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Analytic model for the long-term evolution of circular Earth satellite orbits including lunar node regression
Zhu, Ting-Lei; Zhao, Chang-Yin; Zhang, Ming-Jiang
刊名ASTROPHYSICS AND SPACE SCIENCE
2017
卷号362期号:4页码:69-
英文摘要This paper aims to obtain an analytic approximation to the evolution of circular orbits governed by the Earth's J(2) and the luni-solar gravitational perturbations. Assuming that the lunar orbital plane coincides with the ecliptic plane, Allan and Cook (Proc. R. Soc. A, Math. Phys. Eng. Sci. 280(1380):97, 1964) derived an analytic solution to the orbital plane evolution of circular orbits. Using their result as an intermediate solution, we establish an approximate analytic model with lunar orbital inclination and its node regression be taken into account. Finally, an approximate analytic expression is derived, which is accurate compared to the numerical results except for the resonant cases when the period of the reference orbit approximately equals the integer multiples (especially 1 or 2 times) of lunar node regression period.
语种英语
内容类型期刊论文
源URL[http://libir.pmo.ac.cn/handle/332002/17359]  
专题中国科学院紫金山天文台
推荐引用方式
GB/T 7714
Zhu, Ting-Lei,Zhao, Chang-Yin,Zhang, Ming-Jiang. Analytic model for the long-term evolution of circular Earth satellite orbits including lunar node regression[J]. ASTROPHYSICS AND SPACE SCIENCE,2017,362(4):69-.
APA Zhu, Ting-Lei,Zhao, Chang-Yin,&Zhang, Ming-Jiang.(2017).Analytic model for the long-term evolution of circular Earth satellite orbits including lunar node regression.ASTROPHYSICS AND SPACE SCIENCE,362(4),69-.
MLA Zhu, Ting-Lei,et al."Analytic model for the long-term evolution of circular Earth satellite orbits including lunar node regression".ASTROPHYSICS AND SPACE SCIENCE 362.4(2017):69-.
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