THE MATHEMATICAL MODELING TECHNIQUE OF THE DYNAMIC RESPONSE OF THE STRUCTURE OF LANDING SPACECRAFT IN A GROUND METAL MINING
The paper presents a method of mathematical modeling of the dynamics of the finite element method of landing a spacecraft landing in a bench working out. Provides basic system of equations of the problem of non-stationary deformation structure. Using a software package that implements the solution of this system, get a picture of the behavior of a spacecraft landing on the planet's surface and in a bench working out. A comparison of the results of calculation and concluded that the behavior of the layout according to the spacecraft on the stand the real behavior of the structure.