Research on Modelling of Aviation Piston Engine for the Hardware-in-the-loop Simulation

被引：3
|
作者：
Yu, Bing [1 ,2 ]
Shu, Wenjun [1 ,2 ]
Bian, Wenchao [1 ,2 ,3 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Adv Aero Engine Collaborat Innovat Ctr, Nanjing 210016, Jiangsu, Peoples R China
[3] Shandong Jiaotong Univ, Coll Aeronaut, Jinan 250357, Peoples R China
来源：
2016 SECOND INTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING AND AUTOMATION SCIENCE (ICMEAS 2016) | 2016年 / 157卷
关键词：
D O I：
10.1088/1757-899X/157/1/012004
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In order to build the aero piston engine model which is real-time and accurate enough to operating conditions of the real engine for hardware in the loop simulation, the mean value model is studied. Firstly, the air-inlet model, the fuel model and the power-output model are established separately. Then, these sub models are combined and verified in MATLAB/SIMULINK. The results show that the model could reflect the steady-state and dynamic performance of aero engine, the errors between the simulation results and the bench test data are within the acceptable range. The model could be applied to verify the logic performance and control strategy of controller in the hardware-in-the-loop (HIL) simulation.
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页数：7
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