The paper adopts the energy shaping method to control of rotational motion. A global representation of the rigid body motion is given in the canonical form by a quaternion and its conjugate momenta. A general method for motion control on a cotangent bundle to the 3-sphere is suggested. The design algorithm is validated for three-axis spacecraft attitude control. Udgivelsesdato: AP
A configuration consisting of a star camera, four reaction wheels and magnetorquers for momentum unl...
A controller to rotate a rigid body between two successive orientations is designed. Particular feat...
We present several switching controllers for the attitude stabilization of a spacecraft. The control...
The paper adopts the energy shaping method to control of rotational motion. A global representation ...
This paper addresses three-axis attitude control for a Danish spacecraft, Roemer. The algorithm prop...
The motion control problem for a class of mechanical systems is addressed. The system configuration ...
A method is proposed for constructing a programmed trajectory in the problems of stabilizing a space...
The objective of this paper is to develop a control scheme for stabilization of a hamiltonian system...
In this thesis, the vibration suppression of flexible spacecraft that carries out attitude tracking ...
A parallel configuration using two 3-degree-of-freedom (3-DOF) spherical electromagnetic momentum ex...
Several laws are designed for simultaneous control of the orientation of an Earth-pointing spacecraf...
In this dissertation, we study dynamics and attitude control problems for a multibody system in spac...
Abstract: Problem of angular motion synthesis for interplanetary flight is considered. Con...
UnrestrictedThis dissertation develops in a unified manner a new and simple approach for the modelin...
International audienceThis paper considers the attitude control problem of a generic rotating 3 degr...
A configuration consisting of a star camera, four reaction wheels and magnetorquers for momentum unl...
A controller to rotate a rigid body between two successive orientations is designed. Particular feat...
We present several switching controllers for the attitude stabilization of a spacecraft. The control...
The paper adopts the energy shaping method to control of rotational motion. A global representation ...
This paper addresses three-axis attitude control for a Danish spacecraft, Roemer. The algorithm prop...
The motion control problem for a class of mechanical systems is addressed. The system configuration ...
A method is proposed for constructing a programmed trajectory in the problems of stabilizing a space...
The objective of this paper is to develop a control scheme for stabilization of a hamiltonian system...
In this thesis, the vibration suppression of flexible spacecraft that carries out attitude tracking ...
A parallel configuration using two 3-degree-of-freedom (3-DOF) spherical electromagnetic momentum ex...
Several laws are designed for simultaneous control of the orientation of an Earth-pointing spacecraf...
In this dissertation, we study dynamics and attitude control problems for a multibody system in spac...
Abstract: Problem of angular motion synthesis for interplanetary flight is considered. Con...
UnrestrictedThis dissertation develops in a unified manner a new and simple approach for the modelin...
International audienceThis paper considers the attitude control problem of a generic rotating 3 degr...
A configuration consisting of a star camera, four reaction wheels and magnetorquers for momentum unl...
A controller to rotate a rigid body between two successive orientations is designed. Particular feat...
We present several switching controllers for the attitude stabilization of a spacecraft. The control...
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