Abstract:
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.
Keywords:nanosatellite, attitude control system, mathematical simulation, laboratory testing.
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