Analysis of spacecraft orbital motion around the asteroid Apophis

被引：0
|
作者：
V. V. Ivashkin
Anqi Lang
机构：
[1] Russian Academy of Sciences,Keldysh Institute of Applied Mathematics
[2] Bauman Moscow State Technical University,undefined
来源：
Doklady Physics | 2016年 / 61卷
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摘要：
Analysis has shown that it is possible to choose a main spacecraft orbit (~0.5 km radius) and a minisatellite orbit (~1.5 km radius), so that passive motion of the spacecraft around the asteroid remains stable within the context of a given model for a sufficiently long duration of time, i.e., approximately a month for the main spacecraft and several years for the minisatellite, until Apophis approaches the Earth in 2029.
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页码：288 / 292
页数：4
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