Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/33179
Title: Stabilized controller design for attitude and altitude controlling of quad-rotor under disturbance and noisy conditions
Authors: Muhammad Hassan, Tanveer
Syed Faiz, Ahmed, Dr.
Hazry, Desa, Assoc. Prof. Dr.
Faizan A., Warsi
Muhammad Kamran, Joyo
syedfaiz@unimap.edu.my
hazry@unimap.edu.my
Keywords: Extended Kalman Filter
Lyapunov Stability Theorem
PID
Quad-rotor
Takeoff/Landing and Altitude Control
Issue Date: Jul-2013
Publisher: Science Publication
Citation: American Journal of Applied Sciences, vol. 10(8), 2013, pages 819-831
Abstract: This article presents a control approach to obtain the better stabilization in attitude and altitude of quad-rotor under different disturbance conditions. In the standard Quad-rotor rotor type UAV, controlling of attitude and altitude is one of the most critical tasks and appropriate controller for stabilization of UAV is essential and necessary. These two controls under various conditions of disturbances was a field of research stimulating for the researchers. The controller proposed is contingent on the PID feedback structure with Extended Kalman Filter (EKF). From Lyapunov Stability Theorem, it is proved that quad-rotor proposed altitude control system is asymptotic as well exponentially stability. Extended Kalman Filter (EKF) is used to filter out the sensors and system noises. Finally, the simulations carried out on MATLAB and the result proved the effectiveness of proposed recommended method for stabilization of attitude and altitude of quad-rotor.
Description: Link to publisher's homepage at http://www.scipub.org/
URI: http://thescipub.com/abstract/10.3844/ajassp.2013.819.831
http://dspace.unimap.edu.my:80/dspace/handle/123456789/33179
ISSN: 1546-9239
Appears in Collections:School of Mechatronic Engineering (Articles)
Hazry Desa, Associate Prof.Dr.



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