The invention discloses a spacecraft dynamic energy system based on a convex hull algorithm model and a use method. The system comprises a display control module, a calculation module and energy power supply equipment, the display control module is used for acquiring orbital elements, satellite structure information and satellite time and acquiring satellite attitude data from telemetry data; when the satellite carries out simulated flight simulation, volt-ampere curve data obtained through calculation are obtained from the calculation module, driving data and instructions are generated based on the volt-ampere curve data, and the driving data and the instructions are used for setting the state of the energy power supply equipment located on the ground; the calculation module is used for calculating the power generation efficiency of the solar wing cell panel in real time according to the sunlight incident angle and the star shielding area so as to obtain volt-ampere curve data; and the energy power supply equipment adjusts the state of the energy power supply equipment based on the acquired driving data and instruction, and the adjusted energy power supply equipment outputs real-time electric energy to a satellite.
本发明公开了一种基于凸包算法模型的航天器动态能源系统及使用方法,所述系统包括:显控模块、计算模块以及能源供电设备;所述显控模块用于获取轨道根数、卫星结构信息、星时、从遥测数据获取卫星姿态数据;所述卫星进行模拟飞行仿真时,从所述计算模块获取计算得到的伏安曲线数据,基于所述伏安曲线数据生成驱动数据及指令,所述驱动数据及指令用于设置位于地面的所述能源供电设备的状态;所述计算模块根据太阳光入射角和星体遮挡面积,实时计算太阳翼电池板的发电效率,进而得到伏安曲线数据;所述能源供电设备基于获取的所述驱动数据及指令,调整所述能源供电设备的状态,调整后的所述能源供电设备向卫星输出实时电能。
Spacecraft dynamic energy system based on convex hull algorithm model and use method
基于凸包算法模型的航天器动态能源系统及使用方法
2023-06-23
Patent
Electronic Resource
Chinese
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