Title :
Quaternion-Based Robust Attitude Control for Uncertain Robotic Quadrotors
Author :
Hao Liu ; Xiafu Wang ; Yisheng Zhong
Author_Institution :
Sch. of Astronaut., Beihang Univ., Beijing, China
Abstract :
A robust nonlinear attitude control method is proposed for uncertain robotic quadrotors. The proposed controller is developed based on a nonlinear model with the quaternion representation and subject to parameter uncertainties, nonlinearities, and external disturbances. A new state feedback controller is proposed to restrain the effects of nonlinearities and uncertainties on the closed-loop control system. These uncertainties are considered as input equivalent disturbances and their effects are guaranteed to be attenuated. Experimental results are given to show good steady-state and dynamic tracking performance of the closed-loop system by the proposed robust control method compared with other nonlinear control methods.
Keywords :
aircraft control; attitude control; autonomous aerial vehicles; closed loop systems; control nonlinearities; helicopters; nonlinear control systems; robot dynamics; robust control; state feedback; uncertain systems; vehicle dynamics; closed-loop control system; dynamic tracking performance; external disturbances; input equivalent disturbances; nonlinear model; nonlinearities; parameter uncertainties; quaternion representation; quaternion-based robust attitude control; robust nonlinear attitude control method; state feedback controller; steady-state tracking performance; uncertain robotic quadrotors; Attitude control; Control systems; Quaternions; Robustness; Rotors; Uncertainty; Vehicles; Attitude control; Quadrotor; attitude control; quadrotor; quaternion; robust control; uncertainty;
Journal_Title :
Industrial Informatics, IEEE Transactions on
DOI :
10.1109/TII.2015.2397878