Design of near-optimal Earth escape orbits for solar sail spacecraft

被引：0
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作者：
Shi, Xiao-Ning [1 ]
Li, Li-Tao [1 ]
Cui, Nai-Gang [1 ]
机构：
[1] Dept. Astronautical Engineering, Harbin Institute of Technology, Harbin 150001, China
来源：
Journal of Harbin Institute of Technology (New Series) | 2013年 / 20卷 / 01期
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页码：12 / 16
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