Title :
Simulation and robust trajectory-tracking for a Quadrotor UAV
Author :
Salazar, S. ; Gonzalez-Hernandez, Ivan ; Lopez, R. ; Lozano, Rogelio
Author_Institution :
UMI-LAFMIA, CINVESTAV-IPN, Mexico City, Mexico
Abstract :
In this article, a robust control algorithm using sliding modes is proposed for the efficient regulation on the trajectory tracking tasks, in the nonlinear, multivariable, quadrotor system model, that ensures the asymptotic convergence to a desired trajectory (reference signal - r(t)) in presence of all possible uncertainties and external disturbances. A smooth piecewise continuous function trajectory is proposed where the corresponding derivatives are bounded. Furthermore, we assume that the disturbances on the vehicle are bounded and the signal r(t) are available on line. The proposed algorithm employs a sliding surface based on the errors generated from the current state of the path in order to reach the desired reference r(t). The stability analysis of the closed-loop control system is proven via the use of Lyapunov theory. Finally, a numerical simulation of tracking a smooth trajectory is performed to demonstrate the validity and effectiveness of the proposed robust algorithm in presence of disturbances onto the vehicle.
Keywords :
Lyapunov methods; aircraft control; autonomous aerial vehicles; closed loop systems; convergence; helicopters; multivariable control systems; nonlinear control systems; numerical analysis; robust control; trajectory control; uncertain systems; variable structure systems; Lyapunov theory; asymptotic convergence; closed-loop control system; external disturbances; multivariable system model; nonlinear system model; numerical simulation; quadrotor UAV; quadrotor system model; robust algorithm; robust control algorithm; robust trajectory-tracking; signal; sliding modes; sliding surface; smooth piecewise continuous function trajectory; smooth trajectory tracking; stability analysis; trajectory tracking tasks; uncertainties; vehicle; Aircraft; Mathematical model; Robustness; Rotors; Trajectory; Vehicle dynamics; Vehicles;
Conference_Titel :
Unmanned Aircraft Systems (ICUAS), 2014 International Conference on
Conference_Location :
Orlando, FL
DOI :
10.1109/ICUAS.2014.6842371