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(Reference retrieved automatically from Web of Science through information on FAPESP grant and its corresponding number as mentioned in the publication by the authors.)

Planetary Satellite Orbiters: Applications for the Moon

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Author(s):
dos Santos Carvalho, Jean Paulo [1] ; de Moraes, Rodolpho Vilhena [2] ; Bertachini de Almeida Prado, Antonio Fernando [3]
Total Authors: 3
Affiliation:
[1] Univ Estadual Paulista UNESP, BR-12516410 Guaratingueta, SP - Brazil
[2] Univ Fed Sao Paulo UNIFESP, Inst Ciencia & Tecnol, BR-12331280 Sao Jose Dos Campos, SP - Brazil
[3] INPE, Div Space Mech & Control, BR-12227010 Sao Jose Dos Campos, SP - Brazil
Total Affiliations: 3
Document type: Journal article
Source: MATHEMATICAL PROBLEMS IN ENGINEERING; 2011.
Web of Science Citations: 15
Abstract

Low-altitude, near-polar orbits are very desirable as science orbits for missions to planetary satellites, such as the Earth's Moon. In this paper, we present an analytical theory with numerical simulations to study the orbital motion of lunar low-altitude artificial satellite. We consider the problem of an artificial satellite perturbed by the nonuniform distribution of the mass of the Moon (J(2)-J(5), J(7), and C-22). The conditions to get frozen orbits are presented. Using an approach that considers the single-averaged problem, we found families of periodic orbits for the problem of an orbiter travelling around the Moon, where frozen orbits valid for long periods of time are found. A comparison between the models for the zonal and tesseral harmonics coefficients is presented. (AU)

FAPESP's process: 06/04997-6 - Close approach problems in orbital dynamics
Grantee:Rodolpho Vilhena de Moraes
Support type: Research Projects - Thematic Grants