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58 Multibody Systems Approach to Vehicle Dynamics<br />

the reverse of sign for {V O2 } 1 . If for Body 2 frame O 2 is positioned at either<br />

the mass centre so that ∫ vol {R P } 1 dm {0} 1 , or at a point of attachment to the<br />

non-moving ground, where {V O2 } 1 {0} 1 , then (2.163) reduces to the more<br />

convenient form which we will assume from now on:<br />

(2.164)<br />

If we now take the general case for any body (ignore body subscripts) and<br />

expand the vectors into their full form we get<br />

Applying the vector cross product, making use of the skew-symmetric form<br />

of a vector in the normal manner, leads to<br />

⎡ 0 z<br />

y ⎤ ⎡ 0 z y<br />

⎤ ⎡x⎤<br />

{} R 1 {{ } 1 { R} 1}<br />

<br />

⎢<br />

z 0 x<br />

⎥ ⎢<br />

⎥<br />

z<br />

0 <br />

⎢<br />

x y<br />

⎥<br />

⎢<br />

⎥ ⎢<br />

⎥ ⎢ ⎥<br />

⎣⎢<br />

y<br />

x 0 ⎦⎥<br />

⎢<br />

y x 0 ⎥<br />

⎣<br />

⎦ ⎣⎢<br />

z⎦⎥<br />

⎡ 0 z<br />

y ⎤ ⎡zy<br />

yz⎤<br />

<br />

⎢<br />

z 0 x<br />

⎥ ⎢<br />

⎥<br />

⎢<br />

⎥ ⎢zxxz⎥<br />

⎣⎢<br />

y<br />

x 0 ⎦⎥<br />

⎢<br />

⎣<br />

yxxy⎥<br />

⎦<br />

Substituting (2.165) into (2.164) gives the general expression for the angular<br />

momentum {H} 1 of a body where for simplicity the integral sign is now<br />

taken to indicate integration over the volume of the body:<br />

{ H} { R}<br />

{{ } { R} } d m<br />

(2.166)<br />

∫<br />

∫<br />

{ H } { R } {{ } { R } } dm<br />

2 1 vol P 1 2 1 P 1<br />

⎡Hx<br />

⎤ ⎡x⎤<br />

⎡<br />

x ⎤<br />

{ H} 1 <br />

⎢<br />

H<br />

⎥<br />

y , { R} 1 <br />

⎢<br />

y<br />

⎥<br />

⎢<br />

and { }<br />

1 <br />

⎢<br />

<br />

⎥<br />

⎥ ⎢ ⎥<br />

⎢ y ⎥<br />

⎣⎢<br />

Hz<br />

⎦⎥<br />

⎣⎢<br />

z⎦⎥<br />

⎣⎢<br />

z ⎦⎥<br />

1 1 1 1<br />

⎡y( xyyx) z( zxxz)<br />

⎤<br />

⎢<br />

⎥<br />

⎢z( yzzy) x( xyyx)<br />

⎥<br />

⎢<br />

⎣<br />

x( zxxz) y( yzzy)<br />

⎥<br />

⎦<br />

(2.165)<br />

2<br />

Hx x ∫ ( y z 2 ) d my ∫ xyd mz<br />

∫ xzdm<br />

∫<br />

2<br />

y x y 2 ) z<br />

∫<br />

H xyd m ( x z d m<br />

yzdm<br />

∫<br />

(2.167)<br />

(2.168)<br />

H xzd m yzd m ( x y dm<br />

z x y z<br />

(2.169)<br />

It is now possible to substitute into (2.167) to (2.169) the following general<br />

terms for the moments of inertia I xx , I yy and I zz of the rigid body:<br />

∫<br />

2 2 )<br />

Ixx ( y z d m<br />

∫<br />

∫<br />

∫<br />

2 2 )<br />

(2.170)<br />

∫<br />

2 2 )<br />

Iyy ( x z d m<br />

(2.171)

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