基于插件的航天器测试总控软件系统设计  

Design of Software System Based on Plug-ins for Monitoring and Control in Spacecraft Testing

作　　者：余晟[1] 向永清[1] 宋宏江[1] 

机构地区：[1]北京空间飞行器总体设计部,北京100094

出　　处：《航天器工程》2015年第5期119-125,共7页Spacecraft Engineering

摘　　要：目前,我国测试总控软件系统存在总控核心软件版本较老、维护和升级困难、系统开放性不足、缺少统一的标准和规范等问题,文章提出了一种基于Java OSGi标准的插件化总控软件系统(PMCS),对PMCS软件的体系架构设计和技术路线进行了详细介绍。PMCS基于地面监视与控制模型(MCM),采用动态可配置的插件化体系结构,并将功能模块划分为核心模块和扩展模块,核心模块可在不同任务间通用,扩展模块可以根据需要进行灵活的部署和修改。经验证,文章提出的技术路线切实可行,可为我国地面总控软件系统的研发提供参考。The current monitoring and control software for spacecraft testing in our country has several drawbacks,such as old hardware and software platform,high complexity for maintenance and upgrade,closed software framework and lack of unified software specifications and standards.This paper proposes a design of a plug-in based monitoring and control software（PMCS）system,and introduces the architecture and technologies used in PMCS in details.PMCS is based on the monitoring and control model（MCM）of the ground monitoring and control system and consists of many dynamic and reconfigurable plug-ins The software modules of PMCS can be classified into kernel modules and reference modules.The kernel modules construct the common core among different tasks and the reference modules can be modified to meet specified needs.Through verification,the technique of PMCS is applicable,and PMCS can be used as a reference for the research and development of ground monitoring and control software in our country.

关 键 词：航天器测试 基于插件 总控软件 系统架构 

分 类 号：V556[航空宇航科学与技术—人机与环境工程]