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Relative equilibria of a satellite subjected to gravitational and aerodynamic torques

- V. A. Sarychev, S. Mirer
- Physics
- 2000

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 isolated… Expand

Equilibria of a satellite subjected to gravitational and aerodynamic torques with pressure center in a principal plane of inertia

- V. A. Sarychev, S. Mirer, A. Degtyarev
- Physics
- 14 March 2008

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 in… Expand

Dynamics of a satellite gravitational stabilization system with consideration of atmospheric resistance

- V. A. Sarychev
- Physics
- 1966

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 satellite… Expand

Device for mass measurement under zero-gravity conditions.

- V. A. Sarychev, V. Sazonov, A. S. Zlatorunsky, S. F. Khlopina, A. Egorov, V. I. Somov
- Physics, Medicine
- Acta astronautica
- 1 June 1980

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 estimates… Expand

Dynamics of an axisymmetric gyrostat satellite. Equilibrium positions and their stability

- S. Gutnik, V. A. Sarychev
- Physics
- 2014

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 the… Expand

Relative Equilibria of a Gyrostat Satellite with Internal Angular Momentum Along a Principal Axis

- V. A. Sarychev, S. Mirer
- Physics
- 1 December 2001

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 gyrostat… Expand

Dynamics of a satellite subject to gravitational and aerodynamic torques. Investigation of equilibrium positions

- V. A. Sarychev, S. Gutnik
- Physics
- 24 November 2015

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 equilibrium… Expand

Dual-spin satellites with gyro-damping

- V. A. Sarychev, S. Mirer, A. Isakov
- Physics
- 1 May 1982

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-spring… Expand

Dynamics of a gyrostat satellite with the vector of gyrostatic moment in the principal plane of inertia

- V. A. Sarychev, S. Mirer, A. Degtyarev
- Physics
- 1 February 2008

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 the… Expand

Dynamics of a gyrostat satellite subjected to the action of gravity moment. Equilibrium attitudes and their stability

- S. Gutnik, L. Santos, V. A. Sarychev, André Silva
- Physics
- 1 May 2015

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 equilibrium… Expand

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