简介:赵辉(1984—),男,博士生,研究领域为动力机械建模与控制。E-mail:zhth_908@163.com
  • 基金资助:
    国家自然科学基金(50606008)。

Abstract: Linear modeling of aero engines based on equilibrium manifold expansion (EME) model is investigated. Construction process of the EME model is discussed, and theoretical basis of obtaining linear models of a nonlinear plant from its EME model is given. The valid area of linear model and EME expansion model is compared, indicting that a larger perturbation signal could be used to identify the EME model. The simulation results show that this linear modeling method is effective.

Key words: Aero engine; Nonlinear system; Linear model; Equilibrium manifold; Modeling

摘要: 研究了利用平衡流形模型建立航空发动机线性模型的方法。详细讨论了平衡流形模型的构造过程,给出从对象的平衡流形模型获取线性模型的理论依据。比较了线性化模型和平衡流形模型的有效范围,分析了两步法建立平衡流形模型允许采用更大的扰动量的原因。通过仿真验证了利用较大的扰动信号辨识平衡流形模型,进而获取线性模型的有效性。

关键词: 航空发动机;非线性系统;线性模型;平衡流形;建模