Abstract
The report deals with methodic and engineering aspects of the mobile control principle application for a space station design. Methodic features result from particular model forms of controlled motion associated with the alternative connection of control channels. The methods of system stability analysis and mobile control algorithm synthesis are proposed. A number of applied problems of space station geometry control, the development of combined power control systems on the basis of highly power-intensive flywheels, emergency control and some others is considered. A comparative analysis of the traditional and mobile controls is performed applicably to particular objects.
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