LEO卫星轨道预报精度分析

利用动力学拟合法,以HY-2A卫星为例分析不同拟合区间对预报不同弧长的轨道精度的影响。基于CNES提供的事后精密星历和采用非差简化动力学方法获得的厘米级快速轨道两种产品,进行卫星轨道预报。结果表明：采用24 h和12 h拟合区间分别预报12 h轨道时,其3DRMS优于6 dm;当预报24 h轨道时,3DRMS优于1 m。...

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Published in:Ce hui xue bao 2016-09, Vol.45 (9), p.1035-1041
Main Author: 王亚菲 钟世明 王海涛 欧吉坤
Format: Article
Language:chi ; eng
Subjects:
Collocation积分
Low earth orbits
Satellite orbits
动力学拟合
快速定轨
拟合区间
预报
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creator 王亚菲 钟世明 王海涛 欧吉坤
description 利用动力学拟合法,以HY-2A卫星为例分析不同拟合区间对预报不同弧长的轨道精度的影响。基于CNES提供的事后精密星历和采用非差简化动力学方法获得的厘米级快速轨道两种产品,进行卫星轨道预报。结果表明：采用24 h和12 h拟合区间分别预报12 h轨道时,其3DRMS优于6 dm;当预报24 h轨道时,3DRMS优于1 m。
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subjects Collocation积分
Low earth orbits
Satellite orbits
动力学拟合
快速定轨
拟合区间
预报
title LEO卫星轨道预报精度分析
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