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Next: Rotational Stability Up: Rigid Body Rotation Previous: Eulerian Angles


Gyroscopic Precession

Let us now study the motion of a rigid rotationally symmetric top which is free to turn about a fixed point (without friction), but which is subject to a gravitational torque--see Figure 30. Suppose that the $z'$-axis coincides with the symmetry axis. Let the principal moment of inertia about the symmetry axis be $I_\parallel$, and let the other principal moments both take the value $I_\perp$. Suppose that the $z$-axis points vertically upward, and let the common origin, $O$, of the fixed and body frames coincide with the fixed point about which the top turns. Suppose that the center of mass of the top lies a distance $l$ along its symmetry axis from point $O$, and that the mass of the top is $m$. Let the symmetry axis of the top subtend an angle $\theta $ (which is an Eulerian angle) with the upward vertical.

Figure 30: A symmetric top.
\begin{figure}
\epsfysize =2.5in
\centerline{\epsffile{Chapter08/fig8.03.eps}}
\end{figure}

Consider an instant in time at which the Eulerian angle $\psi$ is zero. This implies that the $x'$-axis is horizontal [see Equation (534)], as shown in the diagram. The gravitational force, which acts at the center of mass, thus exerts a torque $m\,g\,l\,
\sin\theta$ in the $x'$-direction. Hence, the components of the torque in the body frame are

$\displaystyle T_{x'}$ $\textstyle =$ $\displaystyle m\,g\,l\,\sin\theta,$ (556)
$\displaystyle T_{y'}$ $\textstyle =$ $\displaystyle 0,$ (557)
$\displaystyle T_{z'}$ $\textstyle =$ $\displaystyle 0.$ (558)

The components of the angular velocity vector in the body frame are given by Equations (537)-(539). Thus, Euler's equations (504)-(506) take the form:
$\displaystyle m\,g\,l\,\sin\theta$ $\textstyle =$ $\displaystyle I_\perp\,(\ddot{\theta}- \cos\theta\,\sin\theta\,\dot{\phi}^{\,2}) + L_\psi\,\sin\theta\,\dot{\phi},$ (559)
$\displaystyle 0$ $\textstyle =$ $\displaystyle I_\perp\,(2\,\cos\theta\,\dot{\theta}\,\dot{\phi} +\sin\theta\,\ddot{\phi}) - L_\psi\,\dot{\theta},$ (560)
$\displaystyle 0$ $\textstyle =$ $\displaystyle \dot{L}_\psi,$ (561)

where
\begin{displaymath}
L_\psi = I_\parallel\,(\cos\theta\,\dot{\phi}+\dot{\psi})= I_\parallel\,{\mit\Omega},
\end{displaymath} (562)

and ${\mit\Omega} = \omega_{z'}$ is the angular velocity of the top. Multiplying Equation (560) by $\sin\theta$, we obtain
\begin{displaymath}
\dot{L}_\phi = 0,
\end{displaymath} (563)

where
\begin{displaymath}
L_\phi = I_\perp\,\sin^2\theta\,\dot{\phi} + L_\psi\,\cos\theta.
\end{displaymath} (564)

According to Equations (561) and (563), the two quantities $L_\psi$ and $L_\phi$ are constants of the motion. These two quantities are the angular momenta of the system about the $z'$- and $z$-axis, respectively. (To be more exact, they are the generalized momenta conjugate to the coordinates $\psi$ and $\phi$, respectively--see Section 9.8.) They are conserved because the gravitational torque has no component along either the $z'$- or the $z$-axis. (Alternatively, they are conserved because the Lagrangian of the top does not depend explicitly on the coordinates $\psi$ and $\theta $--see Section 9.8.)

If there are no frictional forces acting on the top then the total energy, $E=K+U$, is also a constant of the motion. Now,

\begin{displaymath}
E = \frac{1}{2}\,\left(I_\perp\,\omega_{x'}^{\,2} + I_\perp\...
...+
I_\parallel\,\omega_{z'}^{\,2}\right) + m\,g\,l\,\cos\theta.
\end{displaymath} (565)

When written in terms of the Eulerian angles (with $\psi=0$), this becomes
\begin{displaymath}
E=\frac{1}{2}\left(I_\perp\,\dot{\theta}^{\,2} + I_\perp\,\s...
...{\,2} + L_\psi^{\,2}/I_\parallel\right) + m\,g\,l\,\cos\theta.
\end{displaymath} (566)

Eliminating $\dot{\phi}$ between Equations (564) and (566), we obtain the following differential equation for $\theta $:
\begin{displaymath}
E = \frac{1}{2}\,I_\perp\,\dot{\theta}^{\,2} + \frac{(L_\phi...
...c{1}{2}\frac{L_\psi^{\,2}}{I_\parallel} + m\,g\,l\,\cos\theta.
\end{displaymath} (567)

Let
\begin{displaymath}
E' = E - \frac{1}{2}\frac{L_\psi^{\,2}}{I_\parallel},
\end{displaymath} (568)

and $u=\cos\theta$. It follows that
\begin{displaymath}
\dot{u}^{\,2} = 2\,(E' -m\,g\,l\,u)\,(1-u^2)\,I_\perp^{-1} - (L_\phi-L_\psi\,u)^2\,I_\perp^{-2},
\end{displaymath} (569)

or
\begin{displaymath}
\dot{u}^{\,2} = f(u),
\end{displaymath} (570)

where $f(u)$ is a cubic polynomial. In principal, the above equation can be integrated to give $u$ (and, hence, $\theta $) as a function of $t$:
\begin{displaymath}
t = \int_{u_0}^u\frac{du'}{\sqrt{f(u')}}.
\end{displaymath} (571)

Fortunately, we do not have to perform the above integration (which is very ugly) in order to discuss the general properties of the solution to Equation (570). It is clear, from Equation (571), that $f(u)$ needs to be positive in order to obtain a physical solution. Hence, the limits of the motion in $\theta $ are determined by the three roots of the equation $f(u)=0$. Since $\theta $ must lie between $0$ and $\pi/2$, it follows that $u$ must lie between 0 and 1. It can easily be demonstrated that $f\rightarrow\pm\infty$ as $u\rightarrow\pm\infty$. It can also be shown that the largest root $u_3$ lies in the region $u_3>1$, and the two smaller roots $u_1$ and $u_2$ (if they exist) lie in the region $-1\leq u\leq +1$. It follows that, in the region $-1\leq u\leq 1$, $f(u)$ is only positive between $u_1$ and $u_2$. Figure 31 shows a case where $u_1$ and $u_2$ lie in the range 0 to 1. The corresponding values of $\theta $--$\theta_1$ and $\theta_2$, say--are then the limits of the vertical motion. The axis of the top oscillates backward and forward between these two values of $\theta $ as the top precesses about the vertical axis. This oscillation is called nutation. Incidentally, if $u_1$ becomes negative then the nutation will cause the top to strike the ground (assuming that it is spinning on a level surface).

Figure 31: The function $f(u)$.
\begin{figure}
\epsfysize =2.5in
\centerline{\epsffile{Chapter08/fig8.04.eps}}
\end{figure}

If there is a double root of $f(u)=0$ (i.e., if $u_1 = u_2$) then there is no nutation, and the top precesses steadily. However, the criterion for steady precession is most easily obtained directly from Equation (559). In the absence of nutation, $\dot{\theta}=\ddot{\theta}=0$. Hence, we obtain

\begin{displaymath}
m\,g\,l = -I_\perp\,\cos\theta\,\dot{\phi}^{\,2}+ L_\psi\,\dot{\phi},
\end{displaymath} (572)

or
\begin{displaymath}
{\mit\Omega}= \frac{m\,g\,l}{I_\parallel\,\dot{\phi}} + \frac{I_\perp}{I_\parallel}\,\cos\theta\,\dot{\phi}.
\end{displaymath} (573)

The above equation is the criterion for steady precession. Since the right-hand side of Equation (573) possesses a minimum value, which is given by $2\,\sqrt{m\,g\,l\,I_\perp\,\cos\theta}/I_\parallel$, it follows that
\begin{displaymath}
{\mit\Omega} > {\mit\Omega}_{\rm crit} = \frac{2\,\sqrt{m\,g\,l\,I_\perp\,\cos\theta}}{I_\parallel}
\end{displaymath} (574)

is a necessary condition for obtaining steady precession at the inclination angle $\theta $. For ${\mit\Omega}>{\mit\Omega}_{\rm crit}$, there are two roots to Equation (573), corresponding to a slow and a fast steady precession rate for a given inclination angle $\theta $. If ${\mit\Omega}\gg {\mit\Omega}_{\rm crit}$ then these two roots are approximately given by
$\displaystyle (\dot{\phi})_{\rm slow}$ $\textstyle \simeq$ $\displaystyle \frac{m\,g\,l}{I_\parallel\,{\mit\Omega}},$ (575)
$\displaystyle (\dot{\phi})_{\rm fast}$ $\textstyle \simeq$ $\displaystyle \frac{I_\parallel\,{\mit\Omega}}{I_\perp\,\cos\theta}.$ (576)

The slower of these two precession rates is the one which is generally observed.


next up previous
Next: Rotational Stability Up: Rigid Body Rotation Previous: Eulerian Angles
Richard Fitzpatrick 2011-03-31