Applying GA Algorithm to the Modular Division for Distributed Reconfigurable Satellite System

Abstract:

For the problem of module division for distributed reconfigurable satellite system. A satellite function tree top-down is set up in this paper. And the genetic algorithm was applied in the module division. Finally the entire satellite was decomposed into various standard parts. In practice, users only need to combine those standard parts into a specific function module according to the requirements. Then send those modules into their orbit. And those modules through the way of formation flight, wireless connection to fulfill the task. Considering China's space development strategy, satellite systems long life and high reliability, upgrading, expansibility, satellite systems planning, running, production all kinds of uncertainty factors. Finally the satellite system was divided into 15 standard parts.

• Periodical: Applied Mechanics and Materials (Volume 482)
• Pages: 292-296
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.482.292
• Online since: December 2013
• Authors: Shuo Zhang, Guo Qiang Wu, Xiu Li Han, Rong Bo Cao, Yong Li, Qing Rui Zhou, Hui Wang
• Keywords: Distributed Reconfigurable Satellite System, F6, Function Tree, GA, Module Division

References

[1] M. G. O'neill, H. Yue, S. Nag, et al, Comparing and Optimizing the DARPA System F6 Program Value Centric Design Methodologies, AIAA SPACE 2010 Conference & Exposition, Anaheim, California, 30 August-2 September (2010).

DOI: 10.2514/6.2010-8828

[2] Yongjian Liu, Yuqiang Liu, Jun Shi, Chunlin Tan: Numerical optimization in Spacecraft module division. Chinese Space Science and Technology, 2012. 02.

[3] Sun Jie. Miniature spacecraft flexible and integrated design concepts and methods of. Harbin Institute of Technology . 2008. 06.

[4] Xiaoping Wang, Liming CAO. Genetic algorithm-theory, application and software implementation. Xi'an Jiaotong University Press . 2002. 01, p.3.