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Relative equilibria of a satellite subjected to gravitational and aerodynamic torques
The problem of determining all equilibria of a satellite in a circular orbit is solved in the case where the satellite is subjected to gravitational and aerodynamic torques. The number of isolatedExpand
Equilibria of a satellite subjected to gravitational and aerodynamic torques with pressure center in a principal plane of inertia
Attitude motion of a satellite subjected to gravitational and aerodynamic torques in a circular orbit is considered. In special case, when the center of pressure of aerodynamic forces is located inExpand
Dynamics of a satellite gravitational stabilization system with consideration of atmospheric resistance
One of the important lines in the development of the technique of space flights is the creation of stabilized Earth satellites. The solution of this problem allows one to recover to Earth a satelliteExpand
Device for mass measurement under zero-gravity conditions.
The problem considered in this paper is the investigation of the properties of a mass-meter, i.e. the device for determining the mass of cosmonaut's body under zero-gravity conditions. The estimatesExpand
Dynamics of an axisymmetric gyrostat satellite. Equilibrium positions and their stability
Abstract The dynamics of an axisymmetric gyrostat satellite in a circular orbit in the central Newtonian force field is investigated. All the equilibrium positions of the gyrostat satellite in theExpand
Relative Equilibria of a Gyrostat Satellite with Internal Angular Momentum Along a Principal Axis
Abstract A new analytical solution to the problem of determining all equilibria of a gyrostat satellite in a circular orbit is given in the case where internal angular momentum of the gyrostatExpand
Dynamics of a satellite subject to gravitational and aerodynamic torques. Investigation of equilibrium positions
The rotational dynamics of a satellite moving over a circular orbit under an effect of gravitational and aerodynamic torques is investigated. A method is proposed for determining all equilibriumExpand
Dual-spin satellites with gyro-damping
Abstract In this paper the dual-spin satellite dynamics is investigated. To damp the nutation oscillations of the satellite a single-degree-of-freedom gyroscope is used with a viscous-springExpand
Dynamics of a gyrostat satellite with the vector of gyrostatic moment in the principal plane of inertia
Dynamics of a gyrostat satellite moving along a circular orbit in a central Newtonian field of force is investigated. In a particular case, when the gyrostatic moment vector lies in one of theExpand
Dynamics of a gyrostat satellite subjected to the action of gravity moment. Equilibrium attitudes and their stability
We study the dynamics of the rotational motion of a gyrostat satellite moving in the central Newtonian force field along a circular orbit. We propose a method for determining the equilibriumExpand
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