摘要
在航天器轨道预报的气动力计算中,加入不同高斯分布参数的热层模式密度相对误差,给出相应情况下的轨道预报误差。解答热层模式密度的均值标准差特性如何影响轨道预报的问题,为热层模式改进、建模指明方向。
In the aerodynamic calculation of spacecraft orbital prediction, the relative errors of the thermosphere model density with different Gauss distribution parameters are added to give the corresponding orbital prediction errors. The problem of how the mean standard deviation characteristics of the thermosphere model density affect the orbit prediction can be solved, and the direction for the improvement and modeling of the thermosphere model is pointed out.
作者
刘卫
刘四清
龚建村
王荣兰
LIU Wei;LIU Si-qing;GONG Jian-cun;WANG Rong-lan(National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China;Innovation Academy for Microsatellites of CAS, Shanghai 201210, China;University of Chinese Academy of Sciences, Beijing 100049, China)
出处
《空间碎片研究》
2019年第2期10-17,共8页
Space Debris Research
基金
北京市科技重大专项(Z181100002918004)
深圳科技计划项目(JCYJ20160817172025986)联合资助
关键词
误差均值
标准差
热层模式
轨道预报误差
mean error
stand ard deviation
thermosphere model
orbit prediction error