graduation at Física Bacharelado from Universidade Federal de Pernambuco (2006) and doctorate at Aerospace Engineering from Instituto Tecnológico de Aeronáutica (2011). Has experience in Physics, acting on the following subjects: transferência terra-lua, invariant manifolds, fronteiras de estabilidade fraca, variedades invariantes and dinâmica orbital. (Source: Lattes Curriculum)
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This project aims the investigation of trajectories for missions to asteroids in the context of many-body dynamics. Initially, the role of the invariant manifolds of the Restricted Three-Body Problem will be explored by means of both analytical and numerical approach, using Dynamical Systems tools, in order to determine preliminary profiles for missions to asteroids. Specifically, our goa…
This Scientific Initiation project deals with the study of transport mechanisms related to the hyperbolic invariant manifolds associated with the periodic orbits around the collinear equilibrium points of the Planar Circular Restricte Three-Body Problem (PCRTBP). Understanding the transport dynamics in this model is important to practical applications in Astrodynamics, particularly, in th…
Nonlinear dynamical systems model a variety of natural phenomena and engineering problems, ranging from mechanical rotors to interplanetary transfer trajectories. The elements that allow practical applications of such diverse systems are the invariant solutions of chaotic mathematical models. These special solutions organize the general behavior of the other solutions. Thus, the investiga…
Non-linear dynamical systems model several natural phenomena and engineering problems. The solutions of some of these systems have chaotic behavior, that is, they present sensitive dependence on initial conditions. One such system, which is widely studied, is the Restricted Three-Body Problem. This model displays chaotic dynamics and has applications in Astrodynamics, such as, for example…
This research project comprises the study of dynamical invariant structures of the Spatial Restricted Three-Body Problem (SR3BP) and their practical applications in Astronautics and Astrodynamics, particularly in the design of trajectories for space mission projects and in the dynamics of subsystems of the Solar System. The mathematical model is described by a autonomous non-integrable Ha…
It is possible to exploit multi-body gravitational dynamics to reduce the cost of space missions and allow new mission profiles other than the ones obtained by using the traditional patched conics methods. However, the design and optimisation of these multi-body trajectories is much more complex than that in the two-body approach, requiring a combination of dynamical systems theory and gl…
| 1 / 1 | Completed research grants |
| 1 / 1 | Ongoing scholarships in Brazil |
| 3 / 3 | Completed scholarships in Brazil |
| 1 / 1 | Completed scholarships abroad |
| 6 / 6 | All research grants and scholarships |
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CV Lattes
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