摘要
以液氧加注控制系统为例，介绍液体运载火箭低温推进剂加注控制所采用的两级分布式系统。着重于描述液氧加注控制系统的结构原理、基本功能、设计特，并详细阐明了控制、检测及网络管理技术。
The two level distributed control system for cryogenic propellant loading is introduced,taking the Lox loading control system for example.The emphasis is put on description of the structure principle,basic functions,and design features of the system.Its technique of control,checkout and network management techniques are explained in detail.
出处
《导弹与航天运载技术》
1995年第5期26-32,共7页
Missiles and Space Vehicles
关键词
控制系统
液体推进剂火箭
加注系统
Ground equipment
Control system
Liquid propellent rocket.
