Long-term dynamical evolution of Tundra-type orbits
文献类型：期刊论文
| 作者 | 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 |
| 刊名 | ADVANCES IN SPACE RESEARCH
 |
| 出版日期 | 2017-01-15 |
| 卷号 | 59期号:2页码:682-697 |
| ISSN号 | 0273-1177 |
| 关键词 | Tundra-type orbit Dynamical evolution 1:1 tesseral resonance Lunisolar perturbation |
| DOI | 10.1016/j.asr.2016.10.016 |
| 通讯作者 | Zhao, Chang-Yin(cyzhao@pmo.ac.cn) |
| 英文摘要 | Tundra-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. |
| WOS关键词 | ARTIFICIAL-SATELLITE ORBITS ; CRITICAL INCLINATION ; MOTION ; PERTURBATIONS ; STABILITY ; DESIGN ; CHAOS |
| WOS研究方向 | Astronomy & Astrophysics ; Geology ; Meteorology & Atmospheric Sciences |
| 语种 | 英语 |
| 出版者 | ELSEVIER SCI LTD |
| WOS记录号 | WOS:000392773700016 |
| 源URL | [http://libir.pmo.ac.cn/handle/332002/23318]  |
| 专题 | 中国科学院紫金山天文台 |
| 通讯作者 | Zhao, Chang-Yin |
| 作者单位 | 1.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 |
| 推荐引用方式 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. |
入库方式： OAI收割
来源：紫金山天文台
浏览0
下载0
收藏0
其他版本
除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。