2 April 2010 A distributed MDO architecture and its application on small satellite
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Proceedings Volume 7651, International Conference on Space Information Technology 2009; 76513U (2010) https://doi.org/10.1117/12.855274
Event: International Conference on Space Information Technology 2009, 2009, Beijing, China
Abstract
This paper introduces the technical feature of a former developed MDO (Multidisciplinary Design Optimization) architecture for spacecraft design, which is called Spacecraft Distributed Design Environment (SDIDE). SDIDE is an interactive spacecraft design system based on distributed network computing environment. It applies MDO in the whole lifecycle of spacecraft design, and makes nearly all kinds of system-level and discipline-level analysis tools work collaboratively. SDIDE uses a flexible bus scheme based on Common Object Request Broker Architecture (CORBA) to improve the integration and efficiency. The paper takes the structural optimization of the Tsinghua University "NS-1" small satellite as an example to illustrate the usage of the software system of SDIDE in assisting the overall design of satellite. The result of calculation shows that the software system can effectively decrease the cost of developing a satellite system and improve the overall performance of the satellite, accordingly proving the practicality and feasibility of the SDIDE architecture into the design process of a spacecraft.
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Zheng You, Zheng You, Guanhua Li, Guanhua Li, Junming Fu, Junming Fu, } "A distributed MDO architecture and its application on small satellite", Proc. SPIE 7651, International Conference on Space Information Technology 2009, 76513U (2 April 2010); doi: 10.1117/12.855274; https://doi.org/10.1117/12.855274
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