CV Lattes
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Ministério da Ciência, Tecnologia e Inovações (Brasil). Instituto Nacional de Pesquisas Espaciais (INPE) (Institutional affiliation from the last research proposal) Birthplace: Brazil
Graduated in Full Degree in Physics from the Federal Rural University of Pernambuco (2014), Master in Space Engineering and Technology (2017) by the National Institute for Space Research (INPE) and Doctorate in Space Engineering and Technology (2021) by the National Institute for Space Research (INPE). I have experience in General and Experimental Physics, Celestial Mechanics and Space Engineering, with an emphasis on Photonics, Nonlinear Optics and Orbital Dynamics. I work in the areas of Orbital Dynamics, Nonlinear Dynamics, Applied Physics, Space Exploration, Equilibrium Points, Theoretical and Computational Physics, Flight Dynamics with a specialty in trajectories and orbits. I was a visiting researcher at Politecnico de Milano (Italy) where I actively participated, between 09/2018-08/2019, in the space mission project called Lunar Meteoroid Impact Observer (LUMIO), financed by the ESA (European Space Agency). (Source: Lattes Curriculum)
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Currently, there is a growing interest in space missions of spacecrafts seeking to approach small bodies such as asteroids and comets (Kikuchi S.; Tsuda Y. and Kawaguchi, 2016). There are many important aspects in these missions, such as scientific research of these bodies, which keep characteristics of the formation of the solar system. Believing in the scientific and economic return of …
The objective of this work is to study models and methods for the calculation of spatial trajectories around the lagrangian points of a multiple asteroid system. It will be studied and compared different strategies involving this type of orbit. The main idea is to determine the exact positions of the equilibrium points of the equations of motion for an artificial satellite that travels ar…
The determination of space trajectories around an equilibrium points is a very challenging task, because, in addition to the natural instability of these points, in particular the collinear ones, there are still disturbances due to other celestial bodies and non-gravitational forces that affect the trajectory of a spacecraft from the nominal one. It is proposed, in this study, the search …
| 2 / 2 | Completed scholarships in Brazil |
| 1 / 1 | Completed scholarships abroad |
| 3 / 3 | All Scholarships |
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