Spacecraft formation control strategy on Sun-Earth Lissajous orbit
Lipeng, CuiPingYuan, 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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Spacecraft formation control strategy on Sun-Earth Lissajous orbit
本站小编 哈尔滨工业大学/2019-10-23
相关话题/Spacecraft formation control strategy Sun
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