In a frame centered at the fixed point or centre of mass, a rotating material point has velocity . The identity converts the rotational kinetic energy into , where the inertia tensor is
Likewise integrating gives the angular momentum . These expressions refer to rotational motion about the chosen origin.
In principal axes, and . Substitute the Euler equations for a torque-free rigid body:
For the squared angular momentum,
Thus both and are conserved, even though the body-frame components of generally change.
Place the origin at the centre and the axes along the edges. Symmetry makes the off-diagonal entries of the inertia tensor zero. Uniform density gives , , . Consequently the principal moments of inertia are
For example gives the first expression directly.
Here , so and is the intermediate axis. Eliminating the other components from and the conservation of energy relation gives, with ,
Thus the second Euler equations for a torque-free rigid body reduces to
The sign is minus the sign of ; it is constant along a nontrivial branch. Let . Since , integration yields , with the same sign as in the scalar equation. The remaining components are
Their initial squares are fixed by the preceding algebraic formulas with ; their initial signs determine the branch. Hence as . This trajectory is an intermediate-axis separatrix: approaching intermediate-axis rotation on this special conserved-energy level does not make that rotation stable to generic perturbations. If , all components vanish identically.

Articles by others on the same topic (0)

There are currently no matching articles.