Spacecraft Dynamics and Control

Iintellectual control system for spacecraft rendezvous and docking based on active optical markers and its laboratory prototyping

Determination of orientation, coordinates, relative position and movement parameters of objects in space with the GNSS technology

Research of dynamic regularities of electrodynamic space tethered system as a possible highly efficient passive deorbit systems for space debris at the low earth orbits

Development of robust methods of precision attitude control of small spacecrafts and their implementation at the problem-oriented processors