We consider a special space tethered system consisting of a dumbbell-shaped rigid body and a particle. The particle coast along on the cable. The cable ends are placed in the dumbbell endpoints. We call such system ‘the system with leier constraint (the Dutch term ‘leier’ means the rope with both fixed ends). We assume that the system mass center moves along the circular orbit in the Newtonian Central Force Field. We study the dumbbell's relative motion caused by the particle of small mass in the orbital frame of reference. We deduce a sufficient condition for librations of the dumbbell about its stable equilibrium. We find a family of the dumbbell's asymptotic motions tending to librations about unstable equilibrium. The surface of such as...
International audienceWe study the integrability of a model of elastic satellite whose centre of mas...
The Hamiltonian structure for a fundamental model of a tethered satellite system is constructed. The...
This study is concerned with a planar tether containing payloads in which two lumped masses are fitt...
We consider the system that moves in the Newtonian central force field and consists of a rigid body ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77368/1/AIAA-10546-792.pd
A dumbbell-shaped rigid body can be used to represent certain large spacecraft or asteroids with bim...
A dumbbell-shaped rigid body can be used to represent certain large spacecraft or asteroids with bim...
This thesis considers two systems: a dumb-bell satellite which is a system of two point masses conne...
This research introduces a novel approach to the analysis of relative motion modelling of free and t...
The three dimensional equations of motion for a cable connected space station--counterweight system ...
This work extends the attitude dynamics and stability properties of the classical planar dumbbell pr...
The three dimensional equations of motion for a cable connected space station - counterweight system...
It is well known that the cable elongation or retraction in a tether system causes pitch oscillation...
This paper presents a dynamic analysis of a tethered satellite system with a moving mass. A dynamic ...
The dumbbell satellite is a simple structure consisting of two point masses connected by a massless ...
International audienceWe study the integrability of a model of elastic satellite whose centre of mas...
The Hamiltonian structure for a fundamental model of a tethered satellite system is constructed. The...
This study is concerned with a planar tether containing payloads in which two lumped masses are fitt...
We consider the system that moves in the Newtonian central force field and consists of a rigid body ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77368/1/AIAA-10546-792.pd
A dumbbell-shaped rigid body can be used to represent certain large spacecraft or asteroids with bim...
A dumbbell-shaped rigid body can be used to represent certain large spacecraft or asteroids with bim...
This thesis considers two systems: a dumb-bell satellite which is a system of two point masses conne...
This research introduces a novel approach to the analysis of relative motion modelling of free and t...
The three dimensional equations of motion for a cable connected space station--counterweight system ...
This work extends the attitude dynamics and stability properties of the classical planar dumbbell pr...
The three dimensional equations of motion for a cable connected space station - counterweight system...
It is well known that the cable elongation or retraction in a tether system causes pitch oscillation...
This paper presents a dynamic analysis of a tethered satellite system with a moving mass. A dynamic ...
The dumbbell satellite is a simple structure consisting of two point masses connected by a massless ...
International audienceWe study the integrability of a model of elastic satellite whose centre of mas...
The Hamiltonian structure for a fundamental model of a tethered satellite system is constructed. The...
This study is concerned with a planar tether containing payloads in which two lumped masses are fitt...