DocumentCode :
2574982
Title :
Simulation of spacecraft collision breakup debris
Author :
Li, Yiyong ; Shen, Huairong ; Yang, Lu ; Wang, Weijie
Author_Institution :
Dept. of Space Equip., Acad. of Equip. Command & Technol., Beijing, China
fYear :
2011
fDate :
27-29 June 2011
Firstpage :
1691
Lastpage :
1693
Abstract :
The simulation of spacecraft collision breakup debris is an important research content of spacecraft collision breakup problem. Based on existing models and other research results, functional requirements of simulating spacecraft collision breakup debris were analyzed, and its module composing and computing flow was designed. This software was implemented by MATLAB, VC & STK program techniques well. Finally, it was verified by simulation cases that design of this software was reasonable, and simulation results were creditable. The research is an important reference to study spacecraft collision breakup problem further.
Keywords :
aerospace computing; aerospace simulation; space vehicles; MATLAB; VC & STK program techniques; module composing flow; module computing flow; spacecraft collision breakup debris simulation; Computational modeling; MATLAB; NASA; Satellites; Space debris; Space vehicles; collision breakup; simulation; space debris; spacecraft;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Science and Service System (CSSS), 2011 International Conference on
Conference_Location :
Nanjing
Print_ISBN :
978-1-4244-9762-1
Type :
conf
DOI :
10.1109/CSSS.2011.5972199
Filename :
5972199
Link To Document :
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