Global finite-time attitude tracking via quaternion feedback

被引:46
作者
Gui, Haichao [1 ]
Vukovich, George [2 ]
机构
[1] Ryerson Univ, Dept Aerosp Engn, Toronto, ON M5B 2K3, Canada
[2] York Univ, Dept Earth & Space Sci & Engn, N York, ON M3J 1P3, Canada
关键词
Attitude control; Finite-time stability; Homogeneity; Hybrid control; Output feedback; Saturation; RIGID SPACECRAFT; OUTPUT-FEEDBACK; STABILIZATION; STABILITY; SYSTEMS;
D O I
10.1016/j.sysconle.2016.09.017
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 attitude tracking of a rigid body using a quaternion description. Global finite time attitude controllers are designed with three types of measurements, namely, full states, attitude plus constant-biased angular velocity, and attitude only. In all three scenarios hybrid control techniques are utilized to overcome the well-known topological constraint on the attitude manifold, while coupled nonsmooth feedback inputs are designed via homogeneous theory to achieve finite-time stability. Specially, a finite-time bias observer is derived in the second scenario and a quaternion filter is constructed to provide damping in the absence of velocity feedback. The proposed methods ensure bounded control torques a priori and, in particular, include several existing attitude controllers as special cases. (C) 2016 Elsevier B.V. All rights reserved.
引用
收藏
页码:176 / 183
页数:8
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