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