Finite-time output-feedback position and attitude tracking of a rigid body

被引:60
作者
Gui, Haichao [1 ,2 ]
Vukovich, George [1 ]
机构
[1] York Univ, Dept Earth & Space Sci & Engn, Toronto, ON M3J 1P3, Canada
[2] Ryerson Univ, Dept Aerosp Engn, Toronto, ON M5B 2K3, Canada
关键词
Finite-time; Homogeneity; Output feedback; Passivity; Position and attitude tracking; Rigid body; SPACECRAFT FORMATION; STABILIZATION; STABILITY; SYSTEMS; INTEGRATOR; MOTION;
D O I
10.1016/j.automatica.2016.08.003
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The position and attitude tracking of a rigid body without velocity measurements is addressed. Dual quaternions are used to describe the coupled rotational and translational motions of the rigid body, yielding compact forms of the kinematics and dynamics suitable for control law synthesis. An output feedback pose (position and attitude) tracking controller is then designed by integrating techniques from passivity and homogeneity. More precisely, a passivity-enabling auxiliary system is proposed to provide necessary damping instead of velocity feedback and a homogeneous method is used to ensure finite time convergence. The proposed controller guarantees uniform almost global finite-time stability of the closed-loop system and produces a well-defined vector field on the attitude configuration manifold, thus avoiding the unwinding phenomenon. Moreover, it can be split to obtain velocity-free controllers with finite-time convergence for the cases of translation-only or rotation-only control. Numerical examples verify the effectiveness of the proposed method. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:270 / 278
页数:9
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