A complex approach to spaceflight dynamics, theoretical mechanics and control theory study is described. Except standard lecture course the present approach also provides a practical part whose consideration the main attention is paid to. Description of the software for mathematical modeling, facilities for laboratory simulation of controllable system dynamics like a nanosatellite and practical work for students based on these facilities is given.

nanosatellite, attitude control system, mathematical simulation, laboratory testing

Theoretical and applied problems of mechanics