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Achievable debris orbit prediction accuracy using laser ranging data from a single station

机译:使用来自单站的激光测距数据可获得的碎片轨道预测精度

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摘要

Earlier studies have shown that an orbit prediction accuracy of 20 arc sec ground station pointing error for 1-2 day predictions was achievable for low Earth orbit (LEO) debris using two passes of debris laser ranging (DLR) data from a single station, separated by about 24 h. The accuracy was determined by comparing the predicted orbits with subsequent tracking data from the same station. This accuracy statement might be over-optimistic for other parts of orbit far away from the station. This paper presents the achievable orbit prediction accuracy using satellite laser ranging (SLR) data of Starlette and Larets under a similar data scenario as that of DLR. The SLR data is corrupted with random errors of 1 m standard deviation so that its accuracy is similar to that of DLR data. The accurate ILRS Consolidated Prediction Format orbits are used as reference to compute the orbit prediction errors. The study demonstrates that accuracy of 20 arc sec for 1-2 day predictions is achievable.
机译:较早的研究表明,对低地球轨道(LEO)碎片使用来自单个站的两次传递的碎片激光测距(DLR)数据,可以实现1-2天预测的20弧秒秒地面站指向误差的轨道预测精度大约24小时。通过将预测轨道与来自同一站点的后续跟踪数据进行比较来确定精度。对于远离站的轨道的其他部分,此准确性声明可能过于乐观。本文介绍了在与DLR相似的数据情况下,使用Starlette和Larets的卫星激光测距(SLR)数据可实现的轨道预测精度。 SLR数据因1 m标准偏差的随机误差而损坏,因此其准确性类似于DLR数据。准确的ILRS合并预测格式轨道用作计算轨道预测误差的参考。研究表明,对于1-2天的预测,可以达到20 arc sec的精度。

著录项

  • 来源
    《Advances in space research》 |2014年第1期|119-124|共6页
  • 作者

    Jizhang Sang; James C. Bennett;

  • 作者单位

    School of Geodesy and Geomatics, Wuhan University, 129 Luoyu Road, Wuhan, China;

    The SPACE Research Centre, School of Mathematical and Geospatial Sciences, RMIT University, GPO Box 2476, Melbourne, Victoria 3001, Australia ,EOS Space Systems Pty. Ltd., Mount Stromlo Observatory, Cotter Road, Weston Creek, Australian Capital Territory 2611, Australia;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Satellite laser ranging; Debris laser ranging; Orbit prediction performance;

    机译:卫星激光测距;碎片激光测距;轨道预测性能;

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