Control of quadcopter motion in the horizontal plane

This paper deals with trajectory tracking control of a quadcopter in a horizontal plane. A full rigid body model of the flying vehicle that doesn’t assume smallness of the Euler angles is considered. For synthesis of the tracking control the nonlinear dynamics inversion approach is used. Three diffe...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Glazkov, T. V., Golubev, A. E., Gorbunov, A. V., Krishchenko, A. P.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Euler angles Nonlinear control Nonlinear dynamics Rigid structures Tracking control Trajectory control
Online-Zugang:	Volltext
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