Study of the dynamics of artificial satellites around triple systems
MAPPING AND CONTROL OF SPACE DEBRIS: CONSEQUENCES TO THE ENVIRONMENT AND THE SPACE...
Detection and study of transient solar events and climate change
Full text | |
Author(s): |
Total Authors: 4
|
Affiliation: | [1] Instituto Nacional de Pesquisas Espaciais - Brasil
[2] Instituto Nacional de Pesquisas Espaciais - Brasil
[3] Instituto Nacional de Pesquisas Espaciais - Brasil
[4] Universidade Estadual Paulista - Brasil
Total Affiliations: 4
|
Document type: | Journal article |
Source: | REVISTA MEXICANA DE ASTRONOMIA Y ASTROFISICA; v. 53, n. 2 2019-10-21. |
Abstract | |
ABSTRACT Regarding practical applications of L3 of the Sun-Earth system, there are few studies with the goal of placing a spacecraft at this point, or in orbit around it. One of the main problems in placing a spacecraft near this equilibrium point is the fact that it is located behind the Sun with respect to the Earth. The Sun would be blocking direct communication between the spacecraft and the Earth. The present research gives several options to solve this problem by using a solar sail to place one or two spacecraft above and/or below the Ecliptic plane. This sail could also be used for the mission itself, to collect energy or particles. By using an adequate size, location and attitude of the solar sail, the equilibrium point can be moved from its original location to allow communications between the spacecraft and the Earth. A preliminary study of a solar sail that uses this strategy is shown here. (AU) | |
FAPESP's process: | 14/22295-5 - Study of the dynamics of artificial satellites around triple systems |
Grantee: | Diogo Merguizo Sanchez |
Support Opportunities: | Scholarships in Brazil - Post-Doctoral |
FAPESP's process: | 14/22293-2 - Mapping orbits around the lagrangian points in a triple asteroid |
Grantee: | Leonardo Barbosa Torres dos Santos |
Support Opportunities: | Scholarships in Brazil - Master |
FAPESP's process: | 11/08171-3 - Orbital dynamics of minor bodies |
Grantee: | Othon Cabo Winter |
Support Opportunities: | Research Projects - Thematic Grants |
FAPESP's process: | 16/14665-2 - Astrodynamics applied to space vehicles. |
Grantee: | Antônio Fernando Bertachini de Almeida Prado |
Support Opportunities: | Regular Research Grants |