Nonlinear adaptive control for quadrotor flying vehicle

被引:85
|
作者
Islam, S. [1 ,2 ]
Liu, P. X. [3 ]
El Saddik, A. [1 ]
机构
[1] Univ Ottawa, SITE, Ottawa, ON K1N 6N5, Canada
[2] Harvard Univ, SEAS, Cambridge, MA 02138 USA
[3] Carleton Univ, Dept Syst & Comp Engn, Ottawa, ON K1S 5B6, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Robust and adaptive control; Quadrotor UAV; Lyapunov Method; TRACKING;
D O I
10.1007/s11071-014-1425-y
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this work, we deal with autonomous tracking and disturbance rejection problem of quadrotor vehicle flying in uncertain environment. The vehicles kinematic and modeling error uncertainties are associated with external disturbance, inertia, mass, and nonlinear aerodynamic forces and moments. The proposed method integrate the techniques from adaptive control and robust control theory. Robust and adaptive control algorithms for translational and orientation tracking are derived using Lyapunov method. It is shown in our analysis that the altitude, position, and attitude tracking errors are bounded and their bounds asymptotically converge to zero in Lyapunov sense. Simulation results on a commercial quadrotor flying vehicle are given to demonstrate the effectiveness of theoretical arguments for real world application.
引用
收藏
页码:117 / 133
页数:17
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