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Related citation:Lipeng,CuiPingYuan,CuiHuTao.Spacecraft formation control strategy on Sun-Earth Lissajous orbit[J].Journal of Harbin Institute Of Technology(New Series),2009,16(6):805-809.DOI:10.11916/j.issn.1005-9113.2009.06.012.
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Spacecraft formation control strategy on Sun-Earth Lissajous orbit
Author NameAffiliation
Lipeng Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150080, China 
CuiPingYuan 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 carry out the deep space exploration tasks near Sun-Earth Libration point L2, the CRTBP dynamic model was built up and the numerical conditional quasi-periodic orbit (Lissajous orbit) was computed near L2. Then, a formation controller was designed with linear matrix inequality to overcome the difficulty of parameter tuning. To meet the demands of formation accuracy and present thruster’s capability, a threshold scheme was adopted for formation control. Finally, some numerical simulations and analysis were completed to demonstrate the feasibility of the proposed control strategy.
Key words:  deep space formation  collinear libration point  Lissajous orbit  linear matrix inequality  threshold control
DOI：10.11916/j.issn.1005-9113.2009.06.012
Clc Number:V448.2
Fund:

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