In classical mechanics courses rotations of a rigid body often occupy a good deal or course work. The motion of a rigid body in space is determined by the two equations shown below:
1)
2)
Where:
and:
is the moment of inertia tensor.
Here, F is the total force on the body and N is the total torque about a suitable central point, 0. The velocity about the center of mass is v, while:
is the moment of inertia tensor and w is the angular velocity about the point 0. For an unconstrained object moving in space, 0 is taken to be the center of mass. Consider now two coordinate systems: One fixed to an object to allow calculation of I for the object, i.e.
The other (2nd system) primed for object for changes in orientation.
or: =
Since I is constant relative to the body axes. With proper choice of coordinate system we can write:
=
Þ =
I11 w1 e1^ + I22 w2 e2^ + I33 w3 e3^
And:
=
e1^ wywz (I33 - I22 ) + e2^ wxwz (I11 - I33 ) + e3^ wywx(I22 - I11 )
Where:
Nx = wywz (I33 - I22 ) I11 w1'
Ny = wywz (I11 - I33 ) I22 w2'
Nz = wywz (I11 - I33 ) I22 w2'
for the rate of change of kinetic energy:
Þ
Or:
Finally, for comparison, we examine the Euler's equations for the motion of a rigid body, assuming:
a) No torques,
b) w3 >> w2, w1 and w3 = const.
Then we obtain 2 coupled differential equations:
I1 w1' + (I3 - I2 ) w3w2 = 0
I2 w2' + (I1 - I3 )w1w3 = 0
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Next: I consider solutions for the specific differential equations for w2, w1
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