摘要
分析并总结了导弹总体设计面临的应用集成问题。比较了目前主要的应用集成方法及其解决技术。结合集成框架技术、组件技术、过程建模技术等,提出了基于包装器的导弹总体设计应用集成框架。该框架基于C/S结构,重量级的服务器端对应用提供包装和组件发布的能力,设计人员在轻量级的客户端能够以一致的方式访问所有的包装后的应用组件。给出了基于文件包装器进行应用集成的具体实现过程,并通过实例验证了包装器集成框架的正确性和可行性。
The main problems of integration of heterogeneous applications existed in the general design process of missile were outlined. Some typical methods and solutions were compared and analyzed, such as data model mapping method, integrated framework and component based integration. Together with the actual requirements of application domain, the wrapper-based integration framework for missile general design was proposed. The framework has a C/S architecture, in which the applications are wrapped and published as components at rich server, and engineers can access the components through unified interface at thin client. The implementation of application integration with file wrapper mechanism was given in detail and a box-beam design example was used to demonstrate the wrapper-based integration framework for validity and feasibility
出处
《系统仿真学报》
EI
CAS
CSCD
北大核心
2006年第7期1810-1814,共5页
Journal of System Simulation
关键词
包装器
导弹总体设计
应用集成
集成框架
wrapper
missile general design
application integration
integration framework
