Spacecraft power supply system building method

The invention relates to a spacecraft power supply system building method. The method comprises steps: S1, the power supply performance of a power supply system in each cabin is acquired according todesign parameters of the spacecraft; and S2, the power supply system in the cabin with strong power s...

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Bibliographische Detailangaben
Hauptverfasser: LIANG KE, JIANG JI, DING RUI, REN XIAOQIANG, LIANG XIAOFENG, YU LEI, YI DEYING
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention relates to a spacecraft power supply system building method. The method comprises steps: S1, the power supply performance of a power supply system in each cabin is acquired according todesign parameters of the spacecraft; and S2, the power supply system in the cabin with strong power supply performance is connected with the power supply system in the cabin with weak power supply performance. Through connecting the power supply systems in different cabins, the power supply capability between the cabins is dispatched in a unified mode, and electric energy can be used between the cabins. When a power supply system in a single cabin fails, power can be supplied through other connected power supply systems, and the shortcoming of failure of the whole cabin when the power supply system in a single cabin fails can be effectively solved. The service life of a power supply system with weak power supply performance is effectively enhanced, and the reliability of the power supply system in the whole cabin