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Information × Registration Number 0223U000229, 0122U002079 , R & D reports Title Development of mathematical models and algorithms for determining the design parameters of the distributed energy system of the space industrial platform popup.stage_title Head Lapkhanov Erik O., Доктор філософії Registration Date 05-01-2023 Organization Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine popup.description2  The object of research is the space energy modules of the distributed power supply system of the space industrial platform. The purpose of the work is to determine the dynamic characteristics and select the design parameters of the space energy modules of the distributed power system of the space industrial platform. Research methods: mathematical and computer modeling, system design, mechanics of space flight. An analysis of the current state of development of space power plants was carried out. A structural diagram of a distributed energy system has been developed. A mathematical model has been developed for the analysis of orbital, angular and relative motion of power spacecraft and receiver spacecraft. Algorithms for calculating the parameters of the orientation and stabilization system of powered space vehicles are proposed. A generalized model for determining the maximum distance and the length of the time interval for the transmission of electricity from the power spacecraft to the platform using microwave radiation has been developed. The developed model allows for the selection of design parameters of energy space vehicles at the stage of conceptual design of power systems of the space industrial platform. A generalized mathematical model for controlling the movement of power spacecraft (PS) and receiving spacecraft (RS) of the distributed energy system of the space industrial platform has been developed. The functional for optimizing the orbits of the PS and the RS in view of the maximization of the length of the energy transfer intervals from the PS to the RS was determined. The tests of the software modules for calculating the orbital translational, angular and relative motion of the PS and RS showed the performance of the developed mathematical model. Product Description popup.authors Lapkhanov Erik Oleksandrovych Palii Oleksandr Serhiiovych Svorobin Dmytro Serhiiovych popup.nrat_date 2023-01-05 Close