Copyright © 2013 Tawfik El-Sayed Tawfik. This is an open access article distributed under the Creative Commons Attribution Li-cense, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. This paper considers the problem of controlling the rotational motion of an axi-symmetric rigid body using two inde-pendent control torques without angular velocity measurements. The control law which stabilizes asymptotically this motion is obtained only in terms of the orientation parameters. Global asymptotic stability is shown by applying LaSalle invariance principal. Numerical simulation is introduced
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The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
In this paper we shall use the passive properties of Euler dynamic equations as well as the struc...
In this paper we consider the problem of controlling the orientation of a satellite with thrusters w...
We prove that the angular velocity equations can be smoothly stabilized with a single torque control...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
International audienceThis paper deals with the attitude stabilization problem of a rigid body, wher...
Abstract: It is a well known fact that a symmetric spacecraft with two control torques supplied by g...
It is a well known fact that a symmetric spacecraft with two control torques supplied by gas jet act...
International audiencePractically, the attitude control of rigid bodies necessitates the estimation ...
This paper addresses the noncooperative attitude tracking control problem for rigid bodies whose dyn...
Abstract. This paper introduces a new class of globally asymptotically stabilizing feedback control ...
International audienceWe investigate the problem of stabilising the attitude of a 3-D axially symmet...
Abstract- There has been much interest over the past decade in the problem of asymptotic stabilizati...
The paper deals with the global stabilization of both the attitude and the angular velocities of an ...
The article deals with the problem of triaxial stabilization of an angular position of a rigid body....
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
In this paper we shall use the passive properties of Euler dynamic equations as well as the struc...
In this paper we consider the problem of controlling the orientation of a satellite with thrusters w...
We prove that the angular velocity equations can be smoothly stabilized with a single torque control...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...