On the anomalous increase of the lunar eccentricity

Reading time: 5 minute
...

📝 Original Info

  • Title: On the anomalous increase of the lunar eccentricity
  • ArXiv ID: 1105.4863
  • Date: 2011-05-24
  • Authors: Lorenzo Iorio

📝 Abstract

Possible explanations of the recently reported anomalous increase of the eccentricity of the lunar orbit are sought in terms of classical Newtonian mechanics, general relativity, and long-range modifications of gravity.

💡 Deep Analysis

Deep Dive into On the anomalous increase of the lunar eccentricity.

Possible explanations of the recently reported anomalous increase of the eccentricity of the lunar orbit are sought in terms of classical Newtonian mechanics, general relativity, and long-range modifications of gravity.

📄 Full Content

Anderson and Nieto, in a recent review 1 of some astrometric anomalies detected in the solar system by some independent groups, mentioned also an anomalous secular increase of the eccentricity e of the orbit of the Moon ėmeas = (9 ± 3) × 10 -12 yr -1

(1)

based on an analysis of a long LLR data record spanning 38.7 yr performed by Williams and Boggs 2 with the dynamical force models of the DE421 ephemerides 3,4 including all the known relevant Newtonian and Einsteinian effects. Notice that Eq. 1 is statistically significant at a 3σ-level. The first account 5 of this effect appeared in 2001 by Williams et al., who gave an extensive discussion of the state-of-the-art in modeling the tidal dissipation in both the Earth and the Moon. Later, Williams and Dickey 6 , relying upon the 2001 study 5 , released an anomalous eccentricity rate as large as ėmeas = (1.6 ± 0.5) × 10 -11 yr -1 . Anderson and Nieto 1 commented that Eq. 1 is not compatible with present, standard knowledge of the dissipative processes in the interiors of both the Earth and Moon, which were, actually, modeled by Williams and Boggs 2 .

Naive, dimensional evaluations of the effect caused on e by an additional anomalous acceleration A can be made by noticing that

for the geocentric orbit of the Moon, whose mass is denoted as m. In it, a is the orbital semimajor axis, while n . = µ/a 3 is the Keplerian mean motion in which µ .

= GM (1 + m/M ) is the gravitational parameter of the Earth-Moon system: G is the Newtonian constant of gravitation and M is the mass of the Earth. It turns out that an extra-acceleration as large as

would satisfy Eq. 1. In fact, a mere order-of-magnitude analysis based on Eq. 2 would be inadequate to infer meaningful conclusions: finding simply that this or that dynamical effect induces an extra-acceleration of the right order of magnitude may be highly misleading. Indeed, exact calculations of the secular variation of e caused by such putative promising candidate extra-accelerations A must be performed with standard perturbative techniques in order to check if they, actually, cause an averaged non-zero change of the eccentricity. Moreover, it may well happen, in principle, that the resulting analytical expression for ė retains multiplicative factors 1/e j , j = 1, 2, 3, … or e j , j = 1, 2, 3… which would notably alter the size of the found non-zero secular change of the eccentricity with respect to the expected values according to Eq. 2.

It is well known that a variety of theoretical paradigms 7,8 allow for Yukawa-like deviations 9 from the usual Newtonian inverse-square law of gravitation. The Yukawa-type correction to the Newtonian gravitational potential U N = -µ/r, where µ . = GM is the gravitational parameter of the central body which acts as source of the supposedly modified gravitational field, is

in which µ ∞ is the gravitational parameter evaluated at distances r much larger than the scale length λ. In order to compute the long-term effects of Eq. 5 on the eccentricity of a test particle it is convenient to adopt the Lagrange perturbative scheme 10 . In such a framework, the equation for the long-term variation of e is 10

where ω is the argument of pericenter, M is the mean anomaly of the test particle, and R denotes the average of the perturbing potential over one orbital revolution. In the case of a Yukawa-type perturbation, Eq. 5 yields

where I 0 (x) is the modified Bessel function of the first kind I q (x) for q = 0. An inspection of Eq. 6 and Eq. 7 immediately tells us that there is no secular variation of e caused by an anomalous Yukawa-type perturbation.

The size of the general relativistic Lense-Thirring 11 acceleration experienced by the Moon because of the Earth’s angular momentum 12 S = 5.86 × 10 33 kg m 2 s -1 is just

i.e. close to Eq. 4. On the other hand, it is well known that the Lense-Thirring effect does not cause long-term variations of the eccentricity. Indeed, the integrated shift of e from an initial epoch corresponding to f 0 to a generic time corresponding to f is 13

in which I ′ is the inclination of the Moon’s orbit with respect to the Earth’s equator and f is the true anomaly. From Eq. 9 it straightforwardly follows that after one orbital revolution, i.e. for f → f 0 + 2π, the long-term gravitomagnetic shift of e vanishes.

A promising candidate for explaining the anomalous increase of the lunar eccentricity is, at least in principle, a trans-Plutonian massive body X of planetary size located in the remote peripheries of the solar system. Indeed, the perturbation induced by it would, actually, cause a non-vanishing long-term variation of e. Moreover, since it depends on the spatial position of X in the sky and on its tidal parameter

where m X and d X are the mass and the distance of X, respectively, it may happen that a suitable combination of them is able to reproduce Eq. 1. Let us recall that, in general, the perturbing potential felt by a test particle orbiting a centr

…(Full text truncated)…

📸 Image Gallery

cover.png

Reference

This content is AI-processed based on ArXiv data.

Start searching

Enter keywords to search articles

↑↓
ESC
⌘K Shortcut