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Tennis racket theorem : ウィキペディア英語版
Tennis racket theorem
The tennis racket theorem or intermediate axis theorem is a result in classical mechanics describing the movement of a rigid body with three distinct principal moments of inertia. It is also dubbed the Dzhanibekov effect, after Russian astronaut Vladimir Dzhanibekov who discovered the theorem's consequences while in space in 1985.〔(Эффект Джанибекова (гайка Джанибекова) ), 23 July 2009 〕 An article explaining the effect was published in 1991.
The theorem describes the following effect: rotation of an object about its first and third principal axes is stable, while rotation about its second principal axis (or intermediate axis) is not.
This can be demonstrated with the following experiment: hold a tennis racket at its handle, with face horizontal, and try to throw it in the air so that it will perform a full rotation about the horizontal axis perpendicular to the handle, and try to catch the handle. In almost all cases, during that rotation the face will also have completed a half rotation, so that the other face is now up. By contrast, it is easy to throw the racket so that it will rotate about the handle axis (the third principal axis) without accompanying half-rotation about another axis; it is also possible to make it rotate about the vertical axis perpendicular to the handle (the first principal axis) without any accompanying half-rotation.
The experiment can be performed with any object that has three different moments of inertia, for instance with a book or a remote control. The effect occurs whenever the axis of rotation differs slightly from the object's second principal axis; air resistance or gravity are not necessary.
== Qualitative discussion ==
The tennis racket theorem can be qualitatively analysed with the help of Euler's equations.
Under torque free conditions, they take the following form:
:
\begin
I_1\dot_&=(I_2-I_3)\omega_2\omega_3~~~~~~~~~~~~~~~~~~~~\text\\
I_2\dot_&=(I_3-I_1)\omega_3\omega_1~~~~~~~~~~~~~~~~~~~~\text\\
I_3\dot_&=(I_1-I_2)\omega_1\omega_2~~~~~~~~~~~~~~~~~~~~\text
\end

Here I_1, I_2, I_3 denote the object's principal moments of inertia, and we assume I_1 > I_2 > I_3. The angular velocities about the object's three principal axes are \omega_1, \omega_2, \omega_3 and their time derivatives are denoted by \dot\omega_1, \dot\omega_2, \dot\omega_3.
Consider the situation when the object is rotating about axis with moment of inertia I_1. To determine the nature of equilibrium, assume small initial angular velocities along the other two axes. As a result, according to equation (1), ~\dot_ is very small. Therefore the time dependence of ~\omega_1 may be neglected.
Now, differentiating equation (2) and substituting \dot_3 from equation (3),
:
\begin
I_2 I_3 \ddot_&= (I_3-I_1) (I_1-I_2)(\omega_1)^2\omega_\\
\text~~~~ \ddot_2 &= \text \times \omega_2
\end

Note that \omega_2 is being opposed and so rotation around this axis is stable for the object.
Similar reasoning gives that rotation around axis with moment of inertia I_3 is also stable.
Now apply the same analysis to axis with moment of inertia I_2. This time \dot_ is very small. Therefore the time dependence of ~\omega_2 may be neglected.
Now, differentiating equation (1) and substituting \dot_3 from equation (3),
:
\begin
I_1 I_3 \ddot_&= (I_2-I_3) (I_1-I_2) (\omega_)^2\omega_1\\
\text~~~~ \ddot_1 &= \text \times \omega_1
\end

Note that \omega_1 is ''not'' opposed (and therefore will grow) and so rotation around the 2 axis is ''unstable''. Therefore even a small disturbance along other axes causes the object to 'flip'.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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