The Simulation and Analysis of Fault Mode for Platform of Launch Vehicle
The paper puts forward the mathematical model of the platform of launch vehicle, and then analyzes the fault mode of the platform by changing parameters of the model for fault simulation. A kind of platform used in a launch vehicle is given, and its principle and structure are introduced. The mathematical model is established. The system is simulated using Matlab/Simulink. The normal and fault signals of the system are gotten. The failure mode is analyzed. This method can offer sample data for fault diagnosis in platform. It also provides a valid method of fault simulation for other parts of control system.
Launch vehicle stabilized platform fault mode fault simulation
ZHANG Bin SHEN Huairong ZHOU Weijing
Company of Postgraduate Management, the Academy of Equipment Command & Technology, Beijing 101416, C Department of Space Equipment, the Academy of Equipment Command & Technology, Beijing 101416, China
国际会议
第八届国际测试技术研讨会(8th International Symposium on Test and Measurement)
重庆
英文
789-792
2009-08-01（万方平台首次上网日期，不代表论文的发表时间）