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针对未来空间任务的复杂性对卫星机动性能要求的提高,提出了利用激光输能技术作为卫星机动的能源解决方案;建立了激光传输距离、仰角约束的卫星输能应用模型,用于确定激光有效输能范围;描述了激光器输能时段的选择方法,用于确定最佳输能开始点和结束点;在此基础上,阐述了激光器的协同布站方案,并对该方案进行了仿真。最终仿真结果显示,基于该模型与布站方案,激光器能够完成对过境卫星的输能任务。
In view of the complexity of future space missions, the laser energy transfer technology is proposed as an energy solution to the satellite maneuver. The application of satellite transmission energy with laser transmission distance and elevation constraints is established to determine the laser effective The range of energy transmission is described. The selection method of laser energy transmission period is described, which is used to determine the starting point and end point of the optimal energy transmission. On the basis of this, the synergetic distribution scheme of the laser is illustrated and the scheme is simulated. The final simulation results show that based on the model and the station layout scheme, the laser can accomplish the task of transmitting energy to transit satellites.