Numerical models for the study of motion of lunar satellites
type: Item
instance of: scholarly article
title: Numerical models for the study of motion of lunar satellites
zbMATH Open document ID: 0568.70029
DOI: 10.1007/BF00054336
author: Maria Gousidou-Koutita
published in: Earth, Moon, and Planets
publication date: 1985-01-01T00:00:00Z
review text: The author deals with the numerical analysis of the planar (circular and elliptic) restricted three-body problem (RTBP) as well as of the perturbed RTBP by a fourth body (Sun). The power series method, and fifth-order Runge-Kutta method are used. Simple and multiple (up to multiplicity 165) quasiperiodic orbits of lunar satellites of negligible mass (with Earth and Moon as primaries) are calculated, and results are presented in graphical form in the inertial barycentric as well as in the rotating system.
Mathematics Subject Classification ID: 70M20
Mathematics Subject Classification ID: 70F07
Mathematics Subject Classification ID: 70-08
zbMATH DE Number: 3907848
zbMATH Keywords: planar (circular and elliptic) restricted three-body problem
zbMATH Keywords: power series method
zbMATH Keywords: Runge-Kutta method
zbMATH Keywords: quasiperiodic orbits
zbMATH Keywords: lunar satellites
reviewed by: Zakir F. Seidov
MaRDI profile type: Publication
cites work: Q5341709
cites work: The continuation of periodic orbits from the restricted to the general three-body problem
cites work: The existence of families of periodic orbits in theN-body problem
cites work: Dynamics of close binary systems
cites work: BURRAU'S PROBLEM OF THREE BODIES
description: scientific article; zbMATH DE number 3907848