摘要
介绍了一种以数据采集卡为底层硬件,基于VC++界面和MATLAB数据处理混合编程开发的虚拟仪器技术,并将它用于火箭发动机推进剂药柱粘弹性性能测试。结果表明,此方法开发周期短,效率高,开发的测试系统使用方便。
The paper presented a development method of virtual instrument technology, which used plug-in DAQ board as hardware and the hybrid program on the basis of VC + + interface and MATLAB data treatment. The method was used to measure the viscoelastic properties of the propellant grain. It was shown that the development method is quick, efficient and the developed measuring system is easy to operate.
出处
《固体火箭技术》
EI
CAS
CSCD
北大核心
2004年第1期84-86,共3页
Journal of Solid Rocket Technology
