Analytical development of the lunisolar disturbing function and the critical inclination secular resonance

被引:0
作者
Alessandra Celletti
Cătălin Galeş
Giuseppe Pucacco
Aaron J. Rosengren
机构
[1] University of Rome Tor Vergata,Department of Mathematics
[2] Al. I. Cuza University,Department of Mathematics
[3] University of Rome Tor Vergata,Department of Physics
[4] IFAC-CNR,undefined
来源
Celestial Mechanics and Dynamical Astronomy | 2017年 / 127卷
关键词
Lunisolar perturbations; Disturbing function expansion; Artificial satellites; Space debris; Critical inclination; Secular resonance; Molniya orbits;
D O I
暂无
中图分类号
学科分类号
摘要
We provide a detailed derivation of the analytical expansion of the lunar and solar disturbing functions. Although there exist several papers on this topic, many derivations contain mistakes in the final expansion or rather (just) in the proof, thereby necessitating a recasting and correction of the original derivation. In this work, we provide a self-consistent and definite form of the lunisolar expansion. We start with Kaula’s expansion of the disturbing function in terms of the equatorial elements of both the perturbed and perturbing bodies. Then we give a detailed proof of Lane’s expansion, in which the elements of the Moon are referred to the ecliptic plane. Using this approach the inclination of the Moon becomes nearly constant, while the argument of perihelion, the longitude of the ascending node, and the mean anomaly vary linearly with time. We make a comparison between the different expansions and we profit from such discussion to point out some mistakes in the existing literature, which might compromise the correctness of the results. As an application, we analyze the long-term motion of the highly elliptical and critically-inclined Molniya orbits subject to quadrupolar gravitational interactions. The analytical expansions presented herein are very powerful with respect to dynamical studies based on Cartesian equations, because they quickly allow for a more holistic and intuitively understandable picture of the dynamics.
引用
收藏
页码:259 / 283
页数:24
相关论文
共 49 条
[1]  
Allan RR(1965)On the motion of nearly synchronous satellites Proc. R. Soc. Lond. A 288 60-68
[2]  
Breiter S(2001)Lunisolar resonances revisited Celest. Mech. Dyn. Astr. 81 81-91
[3]  
Celletti A(2014)On the dynamics of space debris: 1:1 and 2:1 resonances J. Nonlinear Sci. 24 1231-1262
[4]  
Galeş C(1994)Frozen orbits for satellites close to an Earth-like planet Celest. Mech. Dyn. Astr. 59 37-72
[5]  
Coffey SL(1978)On the perturbations of a close-Earth satellite due to lunar inequalities Celest. Mech. 16 459-479
[6]  
Deprit A(1962)Luni-solar perturbations of the orbit of an Earth satellite Geophys. J. 6 271-291
[7]  
Deprit E(1993)Luni-solar effects of geosynchronous orbits at the critical inclination Celest. Mech. Dyn. Astr. 57 155-173
[8]  
Cok DR(2013)Dynamics of orbits near 3:1 resonance in the Earth–Moon system J. Astronaut. Sci. 60 51-86
[9]  
Cook GE(2000)The disturbing function in solar system dynamics Icarus 147 129-144
[10]  
Delhaise F(1997)Dynamics of artificial satellite orbits with tesseral resonances including the effects of luni-solar perturbations Int. J. Dyn. Stab. Syst. 12 243-269