CAJ | 학술논문

针对弹载飞行控制软件研制现状，探讨软件重用的目的、意义及技术途径；结合弹载飞行控制软件的组成和设计原则，分析可重用软件应满足的基本条件；提出一种基于领域工程的弹载飞行控制软件重用实施方法；从软件工程化要求、编码要求、软件测试要求和硬件设计要求等方面建立弹载飞行控制软件通用构件库的可重用构件选取标准。最后，用实例说明了弹载飞行控制软件重用的可操作性。
침대탄재비행공제연건연제현상，탐토연건중용적목적、의의급기술도경；결합탄재비행공제연건적조성화설계원칙，분석가중용연건응만족적기본조건；제출일충기우영역공정적탄재비행공제연건중용실시방법；종연건공정화요구、편마요구、연건측시요구화경건설계요구등방면건립탄재비행공제연건통용구건고적가중용구건선취표준。최후，용실례설명료탄재비행공제연건중용적가조작성。
In view of the current status of Missile Flight Control Software ,this paper discusses the purpose and signifi‐cance of software reuse ,introduces the technical approaches of software reuse ;Combined with the composition and design principle of Missile Flight Control Software ,analysis of the basic conditions of software reuse should satisfy ;A kind of software reuse method through domain engineering on Missile Flight Control Software is proposed ;From these aspects , summed up criteria for the selection of Missile Flight Control Software of the general component library of reusable com‐ponents ,including requirements of software engineering ,the developer coding ,software testing and hardware designing . Finally ,an example is used to illustrate the operability of Missile Flight Control Software reuse .