The invention discloses a satellite solar wing circuit, a control method, a control device and a storage medium, the circuit comprises two solar wing sailboards provided with driving mechanisms and two control circuit boards, the first driving mechanism in the first solar wing sailboard is provided with two control interfaces, and the first control interface is connected with the two control circuit boards. A second driving mechanism in the second solar wing sailboard is also provided with two control interfaces; two control interfaces of the first driving mechanism are respectively in control connection with the first control circuit board and the second control circuit board; and two control interfaces of the second driving mechanism are respectively in control connection with the first control circuit board and the second control circuit board. Thus, it is ensured that the driving mechanisms are connected with the two control circuit boards, the use of the solar wing sailboard is not affected when the control interface of any driving mechanism is broken, and the reliability of the solar wing circuit is improved.
本发明公开了卫星太阳翼电路及控制方法、装置、存储介质,其中,该电路包括:两个配置有驱动机构的太阳翼帆板,以及,两个控制电路板,其中,第一太阳翼帆板中的第一驱动机构有两个控制接口,且第二太阳翼帆板中的第二驱动机构也有两个控制接口;第一驱动机构的两个控制接口分别与第一控制电路板、以及第二控制电路板控制连接;第二驱动机构的两个控制接口也分别与第一控制电路板、以及第二控制电路板控制连接。这样,保证驱动机构连接两个控制电路板,任意一个驱动机构的控制接口坏了,都不会影响太阳翼帆板的使用,提高了太阳翼电路的可靠性。
Satellite solar wing circuit, control method and device and storage medium
卫星太阳翼电路及控制方法、装置、存储介质
29.11.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Satellite solar wing fault processing method, related device and storage medium
Europäisches Patentamt | 2024
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