Study on Architecture of Missile Design Service Platform Based on Virtual Design Unit

Article Preview

Abstract:

To solve the problems which refer to share of design resources, and realize reasonable matching of design ability in the collaborative design process of complex product, a new Missile Design Service Platform based on Virtual Design Unit (MDSP-VDU) is proposed. Firstly, main function modules and characteristics of MDS-VDU are described. Secondly, key technologies including design resource virtualization, Virtual Design Unit construction, service description rules design services separation and combination,design process customization, VDUs scheduling are introduced. Thirdly, prototype system of MDS-VDU is built and displayed. Some theories about MDS-VDU have been applied in the implementation of missile design service platform and virtual resource management system in the Group-oriented enterprise CMfg Platform. Finally, application results show that MDSP-VDU is feasible.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 655-657)

Pages:

2057-2064

Citation:

Online since:

January 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Hongyu XIE, Weihua ZHANG and Zhongwei WANG: submitted to Journal of Propulsion Technology (2007).

Google Scholar

[2] Guozheng LI, Min CHEN and Weihua ZHANG: submitted to Journal of Projectiles, Rockets, Missiles and Guidance (2008).

Google Scholar

[3] Bo Li, Hong Liu and Xinhua Lin: submitted to Computer Applications and Software (2008).

Google Scholar

[4] Nianmeng Luo, Qifu Wang and Liping Chen: submitted to Mechanical Science and Technology (2006).

Google Scholar

[5] Fei Xiao, Zhe Gan, Min Chen, Weihua Zhang: Proceedings of the 2008 IEEE International Conference on Information and Automation (2008), p.1681.

DOI: 10.1109/icinfa.2008.4608275

Google Scholar

[6] Ryan P. Starkey: 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2590, (2008).

DOI: 10.2514/misphst08

Google Scholar

[7] Yuzhu Fan, Weihua Zhang and Zhongwei Wang: submitted to Journal of National University of Defense Technology (2012).

Google Scholar

[8] Bohu LI, Lin Zhang and Shilong Wang: submitted to Computer Integrated Manufacturing Systems (2010).

Google Scholar

[9] Chunsheng Hu, Chengdong Xu and Xiaobo Cao: submitted to Applied Mechanics and Materials, Frontiers of Manufacturing and Design Science (2012).

Google Scholar

[10] Xiaobo Cao, Chengdong Xu and Chunsheng Hu: submitted to Computer Integrated Manufacturing Systems (2012).

Google Scholar

[11] Lei Ren, Lin Zhang and Yabin Zhang: submitted to Computer Integrated Manufacturing Systems (2011).

Google Scholar

[12] Ye Liu, Minghua Shi: Computer Integrated Manufacturing Systems (2011).

Google Scholar

[13] Eugene L. Fleeman: 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (2008), AIAA 2008-4908.

DOI: 10.2514/mjpc08

Google Scholar

[14] Jiasheng Wu, Juanmian Miao in: Aerodynamic Configuration and Characteristics of Guided Weapons, edited by National Defence Industrial Press, Beijing (2008), in press. (In Chinese).

Google Scholar

[15] Xianshi Yuan, Chao Gao and Jiang Nan: Journal of Projectiles, Rockets, Missiles and Guidance (2010).

Google Scholar