摘要
主机控制软件是运载火箭一体化测发控系统的关键环节,测试流程可配置是主机控制软件的重要研究方向;针对现役CZ-2D、CZ-4B/C一体化测发控系统主机软件测试流程不可配置、软件代码更改频繁、升级次数多、管理成本高等问题,新一代主机控制软件以简易、可靠、快速可配置、界面友好为主要特征,通过采用"抽象一级基础文件、拼装二级测试文件、独立发送器接收器、网络协议映射"的软件架构开发策略,结合现役主机控制软件优点、新一代测发控软件系统要求、通信类型、接口定义等,实现了新一代可配置主机控制软件,为未来主机控制软件的研究打下了技术基础。
Host control software is the key link of the launch vehicle integrated measurement and control system,Test process configurability is an important research direction of host control software.For the current CZ-2D、CZ-4B/C integrated measurement and control system host control software test process is not configurable,software code changes frequently,upgrade several times,high management costs,etc.The new generation of host control software is simple、reliable and fast Configurable,userfriendly features,Through the use of abstract first-level basic data files,assembled secondary test files,independent transmitter receivers,network protocol mapping software architecture development strategy,combined with the advantages of active host control software,a new generation of measurement and control system requirements,communication types,interface definitions etc,realized a new generation of host control software and laid the technical foundation for the future research of host control software.
作者
于大海
袁杰
白亮
向军
丁景义
Yu Dahai;Yuan Jie;Bai Liang;Xiang Jun;Ding Jingyi(Shanghai Aerospace Electronic Technology Institute,Shanghai 201109,China)
出处
《计算机测量与控制》
2019年第4期102-105,共4页
Computer Measurement &Control
关键词
可配置
通用化
主机控制软件
一体化测发控系统
configurable
generalization
host control software
integrated measurement and control system
