一种弹载软件设计方法及其开发环境原型  

A Design Method of Missile-Borne Software and Development Environment Prototype

作　　者：黄士林[1] 石晓郁[2] 杨志斌[1] 胡凯[1] 胡建平[1] 

机构地区：[1]北京航空航天大学计算机学院,北京100083 [2]中国空空导弹研究院,河南洛阳471009

出　　处：《航空兵器》2009年第1期34-38,共5页Aero Weaponry

基　　金：航空科学基金(20060151003)

摘　　要：面向未来多目标、超远距的空空导弹发展需求,基于多处理器的分布式并行处理系统及其开发环境是弹载软件发展的方向。在保证系统可靠性、可移植性以及实时性的前提下,为提高软件开发效率、降低开发成本,对弹载软件系统的设计与开发方法有了更高的要求。本文基于新型航空嵌入式实时系统体系结构描述语言标准AADL,提出针对的弹载软件设计与分析的方法和基于实时中间件的方法,设计了面向用户的弹载软件开发支持环境的原型系统,从而可支持形成一体化的弹载软件设计、分析与开发框架。Corresponding to the future necessary ultra long range air-to-air missile attacking multi- target, distributed and parallel processor based on multi-processor and its development environment is the direction of missile-borne software. On the foundation of ensuring the reliability, portability and real-time responsibility, in order to increase the development efficiency and depress the development cost, missile- borne software development has higher requirement. Missile-borne software application design and analysis method based on a new type embedded real-time system of aerial architecture describe language is intro- duced, and user-oriented missile-borne software development environment prototype system based on VSI- PL and real-time middleware is designed. Missile-borne software development frame can be implemented by using this method and development Environment.

关 键 词：弹载嵌入式实时软件 AADL VSIPL++ 实时中间件 

分 类 号：TJ95[兵器科学与技术—武器系统与运用工程]