Third body perturbation using a single averaged model considering elliptic orbits for the disturbing body
Nenhuma Miniatura disponível
Data
2008-12-01
Autores
Domingos, Rita De C. [UNESP]
De Moraes, Rodolpho V. [UNESP]
De Almeida Prado, A. F.B.
Título da Revista
ISSN da Revista
Título de Volume
Editor
Resumo
In the present work, we expanded the study done by Solorzano1 including the eccentricity of the perturbing body. The assumptions used to develop the single-averaged analytical model are the same ones of the restricted elliptic three-body problem. The disturbing function was expanded in Legendre polynomials up to fourth-order. After that, the equations of motion are obtained from the planetary equations and we performed a set of numerical simulations. Different initial eccentricities for the perturbing and perturbed body are considered. The results obtained perform an analysis of the stability of a near-circular orbits and investigate under which conditions this orbit remain near-circular.
Descrição
Palavras-chave
Como citar
Advances in the Astronautical Sciences, v. 130 PART 2, p. 1571-1578.