In this paper, we consider the motion of an asymmetric heavy gyrostat, when its center of mass lies along one of the principal axes of inertia. We determine the possible permanent rotations and, by means of the Energy-Casimir method, we give sufficient stability conditions. We prove that there exist permanent stable rotations when the gyrostat is oriented in any direction of the space, by the action of two spinning rotors, one of them aligned along the principal axis, where the center of mass lies. We also derive necessary stability conditions that, in some cases, are the same as the sufficient ones
A contribution is given to clarify gyroscopic effects on stability of parametrically excited rotor s...
The orientation of a spacecraft can be changed efficiently by transferring angular momentum between ...
Abstract: We consider an axially symmetric satellite with a large inner angular momentum (...
In this paper, we consider the motion of an asymmetric heavy gyrostat, when its center of mass lies ...
The stability of the permanent rotations of a heavy gyrostat is analyzed by means of the Energy-Casi...
A control scheme is proposed to guarantee an optimal stabilization of a given rotational motion of a...
A gyrostat is a massive sphere (or disk) mounted such that the supporting apparatus exerts no torque...
The stability behavior of unsymmetric damped gyroscopes varies basically from the well-known behavio...
The set of steady motions of the system named in the title is represented parametrically via the gyr...
This paper is devoted to the study of the problem of exponential asymptotic stability of the rotatio...
The main property of gyroscopic devices is maintaining the axis of a spinning rotor, a mathematical ...
The conditional stability of steady motions of a mechanical isolated system consisting of a rotating...
A one-wheeled robot-gyrostat are modeled by a heavy round disk with a balanced rotating flywheel. Di...
AbstractThe object of this paper is two-fold. On the one hand we want to develop the duality theory ...
Vibrational stability of large flexible structurally damped spacecraft carrying internal angular mom...
A contribution is given to clarify gyroscopic effects on stability of parametrically excited rotor s...
The orientation of a spacecraft can be changed efficiently by transferring angular momentum between ...
Abstract: We consider an axially symmetric satellite with a large inner angular momentum (...
In this paper, we consider the motion of an asymmetric heavy gyrostat, when its center of mass lies ...
The stability of the permanent rotations of a heavy gyrostat is analyzed by means of the Energy-Casi...
A control scheme is proposed to guarantee an optimal stabilization of a given rotational motion of a...
A gyrostat is a massive sphere (or disk) mounted such that the supporting apparatus exerts no torque...
The stability behavior of unsymmetric damped gyroscopes varies basically from the well-known behavio...
The set of steady motions of the system named in the title is represented parametrically via the gyr...
This paper is devoted to the study of the problem of exponential asymptotic stability of the rotatio...
The main property of gyroscopic devices is maintaining the axis of a spinning rotor, a mathematical ...
The conditional stability of steady motions of a mechanical isolated system consisting of a rotating...
A one-wheeled robot-gyrostat are modeled by a heavy round disk with a balanced rotating flywheel. Di...
AbstractThe object of this paper is two-fold. On the one hand we want to develop the duality theory ...
Vibrational stability of large flexible structurally damped spacecraft carrying internal angular mom...
A contribution is given to clarify gyroscopic effects on stability of parametrically excited rotor s...
The orientation of a spacecraft can be changed efficiently by transferring angular momentum between ...
Abstract: We consider an axially symmetric satellite with a large inner angular momentum (...