DocumentCode :
517537
Title :
Linear vs. nonlinear control techniques for a quadrotor vehicle
Author :
Al-Younes, Younes M. ; Al-Jarrah, Mohammed A. ; Jhemi, Ali A.
Author_Institution :
Dept. of Mech. Eng., American Univ. of Sharjah, Sharjah, United Arab Emirates
fYear :
2010
fDate :
20-22 April 2010
Firstpage :
1
Lastpage :
10
Abstract :
The aim of this paper is to propose a nonlinear control algorithm that is able to stabilize the attitude and altitude of a quadrotor vehicle, and then to compare it with the classical techniques, such as PID and LQR. The nonlinear algorithm is based on the backstepping methodology integrated with the integral and adaptation schemes. It´s called “Adaptive Integral Backstepping Controller” (AIBC). The recursive Lyapunov methodology in the backstepping technique will ensure the system stability, the integral action will increase the system robustness against disturbances and model uncertainties, and the adaptation law will estimate the modeling errors caused by assumptions in simplifying the complexity of the quadrotor model. Furthermore, a quadrotor vehicle is designed and modeled in this paper to perform the controlling task.
Keywords :
Lyapunov methods; adaptive control; aircraft control; attitude control; control system synthesis; helicopters; nonlinear control systems; position control; AIBC; LQR; PID; adaptive integral backstepping controller; altitude stability; attitude stability; helicopters; linear control techniques; nonlinear control techniques; quadrotor vehicle; recursive Lyapunov methodology; Attitude control; Backstepping; Mathematical model; Mechatronics; Navigation; Robust stability; Sliding mode control; Software testing; Three-term control; Unmanned aerial vehicles; Adaptation; Altitude; Attitude; Backstepping; Lyapunov;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and its Applications (ISMA), 2010 7th International Symposium on
Conference_Location :
Sharjah
Print_ISBN :
978-1-4244-6665-8
Type :
conf
Filename :
5478427
Link To Document :
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