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Modelling and analysis of suspension systems 239<br />

Referring back to equation (4.329) and the free-body diagram in Figure 4.76<br />

we can see that it is convenient to sum moments of forces acting on Body 2<br />

about the mass centre G 2 to eliminate the inertial force m 2 {A 2 } 1 acting<br />

through the mass centre. In order to carry out the moment balance we will<br />

need to establish new relative position vectors {R EG2 } 1/2 , {R FG2 } 1/2 and<br />

{R GG2 } 1/2 . We will also need to define the vector components in metres for<br />

consistency. Working first in frame O 1 we have:<br />

{R EG2 } T 1 [0.115 0.155 0.005] m<br />

{R FG2 } T 1 [0.115 0.155 0.005] m<br />

{R GG2 } T 1 [0.0 0.120 0.004] m<br />

Applying a vector transformation for the vector {R EG2 } 1 from frame O 1 to<br />

O 2 gives<br />

⎡1 0 0⎤<br />

⎡ 0 1 0⎤<br />

⎡ 0.115 ⎤ ⎡0.155⎤<br />

{ R EG2 } 1 2 <br />

⎢<br />

0 0 1<br />

⎥ ⎢<br />

1 0 0<br />

⎥ ⎢<br />

0.155<br />

⎥<br />

<br />

⎢<br />

0.005<br />

⎥<br />

m<br />

⎢ ⎥ ⎢ ⎥ ⎢ ⎥ ⎢ ⎥<br />

⎣⎢<br />

0 1 0⎦⎥<br />

⎣⎢<br />

0 0 1⎦⎥<br />

⎣⎢<br />

0.005 ⎦⎥<br />

⎣⎢<br />

0.115 ⎦⎥<br />

(4.332)<br />

∑<br />

Applying the same vector transformation to {R FG2 } 1/2 and {R GG2 } 1/2 gives<br />

us the three relative position vectors, referenced to the correct frame O 2 and<br />

in consistent units, needed for the moment balance:<br />

{R EG2 } T 1/2 10 3 [155 5 115] m<br />

{R FG2 } T 1/2 10 3 [155 5 115] m<br />

{R GG2 } T 1/2 10 3 [120 4 0] m<br />

Before writing the rotational equations of motion we can first determine<br />

the moment balance of the constraint forces acting at E, F and G:<br />

{ M } { R } { F } { R } { F } { R } {<br />

F }<br />

G2 12 EG2 12 E21 12 FG2 12 F21 12 GG2 12 G24 12<br />

10<br />

3<br />

⎡ 0 115 5 ⎤ ⎡F<br />

⎢<br />

115 0 155<br />

⎥ ⎢<br />

F<br />

⎢<br />

⎥ ⎢<br />

⎣⎢<br />

5 155 0 ⎦⎥<br />

⎣⎢<br />

F<br />

E21x2<br />

E21y2<br />

E21z2<br />

⎤<br />

⎥<br />

⎥<br />

10<br />

⎦⎥<br />

3<br />

⎡ 0 115<br />

⎢<br />

115 0<br />

⎢<br />

⎣⎢<br />

5 155<br />

5 ⎤ ⎡F<br />

155<br />

⎥ ⎢<br />

⎥ ⎢<br />

F<br />

0 ⎦⎥<br />

⎣⎢<br />

F<br />

F21x2<br />

F21y2<br />

F21z2<br />

⎤<br />

⎥<br />

⎥<br />

⎦⎥<br />

10<br />

3<br />

⎡0 4 0 ⎤ ⎡F<br />

⎢<br />

4 0 120<br />

⎥ ⎢<br />

⎢<br />

⎥ ⎢<br />

F<br />

⎣⎢<br />

0 120 0 ⎦⎥<br />

⎣⎢<br />

F<br />

G24x2<br />

G24y2<br />

G24z2<br />

⎤<br />

⎥<br />

⎥<br />

Nm<br />

⎦⎥<br />

(4.333)<br />

Considering next the rotational inertial terms we have:<br />

∑ { M } [ I ] { 2} [ 2] [ I ] { 2}<br />

G2 12 2 22 12 12 2 22 12<br />

(4.334)

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