Journal of Projectiles, Rockets, Missiles and Guidance >
Investigation of Missile Position Testing System Based on PC104 Bus
Received date: 2009-10-13
Online published: 2025-05-28
A novel missile position testing system based on PC104 control bus and embedded operating system Windows CE was proposed. The testing principle was investigated. Except the design of hardware, the application of multiple thread technology to system software development was suggested. The testing results indicate that the system guarantees accurate simulation of the launching process, and can automatically test multiple channels and many kinds of relative signal. It offers effective solution to missile fault positioning.
Key words： embedded operating system; PC104-bus; testing system; Windows CE
YAN Shuqun , MU Yongmin , LUO Yuhui , LI Yugang , YUAN Guogang . Investigation of Missile Position Testing System Based on PC104 Bus[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(4) : 214 -216 . DOI: 10.15892/j.cnki.djzdxb.2010.04.046
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