Publicação:
Planetary Satellite Orbiters: Applications for the Moon

Carregando...
Imagem de Miniatura

Data

2011-01-01

Orientador

Coorientador

Pós-graduação

Curso de graduação

Título da Revista

ISSN da Revista

Título de Volume

Editor

Hindawi Publishing Corporation

Tipo

Artigo

Direito de acesso

Acesso abertoAcesso Aberto

Resumo

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.

Descrição

Palavras-chave

Idioma

Inglês

Como citar

Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 19, 2011.

Itens relacionados

Unidades

Departamentos

Cursos de graduação

Programas de pós-graduação