导弹总体设计方案的快速生成方法  

Method of Missile Rapid Overall Design

作　　者：谷晓辉[1] 谷良贤[1] 龚春林[1] 杜可君 胡小军 

机构地区：[1]西北工业大学航天学院,陕西西安710072 [2]北京宇航系统工程研究所,北京100076

出　　处：《航空计算技术》2012年第6期99-102,106,共5页Aeronautical Computing Technique

基　　金：武器装备预言基金项目资助(9140A20100111HK0318)

摘　　要：研究导弹总体设计方案快速化的问题。由于导弹设计是一个多系统、多任务的复杂总体任务,难以有效提高导弹设计的效率。为了提高导弹总体设计的效率,提出一种基于库封装的方法对各学科计算模型进行集成。导弹设计中包含大量基础算法,通过将总体设计流程和各学科进行合理拆分,将通用的算法进行剥离封装,可有效地实现导弹设计的通用化和快速化。将各学科计算模型集成到总体设计平台下进行仿真,结果表明,合理的对学科模型进行拆分封装对实现导弹的高效化和通用化具有重要意义。Mission design is a complicated work due to its multi- system and various tasks. Thus it is quite difficult to improve the efficiency of missile design effectively. In order to enhance the speed of the missile overall design,the author demonstrates a kind of model integrated of different disciplines based on library encapsulation method. The mission design contains many basic algorithms and it is useful to realize the generality and speedy of mission design through reasonable split of the overall design process and various disciplines with the process of common algorithms＇ encapsulation. By emulation of various disciplines models under the overall design platform, the result shows that reasonable split and encapsulation of disciplines models is of great importance to the generality and speedy of mission design.

关 键 词：导弹总体设计 库封装 通用化 快速化 

分 类 号：TJ765.4[兵器科学与技术—武器系统与运用工程]