Electricity supply system for a satellite

摘要

The system has load sections (1b) connected to output terminal (B) of batteries (2). Additional regulator (5) is connected to a control input of secondary battery discharge regulator modules (3b) for transmitting an adjustment signal of the current corresponding to excess of current produced by the sections, to the module. Main error amplifier (4) is connected to the regulator to activate operation of the regulator so that a load of a battery set is carried from the sections, while main sections (1a) transmit current to power-supply bus bar (11) supplying an equipment set (10).