Design of a missile launcher test system based on virtual instrument

被引：0
|
作者：
Wang Chenggang [1 ]
Li Baogang [2 ]
Yang Fan [1 ]
Sun Jing [1 ]
机构：
[1] Naval Aeronaut & Astronaut Univ, Dept Basic Expt, Yantai 264001, Peoples R China
[2] Naval Aeronaut & Astronaut Univ, Dept Ordnance Sci & Technol, Yantai 264001, Peoples R China
来源：
PROCEEDINGS OF 2015 IEEE 12TH INTERNATIONAL CONFERENCE ON ELECTRONIC MEASUREMENT & INSTRUMENTS (ICEMI), VOL. 3 | 2015年
关键词：
virtual Instrument; PCI Bus; test system; multithreading;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
In order to meet the requirement of development and field test, a missile launcher test system is designed based on virtual instrument and PCI bus. The composition, working principle, hardware and software structure of the system are introduced. Some key techniques, such as multithreading technology, signal processing and data storage under Labwindows/CVI environment are expatiated. It has been used in development and experiment of a new missile launcher. Application proves that the system has the advantages of easy implementation, high reliability and good operability.
引用
收藏
页码：1415 / 1419
页数：5
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