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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:CUI Ping-yuan,LIPeng,CuiHuTao.Motion modeling and formation form analysis of spacecraft near collinear libration points[J].Journal of Harbin Institute Of Technology(New Series),2009,16(5):687-692.DOI:10.11916/j.issn.1005-9113.2009.05.019.
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Motion modeling and formation form analysis of spacecraft near collinear libration points
Author NameAffiliation
CUI Ping-yuan Deep Space Exploration Research Center,Harbin Institute of Technology,Harbin 150080,China 
LIPeng Deep Space Exploration Research Center,Harbin Institute of Technology,Harbin 150080,China 
CuiHuTao Deep Space Exploration Research Center,Harbin Institute of Technology,Harbin 150080,China 
Abstract:
To meet the increasing research demand for deep space exploration,especially for the second libration point (L2) conditional periodic orbit (Halo orbit) in the Sun-Earth system,the methods to get analytical Halo orbit and differential-correction Halo orbit were described firstly,and the corresponding orbits accuracy was analyzed.Then,based on the results of third-order and differential-correction Halo orbits,the formation form was studied.Analysis was carried out to discuss the influence of system amplitude,initial phase,and phase difference on the formation form,as well as that of initial orbit values on form accuracy.Finally,some simulation results demonstrate the validity of the proposed methods.
Key words:  space exploration  collinear libration point  Halo orbit  formation flying form  analytical solution and differential-correction
DOI:10.11916/j.issn.1005-9113.2009.05.019
Clc Number:V47
Fund:

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