Global searches of frozen orbits around an oblate Earth-like planet

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Yuechen Ma, Yanchao He, Ming Xu, Yaru Zheng
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引用次数: 1

Abstract

A frozen orbit is beneficial for observation owing to its stationary apsidal line. The traditional gravitational field model of frozen orbits only considers the main zonal harmonic terms J2 and limited high-order terms, which cannot meet the stringent demands of all missions. In this study, the gravitational field is expanded to J15 terms and the Hamiltonian canonical form described by the Delaunay variables is used. The zonal harmonic coefficients of the Earth are chosen as the sample. Short-periodic terms are eliminated based on the Hori–Lie transformation. An algorithm is developed to solve all equilibrium points of the Hamiltonian function. A stable frozen orbit with an argument of perigee that equals neither 90◦ nor 270◦ is first reported in this paper. The local stability and topology of the equilibrium points are obtained from their eigenvalues. The bifurcations of the equilibrium points are presented by drawing their global long-term evolution of frozen orbits and their orbital periods. The relationship between the terms of the gravitational field and number of frozen points is addressed to explain why only limited frozen orbits are found in the low-order term case. The analytical results can be applied to other Earth-like planets and asteroids.

在全球范围内搜寻一颗类地扁圆行星的冰冻轨道
冻结轨道由于其静止的顶面线而有利于观测。传统的冻结轨道引力场模型只考虑了主纬向调和项J2和有限的高阶项,不能满足所有任务的严格要求。在这项研究中,引力场被扩展到J15项,并使用Delaunay变量描述的哈密顿正则形式。选取地球的纬向谐波系数作为样本。基于Hori–Lie变换消除了短周期项。提出了一种求解哈密顿函数所有平衡点的算法。一个稳定的冻结轨道,其近地点自变量既不等于90◦ nor 270◦ 是本文首次报道的。平衡点的局部稳定性和拓扑结构是由它们的特征值得到的。通过绘制冻结轨道的全局长期演化及其轨道周期,给出了平衡点的分岔。讨论了引力场项和冻结点数量之间的关系,以解释为什么在低阶项的情况下只发现有限的冻结轨道。分析结果可以应用于其他类地行星和小行星。
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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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