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作 者:刘隆迪 杜兰[1] 张中凯[1] 刘泽军 周佩元 黄俊迦 LIU Longdi;DU Lan;ZHANG Zhongkai;LIU Zejun;ZHOU Peiyuan;HUANG Junjia(Institute of Geospatial Information,Information Engineering University,Zhengzhou 450001,China)
机构地区:[1]信息工程大学地理空间信息学院,郑州450001
出 处:《导航定位学报》2023年第3期29-37,共9页Journal of Navigation and Positioning
摘 要:针对目前空间目标编目库普遍采用的2行根数——简化常规摄动4/简化深空摄动4(TLE-SGP4/SDP4)模型复杂,源码不公开,且轨道精度不高的问题,提出一种地球同步轨道(GEO)带目标编目库的星历设计方法:基于数值积分的多天精密预报轨道,针对GEO的静地特性,设计19/25/31个参数的无奇点根数型星历模型;并采取定时长和多组星历同步更新策略,适用于数小时至数天的日常预报轨道发布及更新。实验结果表明,3种无奇点根数型星历模型可灵活适应合作/非合作GEO目标的预报轨道精度和预报时长,1 d拟合均方根(RMS)均值分别优于30、10和7 m;当缩短拟合时长至12 h,31参数星历模型的拟合精度可优于0.2 m。Aiming at the problem that the two-line element-simplified general perturbations-4/simplified deep-space perturbations-4(TLE-SGP4/SDP4)model commonly used in the current space target catalog is complex,with unavailable source codes in public and low orbit accuracy,the paper proposed the ephemeris design method of space cataloging library with targets on geosynchronous Earth orbit(GEO)ring:based on the multi-day precise forcast orbits of numerical integration,the 19/25/31 covariance element-ephemeris models without singularities were designed for the static characteristics of GEO;and the synchronized update strategy with fixed duration and multi-group ephemeris was adopted,suitable for daily forecast orbit release and update from hours to days.Experimental result showed that the three element-type ephemeris models could flexibly adapt to the forecast orbit accuracy and forecast duration of cooperative/non-cooperative GEO targets,and the mean values of 1 d fitted root mean square(RMS)would be better than 30,10 and 7 m,respectively;when the fitting duration is shortened to 12 h,the fitting accuracy of the 31-parameter ephemeris model could be better than 0.2 m.
关 键 词:地球同步轨道带 空间编目库 无奇点轨道根数 星历
分 类 号:P228[天文地球—大地测量学与测量工程]
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