2.I.9C

Classical Dynamics | Part II, 2005

A rigid body has principal moments of inertia I1,I2I_{1}, I_{2} and I3I_{3} and is moving under the action of no forces with angular velocity components (ω1,ω2,ω3)\left(\omega_{1}, \omega_{2}, \omega_{3}\right). Its motion is described by Euler's equations

I1ω˙1(I2I3)ω2ω3=0I2ω˙2(I3I1)ω3ω1=0I3ω˙3(I1I2)ω1ω2=0\begin{aligned} &I_{1} \dot{\omega}_{1}-\left(I_{2}-I_{3}\right) \omega_{2} \omega_{3}=0 \\ &I_{2} \dot{\omega}_{2}-\left(I_{3}-I_{1}\right) \omega_{3} \omega_{1}=0 \\ &I_{3} \dot{\omega}_{3}-\left(I_{1}-I_{2}\right) \omega_{1} \omega_{2}=0 \end{aligned}

Are the components of the angular momentum to be evaluated in the body frame or the space frame?

Now suppose that an asymmetric body is moving with constant angular velocity (Ω,0,0)(\Omega, 0,0). Show that this motion is stable if and only if I1I_{1} is the largest or smallest principal moment.

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