An Automatic Test System for Missile Control System
This paper presents an automatic test system for missile control system based on modern computer technology. The test system is built in master and slave structure. Its data acquisition is achieved by a slave computer, and data analysis at master computer. The software at the master side is developed via LabWindows/CVI of National Instruments, and that of slave is in a real time environment. They exchange instructions and data via RS232 and TCP/IP protocols. Experimental results show that this kind of automatic test system is more flexible and extendable than traditionally function-fixed instruments and easy to upgrade as test requirement changes.
Virtual Instruments Automatic Test System Master and Slave Structure
WU xun YANG Shuxing ZHAO Lei
School of Aerospace Science and Engineering, Beijing Institute of Technology School of Aerospace Sci College of Computer Science and Technology, Shandong University of Technology
国际会议
北京
英文
2007-08-05（万方平台首次上网日期，不代表论文的发表时间）