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Kinematics and dynamics of rigid bodies 65<br />

Y 2<br />

G 1 X 1<br />

Y 1<br />

G 3 X 3<br />

Y<br />

Y 3<br />

G 2 X 2<br />

G<br />

X<br />

a 2<br />

a 1 a 3<br />

Fig. 2.32<br />

Application of parallel axes theorem<br />

A practical application of the parallel axes theorem given in (2.198) is provided<br />

using the simplified representation of a tie rod as shown in Figure<br />

2.32. The body can be considered an assembly of three components with<br />

centres of mass at G 1 , G 2 and G 3 . The mass centre of the entire body is<br />

located at G. The components have masses m 1 , m 2 and m 3 and moments of<br />

inertia about the local z-axis at each mass centre I G1zz , I G2zz and I G3zz .<br />

Applying the parallel axes theorem would in this case give a moment of<br />

inertia I Gzz for the body using<br />

I Gzz I G1zz m 1 a 1 2 I G2zz m 2 a 2 2 I G3zz m 3 a 3<br />

2<br />

(2.199)<br />

2.12 Principal axes<br />

The principal axes of any rigid body are those for which the products of<br />

inertia are all zero resulting in an inertia matrix of the form<br />

[] I<br />

⎡I1<br />

0 0⎤<br />

<br />

⎢<br />

0 I2<br />

0<br />

⎥<br />

⎢ ⎥<br />

⎣⎢<br />

0 0 I3⎦⎥<br />

(2.200)<br />

where in this case I 1 , I 2 and I 3 are the principal moments of inertia. The<br />

three planes formed by the principal axes are referred to as the principal<br />

planes as shown in Figure 2.33. In this example the geometry chosen is a<br />

solid cylinder to demonstrate the concept.<br />

For the cylinder the principal axes are represented by the frame O 2 positioned<br />

at the mass centre of the body. In this case each of the principal<br />

planes is a plane of symmetry for the body. As can be seen for each element<br />

of mass with positive co-ordinates there are other elements of mass,<br />

reflected in each of the principal planes, with negative co-ordinates. The<br />

result of this is that the products of inertia are all zero.<br />

Returning to the consideration of the angular momentum of a body given in<br />

(2.178) this can now be written as shown in equation (2.201) where I 1 , I 2<br />

and I 3 are the principal moments of inertia for Body 2 taken about the origin<br />

of frame O 2. The moment of inertia matrix is referred to the principal<br />

axes, again frame O 2 and the products of inertia are zero:<br />

{H 2 } 1/2 [I 2 ] 2/2 { 2 } 1/2

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