运载火箭飞行控制软件可重用架构设计方法研究  

Research of the Reusable Architecture Design Method for the Flight Control Software of Launch Vehicle

作　　者：霍宏[1] 刘俊阳[1] 李兰兰[1] 刘学士 Huo Hong;Liu Junyang;Li Lanlan;Liu Xueshi(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》2018年第3期63-70,78,共9页Aerospace Control

摘　　要：面对运载火箭飞行控制软件规模和复杂程度急剧增加、研制周期越来越短的现状,如何运用新的软件开发模式替换传统的研制模式,来提高飞行控制软件的研制效率已成为当前的研究重点。应用可重用软件开发技术能够有效提高软件研制效率,对提高运载火箭飞行控制软件的设计质量和缩短研制周期具有重要的意义。本文基于可重用软件开发技术在需求分析、概要设计和详细设计阶段的具体内容,提出了一种运载火箭飞行控制软件可重用架构设计方法,从而用于提高设计效率,降低维护成本,对运载火箭飞行控制软件研制具有较强的应用价值。Regarding the situation of the flight control software of launch vehicle that the function is complicated and the development cycle is short,How to improve the development efficiency by the new software development model which is used instead of the traditional method has become a hot topic. The reusable software development which can improve the developing efficiency can cast light on the design of the flight control software of launch vehicle. Based on the contents of reusable software development during the stages of the requirement analysis,the summary design and the detail design,the reusable architecture design method for the flight control software is proposed in this paper. It can improve the development efficiency and reduce the maintenance cost for the flight control software. The reusable architecture design method is also of great relevance to applications for the flight control software of launch vehicle.

关 键 词：可重用软件开发 飞行控制软件 架构设计方法 

分 类 号：TP302[自动化与计算机技术—计算机系统结构]