整体式固体火箭冲压发动机与导弹一体化优化设计专家系统  

THE EXPERT SYSTEM FOR INTEGRATED OPTIMIZATION DESIGN OF DSRR AND ITS MISSILE

作　　者：何洪庆[1] 黄生洪[1] 

机构地区：[1]西北工业大学航天工程学院,西安710072

出　　处：《宇航学报》2000年第z1期70-76,共7页Journal of Astronautics

基　　金：航空基金资助项目!编号 96D53 0 50;国家 2 1 1工程建设项目

摘　　要：根据整体式固体火箭冲压发动机与导弹一体化优化设计领域的研究特点、现状 ,首次提出了以专家系统、数据库技术为核心的软件解决方案。在此基础上研究了辅助参数决定 ,自动查询数据库 ,监控计算等专家系统应用的具体环节 ,并提供了计算的实例和结果。A software solution to full development of the integrated optimization design of the Ducted Solid Rocket Ramjet(DSRR) and its missile is proposed in the first time, which is characterized by applying Expert Systems(ES) and Database technology. The detailed links of applying ES in integrated optimization design of DSRR & its missile have been investigated, including helping to determine key parameters, automatic querying database, monitoring and controlling calculating. One example and it's result are provided.

关 键 词：固体火箭冲压发动机 导弹一体化 优化设计 专家系统 数据库 多线程编程 

分 类 号：V4-55[航空宇航科学技术]