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Dynamical Model of Rotation and Orbital Coupling for Deimos
Huang K(黄凯)1,2; Zhang LJ(张利军)1,2; Yang YZ(杨永章)1,3; Ye, Mao4; Li YQ(李语强)1,5
发表期刊REMOTE SENSING
2024-04
卷号16期号:7
DOI10.3390/rs16071174
产权排序第1完成单位
收录类别EI ; SCI
关键词celestial mechanics Deimos rotation dynamical model adjustment model numerical integration ephemerides
摘要This paper introduces a novel dynamical model, building upon the existing dynamical model for Deimos in the current numerical ephemerides, which only encompasses the simple libration effects of Deimos. The study comprehensively incorporates the rotational dynamics of Deimos influenced by the torque exerted by the major celestial bodies (Mars, the Sun) in the solar system within the inertial space. Consequently, a full dynamical model is formulated to account for the complete coupling between the rotation and orbit of Deimos. Simultaneously, employing precision orbit determination methods used for artificial satellites, we develop an adjustment model for fitting data to the complete model. The 12-order Adams-Bashforth-Moulton (ABM) integration algorithm is employed to synchronously integrate the 12 state variables of the full model to obtain the orbit of Deimos.The difference in the orbits obtained by integrating the full model over a period of 10 years and those obtained by the simplified model is at the order of 10 km. After precise orbit determination, this difference decreases to below 100 m, so numerical simulation results indicate that the full dynamical model and adjustment model are stable and reliable. Simultaneously, the integration of the Deimos third-order gravity field in the full model over a 10-year period induces only meter-level positional changes. This suggests that when constructing the complete model, the utilization of a second-order gravity field alone is sufficient. Compared to the simple model, the polar axis of Deimos in the inertial space exhibits a more complex oscillation in the full model. Additionally, the full model calculates that the minimum moment of inertia principal axis of Phobos has an amplitude of approximately 0.5 degrees in the longitude direction and does not exceed 2 degrees in the latitude direction. This work further advances the current dynamical model for Deimos and establishes the foundational model for the generation of a new set of precise numerical ephemerides for Deimos.
资助项目National Natural Science Foundation of China
项目资助者National Natural Science Foundation of China
语种英语
学科领域天文学 ; 天文学:天体测量学
文章类型Article
出版者MDPI
出版地ST ALBAN-ANLAGE 66, CH-4052 BASEL, SWITZERLAND
URL查看原文
WOS记录号WOS:001200882600001
WOS研究方向Environmental Sciences & Ecology ; Geology ; Remote Sensing ; Imaging Science & Photographic Technology
WOS类目Environmental Sciences ; Geosciences, Multidisciplinary ; Remote Sensing ; Imaging Science & Photographic Technology
关键词[WOS]MARTIAN SATELLITES ; MOTION ; ESAPHO ; EPHEMERIDES ; LIBRATION ; MARS
EI入藏号20241615920552
EI主题词Rotation
EI分类号657.2 Extraterrestrial Physics and Stellar Phenomena - 921 Mathematics - 921.2 Calculus - 931.1 Mechanics
引用统计
被引频次:1[WOS]   [WOS记录]     [WOS相关记录]
文献类型期刊论文
版本出版稿
条目标识符http://ir.ynao.ac.cn/handle/114a53/27051
专题应用天文研究组
作者单位1.Yunnan Observatories, Chinese Academy of Sciences, Kunming 650216, China;
2.University of Chinese Academy of Sciences, Beijing 100049, China;
3.Project Supported by MOE Key Laboratory of TianQin Project, Sun Yat-sen University, Zhuhai 519082, China;
4.State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430079, China;
5.Key Laboratory of Space Object and Debris Observation, PMO, CAS, Nanjing 210023, China
第一作者单位中国科学院云南天文台
推荐引用方式
GB/T 7714
Huang K,Zhang LJ,Yang YZ,et al. Dynamical Model of Rotation and Orbital Coupling for Deimos[J]. REMOTE SENSING,2024,16(7).
APA 黄凯,张利军,杨永章,Ye, Mao,&李语强.(2024).Dynamical Model of Rotation and Orbital Coupling for Deimos.REMOTE SENSING,16(7).
MLA 黄凯,et al."Dynamical Model of Rotation and Orbital Coupling for Deimos".REMOTE SENSING 16.7(2024).
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