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Long-term dynamical evolution of Tundra-type orbits
Zhang, Ming-Jiang1,2; Zhao, Chang-Yin1,2; Hou, Yong-Gang3; Zhu, Ting-Lei1,2; Wang, Hong-Bo1,2; Sun, Rong-Yu1,2; Zhang, Wei1,2
2017-01-15
Source PublicationADVANCES IN SPACE RESEARCH
ISSN0273-1177
Volume59Issue:2Pages:682-697
Corresponding AuthorZhao, Chang-Yin(cyzhao@pmo.ac.cn)
AbstractTundra-type orbits are elliptical geosynchronous orbits located at the critical inclination. The long-term dynamical evolution of this type of special orbit is investigated in this paper. First, the effect of Earth's gravitational potential is examined. A simplified Hamiltonian of Tundra-type orbits subjected to Earth's gravitational potential is presented through a strict magnitude comparison of the involved terms. Based on this simplified Hamiltonian with two degrees of freedom, the equilibrium points of the orbits subjected to Earth's gravitational potential and their stabilities are discussed. This simplified Hamiltonian is then reduced to a one-degree-of-freedom system dominating the intermediate-period motion of the orbits approximately. In particular, the main characteristic parameters of the intermediate-period motion for nominal Tundra-type orbits and the corresponding specific results for three Sirius satellites in such orbits are presented. Second, the effect of lunisolar perturbations is examined. A magnitude comparison elementarily illustrates that the effect of tesseral harmonics of the Earth's gravitational potential on the long timespan evolution of Tundra-type orbits is negligible compared to that of lunisolar perturbations. A simplified dynamical model including lunisolar perturbations is then presented. Based on this simplified dynamical model, the influences of lunar precession, the initial longitude of the ascending node, the initial argument of perigee, and the initial epoch on the long-term dynamical evolution of the orbits are comparatively analyzed. Finally, numerical calculations with exact perturbation models are conducted to verify the theoretical analysis and to provide more information about the dynamical evolution of Tundra-type orbits. (C) 2016 COSPAR. Published by Elsevier Ltd. All rights reserved.
KeywordTundra-type orbit Dynamical evolution 1:1 tesseral resonance Lunisolar perturbation
DOI10.1016/j.asr.2016.10.016
WOS KeywordARTIFICIAL-SATELLITE ORBITS ; CRITICAL INCLINATION ; MOTION ; PERTURBATIONS ; STABILITY ; DESIGN ; CHAOS
Indexed BySCI
Language英语
WOS Research AreaAstronomy & Astrophysics ; Geology ; Meteorology & Atmospheric Sciences
WOS SubjectAstronomy & Astrophysics ; Geosciences, Multidisciplinary ; Meteorology & Atmospheric Sciences
WOS IDWOS:000392773700016
PublisherELSEVIER SCI LTD
Citation statistics
Document Type期刊论文
Identifierhttp://libir.pmo.ac.cn/handle/332002/23319
Collection中国科学院紫金山天文台
Corresponding AuthorZhao, Chang-Yin
Affiliation1.Chinese Acad Sci, Purple Mt Observ, Nanjing 210008, Jiangsu, Peoples R China
2.Chinese Acad Sci, Purple Mt Observ, Key Lab Space Object & Debris Observat, Nanjing 210008, Jiangsu, Peoples R China
3.Jinan Univ, Sch Commerce, Jinan 250022, Peoples R China
Recommended Citation
GB/T 7714
Zhang, Ming-Jiang,Zhao, Chang-Yin,Hou, Yong-Gang,et al. Long-term dynamical evolution of Tundra-type orbits[J]. ADVANCES IN SPACE RESEARCH,2017,59(2):682-697.
APA Zhang, Ming-Jiang.,Zhao, Chang-Yin.,Hou, Yong-Gang.,Zhu, Ting-Lei.,Wang, Hong-Bo.,...&Zhang, Wei.(2017).Long-term dynamical evolution of Tundra-type orbits.ADVANCES IN SPACE RESEARCH,59(2),682-697.
MLA Zhang, Ming-Jiang,et al."Long-term dynamical evolution of Tundra-type orbits".ADVANCES IN SPACE RESEARCH 59.2(2017):682-697.
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