which determines t as a function of R by a quadrature; if ()f R is a rational function of
sin R and cos R and if we take as a new variable
()
tan / 2R , then we obtain a
hyperelliptic integral. Taking into account the geometric significance of the function
()f R , specified by the relation (17.1.28), it results that the integral can take only finite
values. We notice that, for
= 0R and =RQ, the function in the second member of the
equation (17.1.34) takes negative values; for
=
0
RR, at the initial moment, the function
can take only a positive value, corresponding to a real value of
R
. It results
0
12
RRR<<, where
1
R and
2
R are two real zeros of the mentioned function. Thus, we
can make for the equation (17.1.34) a study analogous to that in Sects. 15.2.1.1 and
15.2.1.2. In this context, Puiseux showed that one can choose an initial angular velocity
0
3
X sufficiently great so that ()tR remain close to
0
R
at any moment t, the motion of
the rigid solid being thus stable. But Thomson showed that supplementary constraints,
instead to increase the stability of the rigid solid, could lead to a loss of the stability of
its motion (the rigid solid overturns).
We notice that the straight line
QN , normal to the meridian plane, is parallel to the
line of nodes; in this case, if we use the
′
1
Ox -axis, parallel to the fixed axis
′′
1
Ox , the
point
Q being chosen as pole, then the contact point P will be specified by the polar co-
ordinates E and
=+3/2DZ Q . The first equation (17.1.33) leads thus to the equation
()
0
3
2
1
cos
sin
aDBXR
R
=−
.
(17.1.35)
Eliminating d
t between the equations (17.1.34) and (17.1.35), we find an equation with
separate variables which gives the angle Dby a quadrature as a function of the angle R;
taking into account (17.1.29''), it results a relation which links D to E. We obtain thus
the curve described by the contact point
P in the fixed plane P.
If the mass centre is not projected at a fixed point
Q on the plane P, then we observe
that this point has a rectilinear and uniform motion; we report the relative motion to a
frame of reference
′′′
123
Qx x x , observing that this frame is inertial too. Hence, the
relative motion is governed by the same differential equations as the absolute motion; in
the movable frame, the point
Q is fixed, so that the problem is reduced to that studied
above.
As an application, one can study Gervat’s gyroscope (the “equilibrist foot”)
previously considered in Sect. 16.2.1.1.
17.1.2.5 Frictionless Motion of a Heavy Gyroscope on a Fixed Horizontal Plane
The gyroscope is a rigid solid for which the ellipsoid of inertia relative to a fixed point
of it is of rotation. In our case, the fixed point is the contact point
P (at a given
moment), assuming that the gyroscope is bounded at the vicinity of this point by a
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