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基于最新数值行星历表的行星轨道仿真研究

Planetary Orbit Simulation Based on the Latest Numerical Planetary Ephemeris
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摘要 为发展月球和行星探测,美国喷气推进实验室(Jet Propulsion Laboratory,JPL)、法国天体力学与历算研究所(Institut de Mécanique Céleste et de Calcul deséphémérides,IMCCE)、俄罗斯科学院应用天文研究所(Institute of Applied Astronomy of the Russian Academy of Sciences,IAA RAS)分别研制了各自的行星历表。就各个行星历表的发展历程进行概括,对最新版本的3个历表DE438、INPOP19a和EPM2017进行分析,并通过仿真计算比较了月球和行星在太阳质心参考系中的位置和速度的差异,评估了最新历表的相对精度,为中国深空探测和自主历表研制提供技术支撑。结果表明,历表间差异均较小,但月球历表的精度有待提高。 To develop lunar and planetary exploration,Jet Propulsion Laboratory(JPL)in America,French Institute of Astromechanics and Ephemeris,and Institute of Applied Astronomy of Russian Academy of Sciences have developed their own planetary ephemeris.We summarize the development history of each planetary ephemeris,and analyze the latest versions of three ephemeris(DE438,INPOP19a and EPM2017).Through simulation calculation,we compare the differences of positions and velocities of the moon and planets in the solar centroid reference system,and evaluate the relative accuracy of the latest ephemeris,which provides technical support for deep space exploration and development of independent ephemeris in China.The results show that the differences between ephemeris are small,while the accuracy of lunar ephemeris needs to be improved.
作者 孙尚彪 杨永章 马卓希 鄢建国 SUN Shangbiao;YANG Yongzhang;MA Zhuoxi;YAN Jianguo(State Key Laboratory of Information Engineering in Surveying,Mapping and Remote Sensing,Wuhan University,Wuhan 430079,China;Xi’an Technical Division of Surveying and Mapping,Xi’an 710054,China)
出处 《测绘地理信息》 CSCD 2022年第5期42-46,共5页 Journal of Geomatics
基金 国家自然科学基金(U1831132) 国家社会科学基金(2020-SKJJ-C-043)
关键词 行星历表 深空探测 喷气推进实验室(Jet Propulsion Laboratory JPL) INPOP EPM planetary ephemeris deep space exploration Jet Propulsion Laboratory(JPL) INPOP EPM
作者简介 第一作者:孙尚彪,硕士生,主要研究方向为行星探测器精密定轨。E-mail:sunsb2021@whu.edu.cn;通讯作者:杨永章,博士,主要研究方向为天体力学、月球动力学的数值及月球微波测距测速。E-mail:yang.yongzhang@whu.edu.cn
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