Attitude Control for Nanosatellites
Attitude Control, INPE, CubeSat, Nonlinear Control.
With the progress on the use of the CubeSat as an alternative to the traditional satellites project, it is necessary to investigate control strategies that allow the precision required for a specific space mission. In this way, this work will carry out a bibliographical review of control solutions applied to a traditional satellite project, aiming to identify the advantages and disadvantages of these control techniques in the CubeSat context. The result of this evaluation will be used to define the best attitude control that should be used in next generation of the INPE (National Institute For Space Research) nanosatellites.