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Estimação da trajetória ótima de um lançador movido a foguete de propelente sólido
(Universidade Federal de Santa Maria, 2021-08-13)
In this work the optimal trajectory of orbital insertion of a Rocket-Powered Launcher is calculated, considering the discontinuities caused by the stage shifts, via the optimal control
theory. First the translational ...
Procedimento multidisciplinar de análise de tensões em componentes estruturais de asas de RPAs
(Universidade Federal de Santa Maria, 2021-02-08)
Remotely piloted aircraft, RPA, have a growing variety of applications over the past decades. During flight, such aircrafts are subjected to distributed aerodynamic loads that act on the aerodinamic center, respectively, ...
Estudo de um controlador LQT aplicado ao cubesat Sport
(Universidade Federal de Santa Maria, 2021-09-03)
The present work presents a study for the application of a Linear Quadratic Tracker (LQT), control law for the attitude control of the SPORT mission’s CubeSat. The objective is to computationally implement the control ...
Estimação da trajetória ótima de um lançador movido a foguete de propelente sólido
(Universidade Federal de Santa Maria, 2021-08-13)
In this work the optimal trajectory of orbital insertion of a Rocket-Powered Launcher is calculated,
considering the discontinuities caused by the stage shifts, via the optimal control
theory. First the translational ...
Otimização topológica de aerofólios utilizando algoritmo evolucionário bidirecional
(Universidade Federal de Santa Maria, 2021-02-10)
In this work it is presented the topological optimization of an airfoil considering compliance and
stress minimizations subjected to a volume constraint using bidirectional evolutionary structural
optimization (BESO) ...