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Precession of the Earth's axis

Introduction

It has been known since ancient times that the Earth's axis of rotation precesses. That is, the axis itself rotates around the line perpendicular to the ecliptic plane, i.e., the plane containing the Earth's orbit around the Sun. The ancient Greek astronomer Hipparchus concluded that the annual angular displacement of the axis was approximately 45'' (arcseconds), which would imply that the period of axial precession is around 29000 years. Modern measurements indicate that the period is approximately 25800 years. In this problem, you are asked to investigate this phenomenon using Newtonian mechanics.

You may need the following constants:

  • gravitational constant: $G=6.67\times10^{-11}\:\textrm{Nm}^2 / \textrm{kg}^2$
  • average radius of Earth: $R=6.371\times10^6\:\textrm{m}$
  • mass of the Earth: $M_E=5.972\times10^{24}\:\textrm{kg}$
  • average distance of the Sun from the Earth: $d_{SE}=1.496\times10^{11}\:\textrm{m}$
  • mass of the Sun: $M_S=1.989\times10^{30}\:\textrm{kg}$
  • average distance of the Moon from the Earth: $d_{ME}=3.844\times10^8\:\textrm{m}$
  • mass of the Moon: $M_M=7.348\times10^{22}\:\textrm{kg}$
  • Earth's axial tilt: $\alpha=23.5^{\circ}$

Part A. The shape of the Earth (1.0 points)

The Sun and the Moon exert non-zero torques on the Earth because of the Earth's non-spherical shape, giving rise to its axial precession. The main reason behind the Earth's non-spherical shape is the centrifugal force caused by the Earth's rotation about its axis. The tectonic plates located on the Earth's surface have deformed over millions of years to minimise the stresses within them. Therefore, as an approximation, let us model the Earth as a large liquid droplet of uniform density whose shape is determined by centrifugal and gravitational forces. In this model, the Earth's surface is an oblate spheroid (ellipsoid of revolution) characterised by the polar radius $R_p$ and the equatorial radius $R_e$ (see Figure A.1).

Figure A.1. The ellipsoidal shape of the Earth. The polar and equatorial radii are indicated. $\alpha=23.5^\circ$ is the angle between the Earth's axis of rotation and the normal of the ecliptic plane.

The difference between the equatorial and polar radii of the Earth, $h_\textrm{max}=R_e-R_p $ is much smaller than the average radius $R=(R_e+R_p)/2$. Up to a dimensionless constant, the value of $h_\textrm{max}$ can be expressed in terms of the angular speed of the Earth's rotation $\omega$, its mass $M_E$ and average radius $R$ as

$$h_\textrm{max}\propto G^{-1} \omega^\beta M_E^\gamma R^\delta,$$

where $G$ is the gravitational constant, and $\beta$, $\gamma$ and $\delta$ are constant exponents.

A1 Find the values of exponents $\beta$, $\gamma$ and $\delta$.

A2 Calculate the numerical value of $h_\textrm{max}$ assuming that the dimensionless constant for the relation given above is 1.

Regardless of whether you were able to find $h_{\textrm{max}}$ in part A.2., use the empirical value $h_{\textrm{max}}=21~\textrm{km}$ in the following questions.

Part B. The time-averaged gravitational field of the Sun (3.2 points)

To see why the Sun exerts a non-zero torque (with respect to the centre of the Earth) on our planet, consider Figure B.1 below. The difference in distance from the Sun causes the gravitational force $F_1$ to be greater than its counterpart $F_2$.

Figure B.1. Explanation of the non-zero torques exerted by the Sun (right side of the figure) on the Earth (left side).

The magnitude of this torque acting on the Earth varies continuously during the year. In the position shown in Figure B.1, the torque is maximal. A quarter of a year later, due to symmetry, the torque becomes zero. After half a year, it reaches the maximum again. Then after three-quarters of the year it is zero once again, and so on. Since the period of axial precession is much larger than one year, this time-dependent torque can be approximated by its one-year average.

To calculate the average torque exerted by the Sun on the Earth, let us first determine the time average of the gravitational field generated by the Sun in the vicinity of the Earth. This average can be calculated as the field of a uniformly dense ring, a Sun ring, whose mass equals the mass of the Sun $M_S$ and whose radius equals the average distance between the Sun and the Earth $d_{SE}$ (see Figure B.2).

Figure B.2. Time averaging is equivalent to uniformly spreading the Sun along the circle of radius $d_{SE}$.

Let our cylindrical coordinate system have the origin at the centre of the Earth, and let the $z$ axis be perpendicular to the ecliptic plane (i.e. the plane of the ring). The axis of rotation of the Earth makes an angle of $\alpha=23.5^\circ$ with the $z$ axis.

B1 Find the direction and magnitude of the gravitational field generated by the Sun ring at a point on the $z$ axis. Write your answer in terms of $M_S$, $d_{SE}$, and the coordinate $z$. Assume that $\vert z \vert \ll d_{SE}$.

B2 Find the direction and magnitude of the gravitational field generated by the Sun ring at a point in the ecliptic plane whose distance from the origin is $r$. Assume that $r \ll d_{SE}$.

Part C. The torque acting on the Earth (2.6 points)

In this section, you are asked to determine the torque exerted on the Earth due to the gravitational field. For simplicity, consider the Earth as a rigid body with a homogeneous mass distribution. Let us model the rotational ellipsoid as a sphere of radius $R_e$ (the equatorial radius of Earth), with the excess regions at the poles removed (see Figure C.1).

Figure C.1. The ellipsoidal shape of the Earth can be modelled as a sphere of radius $R_e$ with the excess regions at the poles removed.

C1 Find the mass $m$ of one of the two excess regions indicated in Figure C.1. Express your answer in terms of $h_\textrm{max}$, the mass of the Earth $M_E$, and its polar radius $R_p$.

It can be shown that the torque acting on the excess regions is equivalent to the torque acting on two point masses, each with a mass equal to $2m/5$, positioned at the endpoints $A$ and $B$ of the polar diameter (see Figure C.1).

C2 Given this idea, find the torque $\tau$ exerted by the Sun ring on the Earth. Express your answer in terms of $M_E$, $M_S$, $d_{SE}$, $R$ (the average radius), $h_{\textrm{max}}$ and the angle $\alpha$. You can use that $h_\textrm{max}\ll R$.

Part D. Angular speed of the precession of the Earth's axis (2.0 points)

The Earth's axis of rotation moves very slowly around the $z$ axis in a conical motion. That is, it precesses.

D1 Give an expression for the period $T_1$ of precession of the Earth's axis. Express your answer in terms of $M_S$, $d_{SE}$, the angular speed $\omega$ of the Earth's rotation, $h_\textrm{max}$, $R$ and $\alpha$.

D2 Calculate the precession period $T_1$ in years.

Part E. The effect of the Moon (1.2 points)

The value obtained in Part D is much larger than the observed value. The reason for this is that so far we have only considered the torque exerted by the Sun, and neglected the effect of the Moon. In the following calculations, assume that the Moon's orbit is in the ecliptic plane, and that the orbit of the Moon around the Earth is a circle of radius $d_{ME}$. Let us denote the mass of the Moon by $M_M$ and the period of precession in this modified model by $T_2$.

E1 By what factor $T_2/T_1 $ does the period of precession of the Earth's axis change if we also take into account the torque exerted by the Moon? Give your answer in terms of $d_{ME}$, $d_{SE}$, $M_S$ and $M_M$.

E2 By substituting the data, calculate the period of precession $T_2$ in years.