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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.)

Lifetime maps for orbits around Callisto using a double-averaged model

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Author(s):
dos Santos, Josue Cardoso [1] ; Carvalho, Jean P. S. [2] ; Prado, Antonio F. B. A. [3] ; de Moraes, Rodolpho Vilhena [4]
Total Authors: 4
Affiliation:
[1] Sao Paulo State Univ UNESP, BR-12516410 Guaratingueta - Brazil
[2] UFRB, BR-44085132 Feira De Santana - Brazil
[3] Natl Inst Space Res INPE, BR-12201970 Sao Jose Dos Campos - Brazil
[4] Fed Univ Sao Paulo UNIFESP, BR-12231280 Sao Jose Dos Campos - Brazil
Total Affiliations: 4
Document type: Journal article
Source: ASTROPHYSICS AND SPACE SCIENCE; v. 362, n. 12 DEC 2017.
Web of Science Citations: 1
Abstract

The present paper studies the lifetime of orbits around a moon that is in orbit around its mother planet. In the context of the inner restricted three-body problem, the dynamical model considered in the present study uses the double-averaged dynamics of a spacecraft moving around a moon under the gravitational pulling of a disturbing third body in an elliptical orbit. The non-uniform distribution of the mass of the moon is also considered. Applications are performed using numerical experiments for the Callisto-spacecraft-Jupiter system, and lifetime maps for different values of the eccentricity of the disturbing body (Jupiter) are presented, in order to investigate the role of this parameter in these maps. The idea is to simulate a system with the same physical parameters as the Jupiter-Callisto system, but with larger eccentricities. These maps are also useful for validation and improvements in the results available in the literature, such as to find conditions to extend the available time for a massless orbiting body to be in highly inclined orbits under gravitational disturbances coming from the other bodies of the system. (AU)

FAPESP's process: 12/12539-9 - Stability of Frozen Orbits around Planetary Satellites using the Hamiltonian System in its Normalized Form
Grantee:Josué Cardoso dos Santos
Support Opportunities: Scholarships in Brazil - Master
FAPESP's process: 16/14665-2 - Astrodynamics applied to space vehicles.
Grantee:Antônio Fernando Bertachini de Almeida Prado
Support Opportunities: Regular Research Grants
FAPESP's process: 13/26652-4 - Analysis of orbits for scientific missions around natural celestial bodies
Grantee:Josué Cardoso dos Santos
Support Opportunities: Scholarships in Brazil - Doctorate
FAPESP's process: 16/24561-0 - On the relevance of small bodies in orbital dynamics
Grantee:Othon Cabo Winter
Support Opportunities: Research Projects - Thematic Grants
FAPESP's process: 11/08171-3 - Orbital dynamics of minor bodies
Grantee:Othon Cabo Winter
Support Opportunities: Research Projects - Thematic Grants
FAPESP's process: 12/21023-6 - Artificial satellite dynamics
Grantee:Rodolpho Vilhena de Moraes
Support Opportunities: Research Projects - Thematic Grants
FAPESP's process: 11/05671-5 - STABILITY ANALYSIS FOR PLANETARY SATELLITES ORBITS
Grantee:Jean Paulo dos Santos Carvalho
Support Opportunities: Scholarships in Brazil - Post-Doctoral