Add to ORKGThe equilibrium configurations of a deformable spinning satellite are investigated. The system is modelled by three interconnected rigid bodies, two of them having the characteristics of rigidified cables or beams. The equilibrium conditions and stability criteria of this particular system are provided by the multibody formalism. Using these conditions, all the equilibrium configurations which cannot a priori be found to be unstable are determined.Anglai
Abstract. Multibody systems in planar motion are modelled as two or more rigid components that are c...
The equation of motion of a multibody system, described here as a chain of rigid bars and revolute j...
to appear in J. Geom. Phys. This paper gives necessary and sufficient conditions for the (n-dimensio...
In this thesis, an analytical investigation of the dynamics of three-body tethered satellite systems...
The authors determine conditions for equilibrium of an orbiting system of interconnected rigid bodie...
Abstract: A rigid base body, supported by a fixed pivot point, is free to rotate in three dimensions...
In this paper we derive the reduced dynamical equations of motion for a planar three-spacecraft magn...
Positions of the elastic satellite equilibrium on a circular orbit are coonsidered in the paper aimi...
The development of multi-joint-spacecraft mission concepts calls for a deeper understanding of their...
Stability criteria for a spinning multi-body spacecraft were derived and applied to the THEMIS space...
A relatively general formulation for the governing equations of motion, applicable to a large class ...
The dynamics of a rigid body in a central gravitational eld can be modelled by a Hamiltonian system...
The thesis aims at studying the dynamics of single and multibody systems with a variety of spacecraf...
Abstract: Dynamics of attitude motion of a satellite moving along a circular orbit under i...
The Hamiltonian structure for a fundamental model of a tethered satellite system is constructed. The...
Abstract. Multibody systems in planar motion are modelled as two or more rigid components that are c...
The equation of motion of a multibody system, described here as a chain of rigid bars and revolute j...
to appear in J. Geom. Phys. This paper gives necessary and sufficient conditions for the (n-dimensio...
In this thesis, an analytical investigation of the dynamics of three-body tethered satellite systems...
The authors determine conditions for equilibrium of an orbiting system of interconnected rigid bodie...
Abstract: A rigid base body, supported by a fixed pivot point, is free to rotate in three dimensions...
In this paper we derive the reduced dynamical equations of motion for a planar three-spacecraft magn...
Positions of the elastic satellite equilibrium on a circular orbit are coonsidered in the paper aimi...
The development of multi-joint-spacecraft mission concepts calls for a deeper understanding of their...
Stability criteria for a spinning multi-body spacecraft were derived and applied to the THEMIS space...
A relatively general formulation for the governing equations of motion, applicable to a large class ...
The dynamics of a rigid body in a central gravitational eld can be modelled by a Hamiltonian system...
The thesis aims at studying the dynamics of single and multibody systems with a variety of spacecraf...
Abstract: Dynamics of attitude motion of a satellite moving along a circular orbit under i...
The Hamiltonian structure for a fundamental model of a tethered satellite system is constructed. The...
Abstract. Multibody systems in planar motion are modelled as two or more rigid components that are c...
The equation of motion of a multibody system, described here as a chain of rigid bars and revolute j...
to appear in J. Geom. Phys. This paper gives necessary and sufficient conditions for the (n-dimensio...