Analysis of the possibility of creating a stable satellite about the asteroid Apophis as a homogeneous triaxial ellipsoid
2019 ◽
Vol 489
(1)
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pp. 27-33
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The task of creating a stable orbit of the Apophis asteroid satellite as a homogeneous triaxial ellipsoid is investigated. The simulation of the motion of the spacecraft around the asteroid was performed taking into account the main perturbations: from the attraction of celestial bodies, asteroids non-sphericity and solar radiation pressure, and taking into account the asteroids own rotation. It is shown that it is possible to create a stable orbit of an asteroid satellite. This orbit can be used for a detailed study of the characteristics of the asteroid and the refinement of its orbit using ground radio measurements of the motion of a satellite equipped with a radio beacon.
2020 ◽
2015 ◽
Vol 10
(S318)
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pp. 259-264
2020 ◽
Vol 19
(0)
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pp. 101-110
Keyword(s):
Keyword(s):
Keyword(s):
2017 ◽
Vol 60
(10)
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pp. 2146-2154
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