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航空液压系统配电仿真分析
引用本文:陈垚.航空液压系统配电仿真分析[J].商洛师范专科学校学报,2014(2):13-16.
作者姓名:陈垚
作者单位:[1]西北工业大学机电学院,陕西西安710072 [2]商洛学院电子信息与电气工程学院,陕西商洛726000
摘    要:对液压系统参数变化影响电网进行了分析,采用单设备实验测检与系统配电仿真相结合的方式,设计了航空液压系统用电仿真模型,并在SIMULINK下搭建模型进行仿真。该模型通过单设备实验测试获得参数曲线,避免了理论建模时由于条件假设产生的误差,使仿真结果更接近实际情况。该仿真方法不仅提高了仿真速度,还简化了系统模型,仿真结果与实验结果近似,具有工程应用前景。

关 键 词:数学建模  液压系统  仿真

The Simulation Analysis of Power Supply on Hydraulic Pressure System in Aviation
CHEN.The Simulation Analysis of Power Supply on Hydraulic Pressure System in Aviation[J].Journal of Shangluo Teachers College,2014(2):13-16.
Authors:CHEN
Institution:CHEN Yao (1. School of Mechatronics, Northwestern Polytechnical University, Xi'an 710072, Shaanxi; 2.College of Electronic Information and Electrical Engineering, Shangluo University, Shangluo 726000, Shaanxi)
Abstract:Variation of the hydraulic system parameters were analyzed. The aviation hydraulic system simulation model is designed by combining experimental data for a single device and system distribution simulation. The model was simulated with SIMULINK. The models that are made based on the experimental data will be more realistic than theoretical modeling. The simulation method can not only improve the simulation speed, but also simplifies the system model. The simulation results are approximate to the experimental data. The modeling method has engineering application prospect.
Keywords:mathematic model  hydraulic pressure system  simulation
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