Design and Realization of Architecture for Launch Vehicle Test and Simulation System

摘要：

Adopting the Space launch vehicle virtual test platform as research object, and focusing on the key functional demand of distributed virtual test based on numerical simulation, a new architecture based on the Model Driven Architecture (MDA) and High Level Architecture (HLA) is discussed. In the vertical, it separates the federate members logic behavior and code integrated manner, so that the work of developing the platform independent model and platform specific model can be finished at the same time. In the horizontal, the using of HLA can partially achieve the reusability of the models. So the benefit using MDA and HLA in simulation is the reusability and interoperability of the models in whole lifecycle of the software. Using the Measurement Studio to develop the virtual instruments can improve the realtime performance and the architecture based on the MDA and HLA can meet the demands of the Launch Vehicle Test and Simulation System.

关键词： launch vehicle virtual test model driven architecture high level architecture measurement studio

作者: Tongtong Ren Hui Li Kun Zhang Chun Yang

作者单位: Institute of Astronautics and Aeronautics University of Electronic Science and Technology of China C Xichang Satellite Launch Center, Xichang 615000, China Xinjiang Petroleum Company, Karamay 834000, China

会议类型: 国际会议

会议名称: 2009 International Workshop on Information Security and Application(2009 信息安全与应用国际研讨会)

会议地点: 青岛

会议语种:英文

页码: 643-645

在线出版日期: 2009-11-21（万方平台首次上网日期，不代表论文的发表时间）