CV Lattes
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Ministério da Defesa (Brasil). Instituto Tecnológico de Aeronáutica (ITA). Divisão de Ciências Fundamentais (IEF) (Institutional affiliation from the last research proposal) Birthplace: Brazil
graduation at Engenharia Aeronáutica from Instituto Tecnológico de Aeronáutica (1983), master's at Aerospace Engineering from Instituto Tecnológico de Aeronáutica (1986) and doctorate at Aerospace Engineering from Instituto Tecnológico de Aeronáutica (1992). Has experience in Aerospace Engineering, focusing on Trajectories and Orbits, acting on the following subjects: dinâmica orbital, otimização de trajetórias espaciais, astronomia dinâmica, otimizacao de trajetorias espaciais and otimização de trajetórias. (Source: Lattes Curriculum)
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Artificial satellites are nowadays part of daily life as well instruments for advanced research in fields such as geodynamics, astrophysics of the solar system (atmosphere composition, magnetic field of planets), astrobiology ( water content and other materials essential to life as we know it), cosmology (Hubble and its new generation missions), communication satellites, weather and terri…
This research project aims to study optimal impulsive transfers in the dynamics of the restricted three or four-body problems with application to lunar and interplanetary missions, including the ones with swing-by maneuvers. The basic problem consists in transferring a space vehicle from a circular low earth orbit to an elliptical orbit around the moon or around a planet (Mars) by means o…
The research has two main goals: analytical and numerical study of optimization problem of transfers between orbits with small eccentricities performed by low thrust and power limited (electric propulsion) systems in strong central gravitational field (heliocentric phase of interplanetary trajectories). The analytical study of optimal low thrust and power limited trajectories will be deve…
The main purpose of this research project is the study of optimal impulsive transfers in the dynamics of restricted problem of three or four bodies with application to lunar and interplanetary missions. The basic problem of optimization consists in transferring a spacecraft from a low circular orbit around the Earth to a low circular orbit around the Moon or a planet (Mars, in particular)…
| 4 / 3 | Completed research grants |
| 11 / 3 | Completed scholarships in Brazil |
| 15 / 6 | All research grants and scholarships |
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