2023
DOI: 10.3847/1538-3881/acbafa
|View full text |Cite
|
Sign up to set email alerts
|

The Main Problem of Lunar Orbit Revisited

Abstract: A novel algorithm based on the Lindstedt–Poincaré method is proposed to construct an analytical solution of the lunar orbit. Based on the analytical solution, a numerical fitting algorithm is proposed to improve the coefficients of the analytical solution so that its accuracy can reach the level of a few kilometers within 20 yr. By fitting our solution to the long-term JPL ephemerides, we are able to recover the receding speed of the Moon from the Earth due to tidal effects. The proposed algorithm also provide… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2023
2023
2024
2024

Publication Types

Select...
1
1

Relationship

2
0

Authors

Journals

citations
Cited by 2 publications
(1 citation statement)
references
References 22 publications
(25 reference statements)
0
1
0
Order By: Relevance
“…In this paper, we analytically deal with planar sphere-ellipsoid model and carry out the solution of the quasi-periodic motion to high orders by the LP method. As far as the author knows, the LP method is valid for many celestial mechanics problems (Jorba and Masdemont, 1999;Li and Hou, 2023), but it is seldom applied to the spin-orbit coupling study in the complete sphere-ellipsoid model of the binary asteroid system. In contrast to previous studies, where numerical approaches are usually used, or the high-order Hamiltonian normal form is obtained by the canonical transformations (Gkolias et al, 2016), the advantage of the LP method is to directly obtain the explicit quasi-periodic solution.…”
Section: Introductionmentioning
confidence: 99%
“…In this paper, we analytically deal with planar sphere-ellipsoid model and carry out the solution of the quasi-periodic motion to high orders by the LP method. As far as the author knows, the LP method is valid for many celestial mechanics problems (Jorba and Masdemont, 1999;Li and Hou, 2023), but it is seldom applied to the spin-orbit coupling study in the complete sphere-ellipsoid model of the binary asteroid system. In contrast to previous studies, where numerical approaches are usually used, or the high-order Hamiltonian normal form is obtained by the canonical transformations (Gkolias et al, 2016), the advantage of the LP method is to directly obtain the explicit quasi-periodic solution.…”
Section: Introductionmentioning
confidence: 99%