Tethered spacecraft in asteroid gravitational environment

被引：5
|
作者：
Burov, Alexander A. [1 ,2 ]
Guemian, Anna D. [3 ]
Kosenko, Ivan I. [1 ,4 ]
Nikonov, Vasily I. [1 ,3 ]
机构：
[1] Russian Acad Sci, Fed Res Ctr Comp Sci & Control, Moscow, Russia
[2] Natl Res Univ, Higher Sch Econ, Moscow, Russia
[3] Univ Beira Interior, Ctr Mech & Aerosp Sci & Technol, Covilha, Portugal
[4] Natl Res Univ, Moscow Aviat Inst, Moscow, Russia
来源：
ACTA ASTRONAUTICA | 2018年 / 143卷
关键词：
Tether system dynamics; Asteroid exploration; Rotating asteroid; Relative equilibria; RELATIVE EQUILIBRIA; LIBRATION POINTS; PENDULUM; DIVERSION; OSCILLATIONS; STABILITY; STATION; BALLAST; ORBIT;
D O I：
10.1016/j.actaastro.2017.11.018
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Relative equilibria of a pendulum attached to the surface of a uniformly rotating celestial body are considered. The locations of the tether anchor that correspond to a given spacecraft position are defined. The domains, where the spacecraft can be held with the help of such a pendulum, are also described. Stability of the found relative equilibria is studied.
引用
收藏
页码：126 / 132
页数：7
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