The article of record as published may be found at http://dx.doi.org/10.2514/321346A controller to rotate a rigid body between two successive orientations is designed. Particular features are the fact that it is based on the quaternion approach, known to provide singularity-free attitude description, and it is adaptive in the sense that it does not need specific knowledge of the inertia matrix. Global stability of the overall controller is proved analytically and tested in computer simulations
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
This paper develops a quaternion attitude tracking control with an adaptive gains parameter that can...
The problem of stabilizing rigid-body attitude dynamics in the presence of pointwise time delay for ...
A controller to rotate a rigid body between two successive orientations is designed. Particular feat...
Copyright © 2013 by the authors. Published by the American Institute of Aeronautics and Astronautics...
The main contribution of this paper is the derivation of a model independent feedback control law th...
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...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
Presented at American Control Conference, Washington, DC, June 17-19, 2013.In this paper, we suggest...
The aim of this article is to present a novel quaternion based control scheme for the attitude contr...
International audienceWe study attitude control of rigid bodies on quaternion coordinates under thre...
International audienceThis paper considers the attitude control problem of a generic rotating 3 degr...
The operation and accomplishment of a satellite's mission depend on its capacity to control its atti...
The main contribution of this paper is the design of a unit dual quaternion-based attitude and posit...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
This paper develops a quaternion attitude tracking control with an adaptive gains parameter that can...
The problem of stabilizing rigid-body attitude dynamics in the presence of pointwise time delay for ...
A controller to rotate a rigid body between two successive orientations is designed. Particular feat...
Copyright © 2013 by the authors. Published by the American Institute of Aeronautics and Astronautics...
The main contribution of this paper is the derivation of a model independent feedback control law th...
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...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
Presented at American Control Conference, Washington, DC, June 17-19, 2013.In this paper, we suggest...
The aim of this article is to present a novel quaternion based control scheme for the attitude contr...
International audienceWe study attitude control of rigid bodies on quaternion coordinates under thre...
International audienceThis paper considers the attitude control problem of a generic rotating 3 degr...
The operation and accomplishment of a satellite's mission depend on its capacity to control its atti...
The main contribution of this paper is the design of a unit dual quaternion-based attitude and posit...
The unit quaternion is a pervasive representation of rigid-body attitude used for the design and ana...
This paper develops a quaternion attitude tracking control with an adaptive gains parameter that can...
The problem of stabilizing rigid-body attitude dynamics in the presence of pointwise time delay for ...