The invention discloses an energy management method, device and system applied to a satellite, and the method comprises the steps: converting solar energy into electric energy through a solar wing at a first stage of the operation of the satellite; the kinetic energy device is controlled to rotate through electric energy, so that the electric energy is converted into kinetic energy to be stored; in the second stage of satellite operation, kinetic energy stored by the kinetic energy device is converted into electric energy; the kinetic energy device converts electric energy into mechanical energy to be stored in the first stage and converts the mechanical energy into electric energy to be released in the second stage, so that a storage battery in an existing energy system is replaced, and energy supply of a satellite in the second stage is met; and the limitation of the stored energy release frequency does not exist, and the overall service life of the satellite is not limited.
本发明公开了一种应用于卫星的能量管理方法、装置及系统,包括:在卫星运行的第一阶段,利用太阳翼将太阳能转换为电能;利用电能控制动能装置旋转,以将电能转化为动能进行存储;在所述卫星运行的第二阶段,将所述动能装置存储的动能转换为电能;通过动能装置在第一阶段将电能转换为机械能储存,并在第二阶段将机械能转换为电能释放,从而代替了现有的能量系统中的蓄电池,满足了卫星在第二阶段的能量供应;并且不存在储能释放次数的限制,不在制约卫星的整体使用寿命。
Energy management method, device and system applied to satellite
一种应用于卫星的能量管理方法、装置及系统
2023-04-25
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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