Parameters Modeling and Fault Simulation for Flight Control System Based on SIMULINK

被引：0
作者：
Li, Sujie [1 ,2 ]
Su, Haixia [1 ,2 ]
Zhang, Guigang [1 ,2 ]
Wang, Jian [1 ,2 ]
机构：
[1] Chinese Acad Sci, Inst Automat, Beijing, Peoples R China
[2] Shanghai Engn Res Ctr Civil Aircraft Hlth Monitor, Shanghai, Peoples R China
来源：
2017 PROGNOSTICS AND SYSTEM HEALTH MANAGEMENT CONFERENCE (PHM-HARBIN) | 2017年
关键词：
flight control system; simulation model; fault simulation; Simulink; DAMAGE;
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
The establishment of flight control system parameters modeling and fault simulation is the basis of fault diagnosis. In this paper, the flight control system simulation model is established by MATLAB / SIMULINK. We describe the modules and implementation methods of the flight control system parameters modeling in detail. In addition, the simulation of the failure mode and realization is introduced. Finally, we do some simulations and make some analysis to the simulation results. The simulation results show that our methods are well.
引用
收藏
页码：1121 / 1127
页数：7
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