Robust attitude controller design for miniature quadrotors

被引:42
作者
Liu, Hao [1 ,2 ]
Li, Danjun [2 ]
Xi, Jianxiang [3 ]
Zhong, Yisheng [2 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Tsinghua Univ, TNlist, Dept Automat, Beijing 100084, Peoples R China
[3] High Tech Inst Xian, Xian 710025, Peoples R China
基金
中国国家自然科学基金;
关键词
quadrotors; robust control; attitude control; angular velocity measurements; TRAJECTORY TRACKING; STABILITY ANALYSIS; FLIGHT CONTROL; HELICOPTER; STABILIZATION;
D O I
10.1002/rnc.3332
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper addresses the robust attitude control problem of miniature quadrotors. A simplified linear dynamical model is obtained for each attitude angle, whereas nonlinear dynamics, interaxis coupling, parameter perturbations, and external disturbances are considered as uncertainties. For each channel, a linear time-invariant and decoupled robust controller are proposed based on a linear reduced-order observer and a robust compensator. The observer is applied to estimate the angular velocities, and the robust compensator is introduced for reducing the effects of uncertainties. It is proven that the estimation errors of angular velocities and angular tracking errors can converge to the given neighborhood of the origin in a finite time. Experimental results on the miniature quadrotor are presented to verify the effectiveness of the proposed control approach. Copyright (C) 2015 John Wiley & Sons, Ltd.
引用
收藏
页码:681 / 696
页数:16
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