摘要
从运载火箭控制系统工程需求出发，在研究总线技术及其在航天领域中的应用背景的基础上，分析了箭上控制系统总线应用技术的可靠性和必要性，提出了箭上总线控制系统的基本模型，探讨了箭上总线开发、应用、系统设计等有关技术问题。
From the demand of the control system project of launch vehicle and based on the bus technique with its application background in aerospace and aeronautic area, feasibility and requirement of the bus application technique in the control system of rocket were analysed.The basic model of the bus - based control system was presented. Some technical matters on development application and system design on the bus of rocket were discussed.
出处
《航天控制》
CSCD
北大核心
1997年第3期16-21,15,共7页
Aerospace Control
