摘要
导航卫星到寿后的处理关系到其在轨运行的安全性。介绍了现有导航星座废弃卫星的处理现状,分析了导航卫星在轨运行环境,综述了废弃卫星处理策略。对两种废弃卫星处理策略进行归纳总结,指出了偏心率长期稳定策略只能减缓空间碎片的增长;而偏心率增长最大再入大气层策略可以实现空间碎片的清除,同时,利用小推力或太阳光压的离轨方法为废弃卫星的清除提供了思路。
Disposal of navigation satellite at the end life is related to its safety in orbit.The disposal status of the navigation satellite were introduced,and the operating environment of the navigation satellite in orbit were analyzed,the disposal strategy of the disposed satellite were summarized.By comparing the two kinds of disposal strategies.It is pointed out that the long-term stabilization strategy of eccentricity can only slow down the growth of space debris.The strategy of eccentricity increased maximum to re-enter the atmosphere can remove space debris.Meanwhile,the method of deorbit with low thrust or solar radiation pressure can provide ideas for the removal of disposed satellites.
作者
徐家辉
胡敏
XU Jiahui;HU Min(Space Engineering University,Beijing 101416,China)
出处
《兵器装备工程学报》
CAS
北大核心
2018年第12期137-141,共5页
Journal of Ordnance Equipment Engineering
基金
总装试验技术研究重大项目(2013SY41A0010)
关键词
导航卫星
废弃轨道
长期演化
离轨处置策略
中地球轨道
navigation satellite
disposal orbit
long term evolution
de-orbit disposal strategy
medium earth orbit