CV Lattes
ResearcherID
ORCID
Google Scholar Citations
Ministério da Defesa (Brasil). Instituto Tecnológico de Aeronáutica (ITA). Divisão de Engenharia Mecânica (IEM) (Institutional affiliation from the last research proposal) Birthplace: Brazil
João Trentin received his B.S. and Ph.D. degrees in Mechanical Engineering from São Paulo State University - UNESP, School of Engineering of Ilha Solteira, in 2016 and 2020, respectively. He has experience in dynamic modeling, linear and nonlinear control design, simulation, conducting experimental tests and developing embedded software. He was a postdoctoral researcher at Aeronautics Institute of Technology from 2021 to 2022 investigating the dynamic modeling and control of multirotors aerial vehicles. He is currently a product development engineer at Embraer S.A. (Source: Lattes Curriculum)
| News published in Agência FAPESP Newsletter about the researcher |
| More itemsLess items |
| TITULO |
| Articles published in other media outlets ( ): |
| More itemsLess items |
| VEICULO: TITULO (DATA) |
| VEICULO: TITULO (DATA) |
New ways of urban air transportation have attracted attention in the past few years. These solutions aim to reduce the traffic congestion that many people around the world have to undergo every day to get to their workplace, as well as to use clean energy. Therefore, large multirotor aerial vehicles have been studied to undertake this task in such areas. This proposal seeks to investigate…
Variable Speed Control Moment Gyroscope (VSCMG) is an innovative aerospace actuator used to control the attitude of satellites and spacecraft. This kind of mechanism gathers the favorable aspects of using a traditional Control Moment Gyroscope (CMG) but with the spin rate of the reaction wheel variable, being able to avoid singularities that occur when using CMGs. From the controlled chan…
The orientation control using reactios wheels as actuators is one of the most popular forms to stabilize and reject external disturbances in aerospace devices. From the controlled change of angular momentum rate using, for example, a reaction wheel it is possible to control the oscilation and direction rate in rigid bodies in space. Studies show that the reaction wheel pendulum can be con…
The attitude control using as actuators reaction wheels has been one of the most popular way to stabilize and reject external disturbances in aerospace devices. From the controlled change of angular momentum rate of change, using for example reaction wheels, it is possible to control the oscillation and direction rate of change in rigid bodies in space. The idea here is to use the angular…
| 3 / 3 | Completed scholarships in Brazil |
| 1 / 1 | Completed scholarships abroad |
| 4 / 4 | All Scholarships |
| Associated processes | |