This article presents a comparison of controllers which have been applied to a fixed-wing UAV (Unmanned Aerial Vehicle). The comparison is realized between the following nonlinear controllers techniques: sliding modes, nested saturations and back stepping. These controllers are compared and analyzed for altitude, yaw and roll by using simulation tests.
Nonlinear Controllers Applied to Fixed-Wing UAV
2012-11-01
440873 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Nonlinear observers applied to fixed-wing UAVs
IEEE | 2014
|Linear controllers implementation for a fixed-wing MAV
IEEE | 2014
|