航天器远程测试系统设计与应用  

Design and Application of Spacecraft Remote Test System

作　　者：潘顺良[1] 张明江[1] 李鸿飞[1] 何永丛[1] 许宗飞[1] 

机构地区：[1]中国空间技术研究院载人航天总体部,北京100094

出　　处：《航天器工程》2015年第5期113-118,共6页Spacecraft Engineering

基　　金：国家重大科技专项工程

摘　　要：为解决航天器批量测试、高密度发射、多地并行测试等问题,提出了一种支持航天器综合测试的远程测试方案,即通过建立前后方高可靠的通信链路,配合前端设备和远程测试支持设备,将主要测试队伍和测试设备置于后方,有效精简前方设备和人员。文章分析了影响航天器远程测试的设计约束,设计了远程测试系统架构与部署,给出了航天器远程测试的工作模式,并通过航天器测试验证了系统的有效性。To solve the problem of highly-frequent spacecraft launch missions,mass-product test and multi-location parallel test,a scheme of spacecraft integration test based on remote test is proposed.Through the front and rear high-reliability Ethernet link and by support of rear SCOE and remote OCOE,the main test team and main equipment for the remote test system of spacecraft are allowed to stay in the rear,to reduce the front test team.The paper analyzes the design constraints of the spacecraft remote test,and designs the system architecture and deployment of the spacecraft remote test,and presented the work mode of the spacecraft remote test.The effectiveness of the spacecraft remote test system is verified by spacecraft integration test.

关 键 词：航天器综合测试 远程测试 自动化测试 

分 类 号：V556[航空宇航科学与技术—人机与环境工程]