航天器综合测试系统设计  

Design of Spacecraft Overall Checkout System

作　　者：朱维宝[1] 孙波[1] 李砥擎[1] 

机构地区：[1]中国空间技术研究院总体部,北京100094

出　　处：《计算机测量与控制》2009年第8期1457-1459,1466,共4页Computer Measurement &Control

摘　　要：航天器功能及结构日趋复杂,对综合测试系统要求也越来越高,采用新一代测控技术,构建集中监控管理的分布式体系结构较好地解决了综合测试系统设计中面临的众多问题;提出了具有自动化程度高、通用性和扩展性强、集中监控管理特点的航天器综合测试系统设计方案;对航天器综合测试系统中各测试设备功能、组成及具体方案进行了详细介绍。Spacecraft function and structure are increasingly complex, therefore the requirements of overall checkout system are increasingly more strict. Based on new generation of monitoring and control technologies, adoption of centralized monitoring and management distributed architecture can solve much problem in overall checkout system design. A solution of spacecraft overall checkout system which have characteristics with centralized monitoring and management, high degree of automation and versatility is put forward. The function and configuration of equipment in overall checkout system are detailed introduced.

关 键 词：综合测试系统 电性能测试 航天器 

分 类 号：TP274[自动化与计算机技术—检测技术与自动化装置]