基于构件的点火控制软件设计  

Design of Ignition Control Software Based on Component

作　　者：杨振 马鹏飞 赵伟忠 YANG Zhen;MA Pengfei;ZHAO Weizhong(Shanghai Electro-Mechanical Engineering Institute,Shanghai 201109,China)

机构地区：[1]上海机电工程研究所,上海201109

出　　处：《现代防御技术》2023年第4期97-103,共7页Modern Defence Technology

摘　　要：针对飞行器点火控制软件不宜购买商用构件且需要个性化定制的需求,对飞行器点火控制原理进行了研究,并对多种飞行器的点火控制流程进行了抽象,设计了一种基于参数和动作的点火控制软件构件。该构件通过各个子构件之间的配合,利用对点火流程抽象得到的装订参数,可以适应多种不同飞行器的点火控制需求,实现点火控制软件的核心功能。将该构件应用于点火控制软件应用簇的研制,可以降低软件开发成本,有效地提升点火控制软件产品的质量。In view of the requirements that flight vehicle ignition control software is not suitable for purchasing commercial components and needs customized development,the ignition control principles of flight vehicles are studied.The ignition control processes of various flight vehicles are abstracted,and an ignition control software component based on parameters and actions is designed.These subcomponents can cooperate with each other,and the component needs parameters which reflect the characteristics of control process.This component can adapt to the ignition requirements of different systems and realizes the core function of ignition control software,which can reduce the software development cost and improve software quality efficiently in the meantime.

关 键 词：点火控制 软件复用 构件 结构 参数 抽象 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]