The authors determine conditions for equilibrium of an orbiting system of interconnected rigid bodies and find the stability conditions for a given equilibrium configuration. The equations were expressed in a body mean frame and derived from the Roberson-Wittenburg formalism, the combination of the advantages of these methods leading to a rather simple stability analysis by use of the Liapunov technique.Anglai
This thesis presents the quasi-rigid body formulation, a framework for viewing a satellite formation...
A literal Liapunov stability analysis of a spacecraft with flexible appendages often requires a divi...
The dynamics of a rigid body in a central gravitational eld can be modelled by a Hamiltonian system...
The equilibrium configurations of a deformable spinning satellite are investigated. The system is mo...
Subject of inquiry: system of connected rigid bodies, elastic rods, body-space-liquid system. The ai...
Abstract. Multibody systems in planar motion are modelled as two or more rigid components that are c...
In this paper an approach is described for determining equilibrium states of a rigid body suspended ...
In this thesis, an analytical investigation of the dynamics of three-body tethered satellite systems...
The paper is concerned with connection of two gyros and one body hung by a string. The necessary sta...
Positions of the elastic satellite equilibrium on a circular orbit are coonsidered in the paper aimi...
A dumbbell-shaped rigid body can be used to represent certain large spacecraft or asteroids with bim...
: The stability of relative equilibrium solutions for the interaction of two massive bodies is explo...
In this note, we investigate the stability behaviour of torque controlled rotating rigid bodies. The...
It is easy to see whether a system in equilibrium is stable when there are only two forces acting on...
The paper presents the parametric stability analysis of a set of equilibrium con1gurations with resp...
This thesis presents the quasi-rigid body formulation, a framework for viewing a satellite formation...
A literal Liapunov stability analysis of a spacecraft with flexible appendages often requires a divi...
The dynamics of a rigid body in a central gravitational eld can be modelled by a Hamiltonian system...
The equilibrium configurations of a deformable spinning satellite are investigated. The system is mo...
Subject of inquiry: system of connected rigid bodies, elastic rods, body-space-liquid system. The ai...
Abstract. Multibody systems in planar motion are modelled as two or more rigid components that are c...
In this paper an approach is described for determining equilibrium states of a rigid body suspended ...
In this thesis, an analytical investigation of the dynamics of three-body tethered satellite systems...
The paper is concerned with connection of two gyros and one body hung by a string. The necessary sta...
Positions of the elastic satellite equilibrium on a circular orbit are coonsidered in the paper aimi...
A dumbbell-shaped rigid body can be used to represent certain large spacecraft or asteroids with bim...
: The stability of relative equilibrium solutions for the interaction of two massive bodies is explo...
In this note, we investigate the stability behaviour of torque controlled rotating rigid bodies. The...
It is easy to see whether a system in equilibrium is stable when there are only two forces acting on...
The paper presents the parametric stability analysis of a set of equilibrium con1gurations with resp...
This thesis presents the quasi-rigid body formulation, a framework for viewing a satellite formation...
A literal Liapunov stability analysis of a spacecraft with flexible appendages often requires a divi...
The dynamics of a rigid body in a central gravitational eld can be modelled by a Hamiltonian system...
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