http://arxiv.org/abs/2008.02802
The problem of the two-body gravitational interaction has been solved numerically based on the classical mechanics principles. One of the bodies is a deformable three-axis ellipsoid (central body) and the other is a material point (satellite). The relationship of the angular discrepancy between the calculated and actual positions of the satellite pericenter with central body’s gravity anomaly has been established.
D. Kiryan and G. Kiryan
Mon, 10 Aug 20
-804/53
Comments: 13 pages, 6 figures, 1 table