FIELD: electricity.
SUBSTANCE: invention is related to electrotechnical industry and may be used in design of autonomous power supply systems (PSS) of artificial Earth satellites (AES). The invention suggests the load supply method by direct current in autonomous power supply system for AES from solar battery and a set of secondary power supply sources being accumulators Nac of in-series accumulator batteries; the method lies in stabilisation of on-load voltage, charge and discharge of accumulator batteries through individual charge and discharge converters, at that discharge converters are made without booster units and to this end number of accumulators Nac in each accumulator battery is selected on the basis of the following ratio: Nac≥(Uout+1)/Uac.min, where Nac is a number of accumulators in in-series circuit of each accumulator battery; Uout is voltage at output of autonomous power supply system, V; Uac.min is minimum discharge voltage of one accumulator, V; charge converters are made without booster units and to this end number Q-point voltage of the solar battery is selected on the basis of the following ratio: UQ-p>Uac.max·Nac+1, where UQ-p Q-point voltage of the solar battery at the end of its safe operation resource, V; Uac.max is maximum charge voltage of one accumulator, V, at that design number of accumulators Nac is increased additionally on the basis of the following ratio: Nac≥(Uout+1)/Uac.min+Nfail, where Nfail is a number of permitted fails of accumulators; on-voltage stabilisation and charge of accumulator batteries is made using optimising voltage control of the solar battery.
EFFECT: improvement of specific output performance and reliability of autonomous power supply system for AES.
2 dwg
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Authors
Dates
2015-05-10—Published
2013-10-02—Filed