运载火箭制导系统冗余设计技术研究  

Research for Redundant Technology of Launch Vehicle Guidance System

作　　者：胡云中[1] 

机构地区：[1]北京航天自动控制研究所

出　　处：《航天控制》1998年第2期10-15,共6页Aerospace Control

摘　　要：针对提高运载火箭飞行控制系统可靠性问题，从制导系统角度给出了两种系统级冗余方案，对其冗余配置、可靠性、冗余管理、故障检测和隔离、系统同步问题进行了讨论。To improve the reliability of flight control system of launch vehicle, two systemic redundant scheme are proposed in this paper at the view of guidance system. Moreover, research is delved in aspect of reliability, failure detection, redundant configuration and management as well as synchronous problem of the redundant system.

关 键 词：运载火箭 控制系统 冗余技术 故障检测 

分 类 号：V448.12[航空宇航科学与技术—飞行器设计]