DocumentCode :
2081306
Title :
Decentralized adaptive stabilization control for a quadrotor UAV
Author :
Mohammadi, M. ; Shahri, A.M.
Author_Institution :
Sch. of Electr. Eng., Iran Univ. of Sci. & Technol., Tehran, Iran
fYear :
2013
fDate :
13-15 Feb. 2013
Firstpage :
288
Lastpage :
292
Abstract :
In this paper attitude and altitude of a quadrotor Unmanned Aerial Vehicle is stabilized by Decentralized Adaptive control scheme. Parametric uncertainty beside unmodeled dynamics are two main factors that cause the control of this mechanical underactuated nonlinear Multi Input Multi Output (MIMO) become more challenging. Variable payloads in different missions and decreasing voltage of battery during flight time lead to low efficiency of simple controller with constant coefficients in various conditions. Decentralized adaptive controller, which is synthesized based on improved Lyapunov-based Model Reference Adaptive Control (MRAC) technique, is suggested to solve the problem. The controllers consist of proportional derivative terms plus auxiliary term with variable coefficient. Experimental results validate the efficiency and robustness of the suggested controller.
Keywords :
Lyapunov methods; MIMO systems; adaptive control; aerospace control; autonomous aerial vehicles; decentralised control; helicopters; mobile robots; telerobotics; uncertain systems; Lyapunov based model reference adaptive control; MIMO; MRAC; decentralized adaptive control scheme; decentralized adaptive stabilization control; mechanical underactuated nonlinear multi input multi output; parametric uncertainty; quadrotor UAV; quadrotor unmanned aerial vehicle; Propulsion; Robot sensing systems; Robustness; Vectors; Stabilization control; adaptive control; decentralized control; quadrotor UAV;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics and Mechatronics (ICRoM), 2013 First RSI/ISM International Conference on
Conference_Location :
Tehran
Print_ISBN :
978-1-4673-5809-5
Type :
conf
DOI :
10.1109/ICRoM.2013.6510121
Filename :
6510121
Link To Document :
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