CV Lattes
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Ministério da Defesa (Brasil). Instituto Tecnológico de Aeronáutica (ITA). Divisão de Engenharia Aeronáutica (IEA) (Institutional affiliation from the last research proposal) Birthplace: Brazil
Bachelor in Physics from the University of São Paulo and PhD in Physics from the University of São Paulo. She is currently an Associate Professor at the Aeronautics Institute of Technology and the Coordinator of the Undergraduate Course in Aerospace Engineering at ITA. She has experience in Aerospace Engineering, with an emphasis on Trajectories and Orbits, working mainly on the following topics: modern space mission designs, detection and calculation of hyperbolic dynamic structures in high-dimensional systems, transfer orbit design, practical stability regions in many-body dynamical systems, Hamiltonian systems and chaotic dynamics. She is a Permanent Professor on the Postgraduate Course in Aeronautical and Mechanical Engineering at ITA (PG-EAM) and collaborate on the Postgraduate Course in Physics at ITA (PG-FIS). (Source: Lattes Curriculum)
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With the current heightened global interest in lunar missions, new trajectories that facilitate or lower the cost of a space flight can have a huge impact. In this scenario, the circular restricted three-body problem (CRTBP) has been exploited, given that it models in a good first approximation the nonlinearity of the cislunar gravitational field and the trajectories and orbits populating…
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…
Realistic models and the development of efficient techniques for space trajectory design are essential with the increasing global interest and activities in space missions in the cislunar and lunar regions. As Brazil starts to collaborate and develop its own lunar missions, being the first South American country to sign the Artemis Accords, it is essential to have the expertise in realist…
This research project aims to develop analytical and numerical techniques based on the Parameterization Method to compute high-dimensional hyperbolic invariant sets in Hamiltonian systems with applications in Astrodynamics and Celestial Mechanics. These dynamical structures constitute an essential part of the skeleton of the dynamics in the phase space and are fundamental to compute trans…
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…
(Only some records are available in English at this moment)
| 5 / 3 | Completed research grants |
| 3 / 2 | Completed scholarships in Brazil |
| 4 / 4 | Completed scholarships abroad |
| 12 / 9 | All research grants and scholarships |
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