基于网络技术的火箭发动机试验台控制测量系统设计与实现  

Design and Implementation of a Controlling and Measuring System for the Testing of Rocket Engines Based on Network Technology

作　　者：陈晖[1] 姜春林[1] 谢伦娅[1] 

机构地区：[1]国防科技大学航天与材料工程学院,湖南长沙410073

出　　处：《国防科技大学学报》2004年第4期27-30,共4页Journal of National University of Defense Technology

基　　金：国家863高技术资助项目(2003AA723073)

摘　　要：介绍了在WINDOWS2000平台下,基于网络技术的多功能火箭发动机试验台控制测量系统设计与实现。给出了系统的硬、软件结构,完成了系统的研制并通过试验验证了该系统。The design and implementation of a maltitask controlling and measuring system for the testing of rocket engines are presented. The system is developed under Windows2000,based on the network technology. The architectures of hardware and software of the system are described in detail .The system is implemented and its function is verified by the testings of engines.

关 键 词：控制系统 测量系统 局域网 驱动网 

分 类 号：V448.25[航空宇航科学与技术—飞行器设计]