于达仁的论著成果

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热心网友 时间：2022-06-21 10:14

[1]Yu Daren, Cui Tao, Bao Wen. An Idea of Distributed Parameter Control for Scramjet Engines. The Aeronautical Journal, vol. 111, no.1126, 787-796 2007
[2]Cui Tao, Yu Daren, Bao Wen. Distributed Parameter Control Arithmetic for an Axisymmetrical Dual-mode Scramjet. The Aeronautical Journal, Vol. 112, No.1135 2008
[3]Juntao Chang, Daren Yu, Wen Bao. Effects of Boundary Layers Bleeding on Unstart/Restart Characteristics of Hypersonic Inlets. The Aeronautical Journal, 2009, 113(1142).
[4]Chang J, Yu DR, Bao W, et al. Dimensionless analysis of the unstart boundary for 2D mixed hypersonic inlets. AERONAUTICAL JOURNAL Volume: 112 Issue: 1135 Pages: 547-555, 2008
[5]Cui Tao, Yu Daren, Chang Juntao,Bao wen. Topological Geometry Interpretation of Hypersonic Inlet Start/Unstart Based on Catastrophe Theory. AIAA Journal of Aircraft, vol. 45, no.4, 1464-1468 2008
[6]Yu Daren, Chang Juntao, Bao Wen. Optimal Classifications Criterions of Hypersonic Inlet Start/Unstart. AIAA Journal of Propulsion and Power ,23 (2) 2007
[7]Juntao Chang, Daren Yu, Wen Bao. A CFD Assessment of Classifications for Hypersonic Inlet Start/Unstart Phenomena. The Aeronautical Journal, 2009, 113(1141)
[8]Juntao Chang, Daren Yu, Wen Bao. Operation Pattern Classification of Hypersonic Inlets. Acta Astronautica, 2009, DOI: 10.1016/j.actaastro.2009.02.011, In Press
[9]Yu DR, Tao C, Wen B. Equilibrium manifold linearization model for normal shock position control systems. JOURNAL OF AIRCRAFT. Volume: 42 Issue: 5 Pages: 1344-1347, 2005
[10]Cui T, Yu D, Bao W, et al. Gain scheling control of nonlinear shock motion based on equilibrium manifold linearization model. CHINESE JOURNAL OF AERONAUTICS. Volume: 20 Issue: 6 Pages: 481-487 2007.
[11]Yu DR, Xu ZQ. Nonlinear coordinated control of drum boiler power unit based on feedback linearization. IEEE TRANSACTIONS ON ENERGY CONVERSION, Volume:20 Issue:1, Pages: 204-210, 2005.
[12]Daren Yu, Xiaofeng Liu, Wen Bao, Zhiqiang Xu. Multi-objective Robust Regulation and Protecting Control for Aero Engines. Journal of Engineering for Gas Turbines and Power, Accepted for publication.
[13]于达仁范轶.徐志强. 炉膛辐射能信号和热量信号的信息融合方法, 中国电机工程学报, 2003.4, 23(4),158-161
[14]于达仁刘强, 汽轮机调节系统卡涩故障的鲁棒诊断方法, 中国电机工程学报, 2003, ,23(3), :179-182
[15]于达仁王西田等 , 基于LMI方法多目标综合的H∞扭振模态观测器, 中国电机工程学报, 2002．10, 22(10),136-141
[16]于达仁杨永滨等, 大范围线性化最优鲁棒容错快关控制系统的设计, 中国电机工程学报, 2002.9, 22(9),25-29
[17]于达仁翁一武等, 火电单元机组的柔性控制, 中国电机工程学报, 2002.7, 22(7), 129-133
[18]于达仁徐志强等, 基于神经网络解耦线性化方法的锅炉主汽压力控制, 中国电机工程学报, 2002.5, 22(5),143-147
[19]于达仁，王建波等, Leak Fault Detection of Liquid Rocket Engine Based on Strong Tracking Filter, JOURNAL OF PROPUL- SION AND POWER, 2002.4, 18(2), 280-283
[20于达仁郭钰锋, 一次调频的随机过程分析, 中国电机工程学报, 2002．6, 22(6), 38-41
[21于达仁项庆华等, 汽轮机调节系统阀杆卡涩故障在线检测方法, 中国电机工程学报, 2001.12, 21, 59-62
[22]于达仁郭钰锋等, 发电机组并网运行一次调频的稳定性, 中国电机工程学报, 2000.9, 20, 59-63