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大型低轨星座构型演化分析及维持控制策略研究

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针对大型低轨星座构型维持控制问题,搭建了一套星座构型演化及维持控制分析流程,适用于千颗量级的大型低轨Walker卫星星座构型演化分析及维持控制;采用去平均漂移偏差的相对构型保持方法分析星座构型演化情况,有效减小了控制频次、均衡了控制卫星分布;采用自由段维持策略有序规划各卫星位置维持控制时序和控制弧段,实现了整个星座在时间和空间维度有序、分散的控制,降低了对星座服务性能的影响.
Evolution Analysis and Maintenance Control Strategy Study on LEO Mega-Constellation Configuration
In view of the configuration maintenance control problem of low-Earth-orbit(LEO)mega-constellations,a process for the evolution analysis and maintenance control of constellation configuration is established.The process is suitable for the constellation configuration evolution analysis and maintenance control of LEO Walker satellites of 1 000 magnitude.The relative configuration preservation method without mean drift deviation is used to analyze the constellation configuration evolution,which not only effectively minimizes the control frequency,but also balances the control satellite distribution.Besides,a free segment maintenance strategy is adopted to orderly plan the control timing and position of each satellite,which realizes an orderly and decentralized control in time and space dimensions.The presented process and method reduce the negative impact on constellation service performance,and offer a significant advancement in the field of mega-constellation configuration maintenance control.

mega-constellationconfiguration evolutionconfiguration maintenance controllow-earth-orbit

储银、李文博、龚胜平、张峰

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清华大学 航天航空学院,北京 100084

北京航空航天大学 宇航学院,北京 100191

军事科学院战略评估咨询中心,北京 100091

大型星座 构型演化 构型维持控制 地球低轨卫星 智能轨迹优化

国家自然科学基金

12372044

2024

上海航天(中英文)
上海航天技术研究院

上海航天(中英文)

CSTPCD
影响因子:0.166
ISSN:2096-8655
年,卷(期):2024.41(1)
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