The axis of a gyroscope is free to rotate within a smooth horizontal circle in
colatitude \(\lambda\). Due to the Coriolis force, there is a couple on the
gyroscope. To find the effect of this couple, use the equation for the rate of
change of angular momentum in a frame rotating with the Earth (e.g., that of
Fig. 5.7), \(\dot{\boldsymbol{J}}+\boldsymbol{\Omega} \wedge
\boldsymbol{J}=\boldsymbol{G}\), where \(\boldsymbol{G}\) is the couple
restraining the axis from leaving the horizontal plane, and
\(\boldsymbol{\Omega}\) is the Earth's angular velocity. (Neglect terms of order
\(\Omega^{2}\), in particular the contribution of \(\boldsymbol{\Omega}\) to
\(\boldsymbol{J} .\) ) From the component along the axis, show that the angular
velocity \(\omega\) about the axis is constant; from the vertical component show
that the angle \(\varphi\) between the axis and east obeys the equation
\(I_{1} \ddot{\varphi}-I_{3} \omega \Omega \sin \lambda \cos \varphi=0\)
Show that the stable position is with the axis pointing north. Determine the
period of small oscillations about this direction if the gyroscope is a flat
circular disc spinning at 6000 r.p.m. in latitude \(30^{\circ} \mathrm{N}\).
Explain why this system is sensitive to the horizontal component of
\(\boldsymbol{\Omega}\), and describe the effect qualitatively from the point of
view of an inertial observer.