INTELLECTUALIZATION SPACECRAFT POWER SYSTEM
Possibilities of intellectualization of the automation and stabilization unit of a small spacecraft based on a microcontroller are stated. An option for constructing an MBAS based on the PIC16F877A microcontroller is considered, with the implementation of energy extraction from unconventional sources and a partially illuminated SB based on extreme regulation and maintaining the power level of the generated solar battery not lower than a given level by the interval method. The results of modeling such a system are presented.