| Full text | |
| Author(s): |
Gomes, Vivian Martins
;
Bertachini de Almeida Prado, Antonio Fernando
;
Golebiewska, Justyna
Total Authors: 3
|
| Document type: | Journal article |
| Source: | SCIENTIFIC WORLD JOURNAL; v. N/A, p. 6-pg., 2013-01-01. |
| Abstract | |
The present research studies the motion of a particle or a spacecraft that comes from an orbit around the Sun, which can be elliptic or hyperbolic, and that makes a passage close enough to the Earth such that it crosses its atmosphere. The idea is to measure the Sun-particle two-body energy before and after this passage in order to verify its variation as a function of the periapsis distance, angle of approach, and velocity at the periapsis of the particle. The full system is formed by the Sun, the Earth, and the particle or the spacecraft. The Sun and the Earth are in circular orbits around their center of mass and the motion is planar for all the bodies involved. The equations of motion consider the restricted circular planar three-body problem with the addition of the atmospheric drag. The initial conditions of the particle or spacecraft (position and velocity) are given at the periapsis of its trajectory around the Earth. (AU) | |
| FAPESP's process: | 11/13101-4 - Study of orbital maneuvers to escape from collisions for a spacecraft and a group of particles |
| Grantee: | Vivian Martins Gomes |
| Support Opportunities: | Research Grants - Young Investigators Grants |
| FAPESP's process: | 11/09310-7 - Orbital study of the motion of spacecrafts |
| Grantee: | Antônio Fernando Bertachini de Almeida Prado |
| Support Opportunities: | Regular Research Grants |
| FAPESP's process: | 11/08171-3 - Orbital dynamics of minor bodies |
| Grantee: | Othon Cabo Winter |
| Support Opportunities: | Research Projects - Thematic Grants |