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Proceedings of 2009 International Workshop on Information Security and Application (IWISA 2009)

Qingdao, China, November 21-22, 2009

Editors: Feng Gao and Xijun Zhu

AP Catalog Number: AP-PROC-CS-09CN004

ISBN: 978-952-5726-06-0

Page(s): 643-645

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

        Tongtong Ren, Hui Li, Kun Zhang, and Chun Yang

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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 real-time performance and the architecture based on the MDA and HLA can meet the demands of the Launch Vehicle Test and Simulation System.

Index Terms

launch vehicle, virtual test, model driven architecture, high level architecture, measurement studio

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