Abstract
The control system for the «Moon-Glob» spacecraft landing at the stage of precision braking is considered. The imp lementation of the landing process on the moon is supposed to be carried out on the basis of information from a promising measuring complex. The mathematical model of the landing control system in the precision braking area and the simulation results are presented. A mathematical model of a control system for landing a spacecraft on the lunar surface by using MatLab and Simulink software products is obtained. Keywords spacecraft, landing control system, precision braking, mathematical model of motion
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