基于虚拟化的火箭测发控软件冗余技术  

Redundancy Technology of Rocket Test and Launch Control Software Based on Virtualization

作　　者：吕跃鹏 刘俊阳[1] 杨喆[1] Lv Yuepeng;Liu Junyang;Yang Zhe(Beijing Aerospace Automatic Control Institute,Beijing 100854,China)

机构地区：[1]北京航天自动控制研究所,北京100854

出　　处：《航天控制》2020年第3期61-68,共8页Aerospace Control

摘　　要：火箭测发控软件是地面的核心软件,其重点业务需要使用软件冗余技术来保障发射的可靠性。本文研究并提出一种基于B/S架构的测发控软件系统设计方案,并在虚拟化平台上实现软件冗余技术,以满足日益增长的对测发控软件可靠性的需求。Rocket test and launch control software is the core of the ground software.The key role is to use software redundancy technology to ensure the reliability of the launch.A design scheme of test and launch control software based on B/S architecture is studied and proposed,and software redundancy technology is implemented on the virtualization platform to meet the increasing demands for reliability of test and launch control software.

关 键 词：火箭测发控软件 虚拟化 软件冗余技术 

分 类 号：V554[航空宇航科学与技术—人机与环境工程]