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The authors have proposed the embodiments of the spacecraft power system with high frequency link, which allows adjusting solar battery voltage in a range sufficient to implement the maximum power point tracking (MPPT) mode and provides the coordination of voltage level of the solar battery, accumulator battery and load. The calculating technique of the weight dimension characteristics of spacecraft...
The authors have proposed the structure of the highvoltage power supply system of low-orbit spacecraft based on regulated current inverter, which allows adjusting solar battery voltage in a range sufficient to implement the maximum power point tracking mode. The characteristics at drift of current-voltage curve of solar battery and different values of the load were obtained. The power supply system...
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