International audienceIn this paper we address the problem of output-feedback attitude control of a rigid body in quaternion-coordinate space through a hybrid (switching) PD+ based tracking controller; we establish stability for all initial values in a compact subset which may be arbitrarily enlarged by increasing the control gains. Assumptions used in the literature such as supposing that the initial states lay in a determined compact set or that the attitude error norm is smaller than π rad for all time, are removed by including a switching law. Simulation results are presented to corroborate our theoretical findings, showing that the system stabilises as expected, even when the initial estimated velocity error is large
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
International audienceIn this paper we address the problem of output-feedback attitude control of a ...
International audiencen this paper we address the problem of output feedback attitude control of a r...
International audienceWe address the problem of output feedback attitude control of a rigid body in ...
International audienceWe address the problem of state feedback atti- tude control of a rigid body in...
Abstract — We address the problem of state feedback atti-tude control of a rigid body in quaternion ...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
This paper provides a unified solution for the attitude and position tracking problem of a rigid bod...
International audienceThis paper considers the attitude control problem of a generic rotating 3 degr...
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...
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...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
International audienceIn this paper we address the problem of output-feedback attitude control of a ...
International audiencen this paper we address the problem of output feedback attitude control of a r...
International audienceWe address the problem of output feedback attitude control of a rigid body in ...
International audienceWe address the problem of state feedback atti- tude control of a rigid body in...
Abstract — We address the problem of state feedback atti-tude control of a rigid body in quaternion ...
Copyright © 2013 IEEEPresented at European Control Conference (ECC), July 17-19, 2013, Zurich, Switz...
This paper provides a unified solution for the attitude and position tracking problem of a rigid bod...
International audienceThis paper considers the attitude control problem of a generic rotating 3 degr...
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...
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...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...