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Kinematics and dynamics of rigid bodies 59<br />

∫<br />

2 2 )<br />

Izz ( x y d m<br />

In addition we can introduce the products of inertia I xy , I yz and I xz :<br />

(2.172)<br />

Ixy Iyx ∫ xy dm<br />

Iyz Izy ∫ yz d m<br />

Ixz Izx ∫ xz d m<br />

(2.173)<br />

(2.174)<br />

(2.175)<br />

This allows (2.167) to (2.169) to be arranged in matrix form as follows:<br />

⎡Hx<br />

⎤ ⎡Ixx Ixy Ixz<br />

⎤ ⎡<br />

x ⎤<br />

⎢<br />

H<br />

⎥ ⎢<br />

⎥<br />

(2.176)<br />

⎢ y ⎥<br />

I I I<br />

⎢<br />

⎢ xy yy yz ⎥ ⎢<br />

<br />

⎥<br />

y ⎥<br />

⎣⎢<br />

Hz<br />

⎦⎥<br />

⎢I I I ⎥<br />

⎣ xz yz zz ⎦ ⎣⎢<br />

z ⎦⎥<br />

If we return to our earlier consideration of Body 2 shown in Figure 2.27 the<br />

matrix equation in (2.176) would lead to<br />

{H 2 } 1/1 [I 2 ] 2/1 { 2 } 1/1 (2.177)<br />

In writing the vectors {H 2 } 1/1 { 2 } 1/1 we revert to the full definition of a<br />

vector used here where the upper suffix indicates that the vector is measured<br />

relative to the axes of reference frame O 1 and the lower suffix indicates<br />

that the components of the vector are resolved parallel to the axes of<br />

frame O 1 . The matrix [I 2 ] 2/1 is the moment of inertia matrix for Body 2<br />

about its mass centre G 2 located at frame O 2 . The use of the upper and<br />

lower suffix here indicates that the moments of inertia have been measured<br />

relative to frame O 2 but transformed to frame O 1 . This is necessary so that<br />

the vector operation in (2.177) is consistent. This is only possible if the<br />

vectors and matrix are referred to the same frame, which in this case is O 1 .<br />

Note that in this form (2.177) is not practical since the orientation of frame<br />

O 2 relative to frame O 1 will change as the body rotates requiring the recomputation<br />

of [I 2 ] 2/1 at each time step. The matrix [I 2 ] 2/2, or in simpler form<br />

[I 2 ] 2 , is constant since it is measured relative to and referred to a frame that<br />

is fixed in Body 2 and hence only needs to be determined once for an undeformable<br />

body. When considering the equation for the angular momentum<br />

of a body it is preferable therefore to consider all quantities to be referred<br />

to a frame fixed in the body, in this case frame O 2 :<br />

{H 2 } 1/2 [I 2 ] 2/2 { 2 } 1/2 (2.178)<br />

Before progressing to develop the equations used to describe the dynamics of<br />

rigid bodies translating and rotating in three-dimensional space the definition<br />

of the moments of inertia introduced here requires further consideration.<br />

2.10 Moments of inertia<br />

From our previous consideration of the angular momentum of a rigid body<br />

we see that there are three moments of inertia and three products of inertia

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