Software design of missile integrated test system

被引:0
|
作者
Dai Jing [1 ]
Zhang Ping [1 ]
Li Xingshan [1 ]
Liao Canxing [1 ]
Wang Zongli [1 ]
机构
[1] BeiHang Univ, Sch Automat Sci & Elect Engn, Beijing 100083, Peoples R China
关键词
integrated test system; missile; multithreading; virtual instrument; power-on time;
D O I
10.1117/12.718066
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Based on virtual instrument, software design precept of missile integrated test system is proposed in this paper. The integrated test system software was developed under modular, intelligent and structured precept. In this way, the expansion capability of the test software is improved, and it is very convenient for second-development and maintenance. This test software is of higher-degree automation, its integrated test environment gives full play to the hardware platform of the missile integrated test system. In response to the specific hardware configuration of the test system and special missile test requirements, the application of test resources was optimized in the test procedure to improve test speed greatly and satisfy the power-on time limit for missile test. At the same time, by applying multithreading and hardware clock on a data acquisition card, accurate data acquisition, data calculating and data injecting can be completed in a millisecond to satisfy the harsh missile test requirement. This automatic test equipment can automatically test the nose cabin and control cabin only of a missile and a training missile; all the missile test items can be accomplished in a short period of time to enhance the efficiency and reliability of the test.
引用
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页数:7
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