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(Referência obtida automaticamente do Web of Science, por meio da informação sobre o financiamento pela FAPESP e o número do processo correspondente, incluída na publicação pelos autores.)

A survey of different classes of Earth-to-Moon trajectories in the patched three-body approach

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Autor(es):
de Sousa-Silva, Priscilla A. ; Terra, Maisa O.
Número total de Autores: 2
Tipo de documento: Artigo Científico
Fonte: ACTA ASTRONAUTICA; v. 123, p. 340-349, JUN-JUL 2016.
Citações Web of Science: 6
Resumo

This paper deals with Earth-to-Moon transfers in the patched three-body approach, in which the Sun Earth -Moon-Spacecraft four-body system is approximated by two coupled Circular Restricted Three Body Problems (CR3BP). This approach provides preliminary solutions that can be numerically refined into full four-body solutions. The standard transfers in this approach are low-energy manifold guided solutions with long transfer time which connect transit and non-transit orbits of each three-body system. Besides the standard transit-non-transit connections, there are alternative solutions involving a biparametric family of quasi-periodic orbits around the Earth. These solutions connect quasi-periodic orbits on two-dimensional tori of the Sun-Earth-Spacecraft system with L-1 or L-2 transit solutions of the Earth-Moon-Spacecraft system to provide transfers with lunar ballistic capture and short flight time. We review the dynamical elements employed to obtain the different classes of transfers and give examples of solutions obtained from sets of initial conditions around the Earth that are consistent with current infrastructure for space exploration. (C) 2016 IAA. Published by Elsevier Ltd. All rights reserved. (AU)

Processo FAPESP: 14/14448-6 - 65th International Astronautical Congress
Beneficiário:Maisa de Oliveira Terra
Linha de fomento: Auxílio à Pesquisa - Reunião - Exterior
Processo FAPESP: 13/07174-4 - Aplicações práticas das estruturas invariantes do problema restrito de três corpos espacial na dinâmica do sistema solar
Beneficiário:Priscilla Andressa de Sousa Silva
Linha de fomento: Bolsas no Brasil - Pós-Doutorado
Processo FAPESP: 12/21023-6 - Dinâmica de satélites artificiais
Beneficiário:Rodolpho Vilhena de Moraes
Linha de fomento: Auxílio à Pesquisa - Temático