Linear modeling of aero engines based on equilibrium manifold model
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
[2] 樊思齐.航空发动机控制[M].西安:西北工业大学出版社,2008. [3] 冯正平,孙健国.航空发动机小偏差状态变量模型的建立方法[J].推进技术1,2(1).(FENG Zheng-ping,SUN Jian-guo.Modeling of small perturbation state variable model for aeroengines[J].Journal of Propulsion Technology,1,2(1).) [4] 冯正平,孙建国,黄金泉,等.一种建立航空发动机状态变量模型的新方法[J].航空动力学报,8,3(4). [5] 孙健国.现代航空发动机多变量控制系统[M].北京:北京航空航天大学出版社,2005. [6] Frederick D K,Garg S, Adibhatla S.Turbofan engine control design using robust multivariable control technologies [J].IEEE Transactions on Control Systems Technology, 0,8(6). [7] 于达仁,隋岩峰.非线性系统平衡流形展开模型[J].系统仿真学报,6,8(9). [8] 于达仁,隋岩峰.涡轮发动机平衡流形展开模型[J].燃气轮机技术,6,9(2). [9] 隋岩峰,于达仁.涡轮发动机平衡流形展开模型辨识方法研究[J].航空学报,7,8(3). [10] 胡卫红,李述清,孙建国.基于非线性系统平衡流形的某型涡扇发动机建模研究[J].航空动力学报,0,5(1).
