| Full text | |
| Author(s): |
Domingos, Rita de C.
;
de Moraes, Rodolpho V.
;
de Almeida Prado, A. F. B.
;
Seago, JH
;
Neta, B
;
Eller, TJ
;
Pelletier, FJ
Total Authors: 7
|
| Document type: | Journal article |
| Source: | ASTRODYNAMICS 2018, PTS I-IV; v. 130, p. 2-pg., 2008-01-01. |
| Abstract | |
In the present work, we expanded the study done by Solorzanol(1) 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. (AU) | |
| FAPESP's process: | 06/04997-6 - Close approach problems in orbital dynamics |
| Grantee: | Rodolpho Vilhena de Moraes |
| Support Opportunities: | Research Projects - Thematic Grants |