DocumentCode
3492331
Title
New method to build a satellite vibration simulation platform with six degrees of freedom
Author
Ni, Xiaolong ; He, Jingyi ; Kong, Yue ; Shi, Haodong
Author_Institution
Inst. of Space Opt. Technol., Changchun Univ. of Sci. & Technol., Changchun, China
fYear
2012
fDate
23-25 Aug. 2012
Firstpage
276
Lastpage
279
Abstract
In the research of space-borne platform vibration, There are some problems such as modeling complex, bad realtime, long modeling cycle, hard to deployment exists in the traditional simulation method. Combining with the theory of six axis parallel positioning platform and multidiscipline physical modeling and simulation tools Maplesim, adopts the non-causal modeling method to set up a satellite vibration simulation platform with six degrees of freedom, by defining the acceleration and angle acceleration of the centroid of the platform to generation the simulation data quickly and accurately. The new method solved the problems existing in the traditional simulation method and provide a new method to model the Space-borne platform model quickly and a new way to test the Control system.
Keywords
aerospace simulation; artificial satellites; attitude control; vibrations; Maplesim; angle acceleration; modeling complex; modeling cycle; multidiscipline physical modeling; noncausal modeling method; satellite vibration simulation platform; simulation tools; six axis parallel positioning platform; space-borne platform vibration; Acceleration; Data models; Fasteners; Load modeling; Mathematical model; Satellites; Vibrations; satellite vibration; six axis parallel platform; son-causal modeling;
fLanguage
English
Publisher
ieee
Conference_Titel
Optoelectronics and Microelectronics (ICOM), 2012 International Conference on
Conference_Location
Changchun, Jilin
Print_ISBN
978-1-4673-2638-4
Type
conf
DOI
10.1109/ICoOM.2012.6316272
Filename
6316272
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