FLIGHT CONTROL OF A VTOL AIR VEHICLE (QUADROTOR)

This study includes altitude stabilization, hovering control and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear...

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Bibliographic Details
Main Authors: İ. Can DİKMEN, Aydemir ARISOY, Hakan TEMELTAŞ
Format: Article
Language:English
Published: Hezarfen Aeronautics and Space Technologies Institue 2010-01-01
Series:Havacılık ve Uzay Teknolojileri Dergisi
Subjects:
PD
Online Access:http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/312/265