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...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Turkish Air Force Academy
2010-01-01
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Series: | Havacılık ve Uzay Teknolojileri Dergisi |
Subjects: | |
Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/312/265 |