Author:
Somov Ye.I., ,Butyrin S.A.,Somov S.Ye., , , ,
Abstract
The control problems on a space robot during its approach to an information geostationary satellite are considered. The robot motion control system uses an electric propulsion system with 8 engines at the pulse-width modulation of their thrust values and a gyroscopic moment cluster based on 4 gyrodines with digital control. Numerical results are presented that demonstrate the effectiveness of the developed discrete guidance and control algorithms.
Publisher
Samara Federal research center of the Russian Academy of Sciences
Cited by
1 articles.
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