R. V. Kozlov, V. Bukreev, M. V. Nesterishin, A. Lelekov
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Simulation Model of Spacecraft Power System for Power Balance Calculation
The article discusses the methodology for constructing a simulation model of a spacecraft electrical power system (EPS). The relevance of research is substantiated, the tasks are set to develop and confirm the adequacy of the simulation model of the EPS and its components. Areas of the possible application of the proposed EPS model are presented and the directions for further research are determined.
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