This paper provides a unified solution for the attitude and position tracking problem of a rigid body in 3-dimensional space, using the concept of the unit dual quaternion. The error dynamics described by a unit dual quaternion are deduced after the dual-quaternion-based dynamics of a single rigid body are given. Then by utilizing the feedback linearization principle, a unit dual quaternion based tracker is proposed based on the error dynamics, which is proven to render the equilibrium point of the closed loop system asymptotically stable, and includes the attitude and position regulation problems as particular cases. Furthermore, to solve the two equilibria problem, a switching parameter is introduced to improve the tracker, which causes t...
Both stabilizing and tracking solutions of the rigid-body attitude control problem, using various at...
This paper addresses the simultaneous attitude and position tracking of a target spacecraft in the p...
International audiencen this paper we address the problem of output feedback attitude control of a r...
The main contribution of this paper is the design of a unit dual quaternion-based attitude and posit...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
The adoption of the dual quaternion formalism to represent the pose (position and orientation) of a ...
The adoption of the dual quaternion formalism to represent the pose (position and orientation) of a ...
Copyright © 2013 by the authors. Published by the American Institute of Aeronautics and Astronautics...
This paper focuses on finding a dual quaternion solution to attitude and position control for multip...
In this paper dual-quaternions are used to model a fully actuated rigid-body. A backstepping-control...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
Presented at American Control Conference, Washington, DC, June 17-19, 2013.In this paper, we suggest...
A hybrid feedback control scheme is proposed for stabilization of rigid body dynamics (pose and velo...
A hybrid feedback control scheme is proposed for stabilization of rigid body dynamics (pose and velo...
Both stabilizing and tracking solutions of the rigid-body attitude control problem, using various at...
This paper addresses the simultaneous attitude and position tracking of a target spacecraft in the p...
International audiencen this paper we address the problem of output feedback attitude control of a r...
The main contribution of this paper is the design of a unit dual quaternion-based attitude and posit...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
The adoption of the dual quaternion formalism to represent the pose (position and orientation) of a ...
The adoption of the dual quaternion formalism to represent the pose (position and orientation) of a ...
Copyright © 2013 by the authors. Published by the American Institute of Aeronautics and Astronautics...
This paper focuses on finding a dual quaternion solution to attitude and position control for multip...
In this paper dual-quaternions are used to model a fully actuated rigid-body. A backstepping-control...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
Presented at American Control Conference, Washington, DC, June 17-19, 2013.In this paper, we suggest...
A hybrid feedback control scheme is proposed for stabilization of rigid body dynamics (pose and velo...
A hybrid feedback control scheme is proposed for stabilization of rigid body dynamics (pose and velo...
Both stabilizing and tracking solutions of the rigid-body attitude control problem, using various at...
This paper addresses the simultaneous attitude and position tracking of a target spacecraft in the p...
International audiencen this paper we address the problem of output feedback attitude control of a r...