Aircraft roll control system using LQR and fuzzy logic controller

In this paper, an aircraft roll control system based on design an autopilot that controls the roll angle of an aircraft is modeled using Matlab/Simulink. Firstly, modeling phase begins with a derivation of suitable mathematical model to describe the lateral directional motion of an aircraft. Then, t...

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Bibliographische Detailangaben

Hauptverfasser:	Usta, M. A., Akyazi, O., Akpinar, A. S.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerospace control Aircraft aircraft roll control Atmospheric modeling autopilot Control systems Equations FLC Fuzzy logic lateral directional dynamic LQR Mathematical model
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