首页|广播星历旋转误差对低轨星载BDS-3/GPS实时精密定轨影响分析

广播星历旋转误差对低轨星载BDS-3/GPS实时精密定轨影响分析

Effects of broadcast ephemeris rotation error on real-time orbit determination for a low Earth orbit satellite using onboard BDS-3/GPS observations

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基于LT-01A卫星星载BDS-3/GPS观测值进行了星载实时精密定轨研究,并重点分析了广播星历旋转误差对实时定轨精度的影响.通过赫尔默特转换评估了所选时段内GPS和BDS-3广播星历轨道旋转误差,显示BDS-3广播星历旋转误差可达-8.7 mas,平均量级较GPS大约2.5倍.BDS-3广播星历经旋转改正后,轨道切向、法向均方根(RMS)误差从25 cm左右提升至10 cm量级,提升幅度超过50%.因此,基于星载BDS-3以及BDS-3/GPS联合的实时定轨精度受BDS-3星历旋转误差影响严重,且主要作用于切向和法向.经过旋转改正后,单独BDS-3实时定轨在切向、法向、径向RMS分别为21.0 cm、10.7 cm及11.2 cm,其切向和法向精度比改正前分别提升15.0%和31.8%;BDS-3与GPS联合定轨进一步提升切向精度至19.4 cm.得益于BDS-3广播星历较高的精度,单BDS-3以及BDS-3/GPS联合的实时定轨在旋转改正前的三维RMS分别为31.9 cm和29.2 cm,较单GPS实时定轨分别提升9.1%和16.8%;添加旋转改正后,其定轨精度分别提升至26.7 cm和25.0 cm,较单GPS实时定轨分别提升22.6%和27.5%.
The real-time orbit determination(RTOD)performance with onboard BDS-3 and GPS observations from a Chinese low Earth orbit satellite,LT-01A,is analyzed,with a focus on the impact of broadcast ephemeris rotation error on RTOD accuracy.The orbit rotation errors of GPS and BDS-3 broadcast ephemeris are evaluated by Helmert transformation with respect to post pre-cise orbit product.BDS-3 broadcast ephemeris reveals rotation errors reaching up to-8.7 mas,and indicates an average rotation error about 2.5 times larger than that of GPS.After the rotation correction of BDS-3 broadcast ephemeris,the root mean square(RMS)errors in the along-track and cross-track components of BDS-3 broadcast ephemeris show significant reductions from about 25 cm to a level around 10 cm,manifesting an improvement by more than 50%.Therefore,the RTOD accuracy based on spaceborne BDS-3 and BDS-3/GPS combination are significantly affected by the rotation error of BDS-3 ephemeris,which mainly degrades the along-track and cross-track components.For BDS-3 only RTOD,the along-track,cross-track,and radial RMS errors with ro-tation correction are 21.0 cm,10.7 cm,and 11.2 cm,respectively;the along-track and cross-track accuracies present improvements by 15.0%and 31.8%,respectively.By combining BDS-3 and GPS observations,the RTOD errors at the along-track components are further improved to 19.4 cm.Thanks to the high accuracy of BDS-3 broadcast ephemeris,the three-dimensional RMS errors of independent BDS-3 and combined BDS-3/GPS RTOD are 31.9 cm and 29.2 cm,respec-tively,which are 9.1%and 16.8%smaller than GPS-only RTOD errors,respectively.With rota-tion correction,the orbit determination accuracies are improved to 26.7cm and 25.0cm,respec-tively,which is 22.6%and 27.5%smaller than those of single GPS real-time orbit determination.

Low Earth orbit satelliteBeiDou navigation satellite system with global coverage(BDS-3)Broadcast ephemerisReal-time orbit determinationRotation error

李敏、王煜斌、李文文、蒋科材、陈国、赵齐乐

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武汉大学卫星导航定位技术研究中心,武汉 430079

香港理工大学土地测量与地理资讯学系,香港

低轨卫星 北斗三号 广播星历 实时精密定轨 旋转误差

国家自然科学基金国家自然科学基金国家自然科学基金国家自然科学基金国家自然科学基金

4200402042074032420301094220402042204019

2024

导航定位与授时

导航定位与授时

CSTPCD
ISSN:
年,卷(期):2024.11(1)
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