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
Conference paper
Electronic Resource
English
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