Abstract: The known intergrable in quadratures problem is examined about motion in the central field. The force function of the problem depends only on distance of material point to the chosen origin of the coordinates. In general case of arbitrary central force no rigorous analytical solution of the problem can be obtained due to the complexity of the integrals. In the present work for a case, when distance changes in finite limits, the semi-analytical method for construction of approximate solution, getting dependences of polar coordinates on time, is offered using elliptical functions and integrals. A model problem is as an example considered for perturbing motion of hypothetical equatorial satellites of the Jupiter and of the ...
This paper concerns the dynamics of a rigid body moving under the influence of a central gravitation...
The problem of controlling the movement of a mechanical system refers to the inverse problems of dyn...
In the dynamical model of relative motion with circular reference orbit, the equilibrium points are ...
The paper presents the exact solution to the relative orbital motion that takes place in a central f...
Abstract: The problem about a motion of material point (satellite) with negligible small m...
We present here some applications of the Forces's method in dynamic systems. In particular, we consi...
We present here some applications of the Forces ’ method in dynamic systems. In particular, we consi...
Numerous studies have been conducted on equilibrium orientations of objects moving under the influen...
Abstract: Double-averaged Hill’s problem taking into account the oblateness of the central...
A different approach is proposed for the study of satellite relative motion in an axially-symmetric ...
We develop a theory of orbits for the inverse-square central force law which differs considerably f...
In the first chapter of this thesis we analyse the problem of a dumbbell body moving in a homogeneou...
Orbital motion about irregular bodies is highly nonlinear due to inhomogeneities in the gravitationa...
Context. The modelling of stationary galactic stellar populations can be performed using distributio...
We will make the case that pedal coordinates (instead of polar or Cartesian coordinates) are more na...
This paper concerns the dynamics of a rigid body moving under the influence of a central gravitation...
The problem of controlling the movement of a mechanical system refers to the inverse problems of dyn...
In the dynamical model of relative motion with circular reference orbit, the equilibrium points are ...
The paper presents the exact solution to the relative orbital motion that takes place in a central f...
Abstract: The problem about a motion of material point (satellite) with negligible small m...
We present here some applications of the Forces's method in dynamic systems. In particular, we consi...
We present here some applications of the Forces ’ method in dynamic systems. In particular, we consi...
Numerous studies have been conducted on equilibrium orientations of objects moving under the influen...
Abstract: Double-averaged Hill’s problem taking into account the oblateness of the central...
A different approach is proposed for the study of satellite relative motion in an axially-symmetric ...
We develop a theory of orbits for the inverse-square central force law which differs considerably f...
In the first chapter of this thesis we analyse the problem of a dumbbell body moving in a homogeneou...
Orbital motion about irregular bodies is highly nonlinear due to inhomogeneities in the gravitationa...
Context. The modelling of stationary galactic stellar populations can be performed using distributio...
We will make the case that pedal coordinates (instead of polar or Cartesian coordinates) are more na...
This paper concerns the dynamics of a rigid body moving under the influence of a central gravitation...
The problem of controlling the movement of a mechanical system refers to the inverse problems of dyn...
In the dynamical model of relative motion with circular reference orbit, the equilibrium points are ...