Presented at American Control Conference, Washington, DC, June 17-19, 2013.In this paper, we suggest a new representation for the combined translational and rotational dynamic equations of motion of a rigid body in terms of dual quaternions. We show that with this representation it is relatively straightforward to extend existing attitude controllers based on quaternions to combined position and attitude controllers based on dual quaternions. We show this by developing setpoint nonlinear controllers for the position and attitude of a rigid body with and without linear and angular velocity feedback based on existing attitude-only controllers with and without angular velocity feedback. The combined position and attitude velocity-free controll...
A hybrid feedback control scheme is proposed for stabilization of rigid body dynamics (pose and velo...
The problem of stabilizing rigid-body attitude dynamics in the presence of pointwise time delay for ...
International audienceIn this paper we address the problem of output-feedback attitude control of a ...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
Copyright © 2013 by the authors. Published by the American Institute of Aeronautics and Astronautics...
This paper provides a unified solution for the attitude and position tracking problem of a rigid bod...
The main contribution of this paper is the design of a unit dual quaternion-based attitude and posit...
The adoption of the dual quaternion formalism to represent the pose (position and orientation) of a ...
This paper presents results on kinematic controllers for the stabilization of rigid body displacemen...
Rigid body motion tracking without linear and angular velocity feedback using dual quaternion
This paper focuses on finding a dual quaternion solution to attitude and position control for multip...
This paper presents a review of recent results in the field of dual quaternion based motion control....
The article of record as published may be found at http://dx.doi.org/10.2514/321346A controller to r...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
The aim of this article is to present a novel quaternion based control scheme for the attitude contr...
A hybrid feedback control scheme is proposed for stabilization of rigid body dynamics (pose and velo...
The problem of stabilizing rigid-body attitude dynamics in the presence of pointwise time delay for ...
International audienceIn this paper we address the problem of output-feedback attitude control of a ...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
Copyright © 2013 by the authors. Published by the American Institute of Aeronautics and Astronautics...
This paper provides a unified solution for the attitude and position tracking problem of a rigid bod...
The main contribution of this paper is the design of a unit dual quaternion-based attitude and posit...
The adoption of the dual quaternion formalism to represent the pose (position and orientation) of a ...
This paper presents results on kinematic controllers for the stabilization of rigid body displacemen...
Rigid body motion tracking without linear and angular velocity feedback using dual quaternion
This paper focuses on finding a dual quaternion solution to attitude and position control for multip...
This paper presents a review of recent results in the field of dual quaternion based motion control....
The article of record as published may be found at http://dx.doi.org/10.2514/321346A controller to r...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
The aim of this article is to present a novel quaternion based control scheme for the attitude contr...
A hybrid feedback control scheme is proposed for stabilization of rigid body dynamics (pose and velo...
The problem of stabilizing rigid-body attitude dynamics in the presence of pointwise time delay for ...
International audienceIn this paper we address the problem of output-feedback attitude control of a ...