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LRO绕月探测器精密定轨研究
Precise Orbit Determination of LRO Lunar Probe
【摘要】 月球勘测轨道器(lunar reconnaissance orbiter, LRO)为月球科学研究和未来的月球探测任务提供了大量科学数据,其精密轨道的获取是开展其他科学数据研究的前提.利用LRO的白沙站及USN站的S波段射电跟踪数据,使用高精度光压模型并应用高增益天线改正,基于自主的WUDOGS软件对LRO进行了精密定轨.将本文结果与NASA GSFC官方公布的精密轨道进行了对比分析,结果表明使用高精度多帆板模型并进行高增益天线改正后,本文获取的精密轨道与NASA GSFC事后精密轨道的精度相当,位置差距在10 m水平,速度在10 mm/s水平.
【Abstract】 The Lunar Reconnaissance Orbiter(LRO) has provided a vast amount of scientific data for lunar research and future lunar exploration missions,with the acquisition of its precise orbit being a prerequisite for other scientific studies.Based on the independently developed WUDOGS software,this paper performs precise orbit determination for LRO using S-band radio tracking data from the White Sands and USN stations, applying a high-precision solar radiation pressure model and high-gain antenna correction. A comparative analysis between the results of this study and the official precise orbit released by NASA GSFC indicates that,after applying a high-precision multi-panel model and high-gain antenna correction,the obtained precise orbit is comparable in accuracy to NASA GSFC’s post-processed precise orbit,with a positional discrepancy at the 10 m level and velocity accuracy. at the 10 mm/s level.
【Key words】 precise orbit determination; LRO; lunar orbiter; HGA; radiometric tracking data;
- 【文献出处】 空间控制技术与应用 ,Aerospace Control and Application , 编辑部邮箱 ,2025年03期
- 【分类号】V412.41;V476.3
- 【下载频次】41