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88 Mutibody Systems Approach to Vehicle Dynamics<br />

In summary there are now a set of kinematic position and velocity variables<br />

for the nth part with components measured in the GRF and also a set of orientation<br />

and angular velocity variables measured about the Euler-axis frame:<br />

{Rn} 1 [Rnx Rny Rnz] T (3.7)<br />

{Vn} 1 [Vnx Vny Vnz] T (3.8)<br />

{n} e [n n n] T (3.9)<br />

{n} e [nn n] T (3.10)<br />

There is also a set of kinematic equations associated with the part which<br />

may be simply stated as:<br />

d<br />

{ Vn} 1 { Rn}<br />

1<br />

dt<br />

(3.11)<br />

d<br />

{ n} e { n}<br />

e<br />

(3.12)<br />

dt<br />

The remaining part variables and equations are those obtained by considering<br />

the equations of motion for a rigid body. Each part can be considered to<br />

have a set of six generalized co-ordinates given by<br />

q j [Rnx, Rny, Rnz, n, n, n] (3.13)<br />

The translational co-ordinates are the translation of the centre of mass<br />

measured parallel to the axes of the ground reference frame while the rotational<br />

co-ordinates are provided by the Euler angles for that part. For any<br />

part the translational forces are therefore summed in the X, Y and Z directions<br />

of the GRF while the summation of moments takes place at the centre<br />

of mass and about each of the axes of the Euler-axis frame. Using a form of<br />

the Lagrange equations this can be shown as:<br />

d<br />

dt<br />

⎛ ∂T<br />

⎞ ∂T<br />

⎜<br />

Qj<br />

⎝ ∂q<br />

⎟ <br />

˙<br />

j⎠<br />

∂q<br />

j<br />

n<br />

∑<br />

i1<br />

∂i<br />

i 0<br />

∂q<br />

j<br />

(3.14)<br />

The kinetic energy T is expressed in terms of the generalized co-ordinates<br />

q j and is given by<br />

1 T 1 T T<br />

T { Vn} 1m{ Vn} 1 { n} e [ B] [ In][ B]{ n}<br />

e<br />

(3.15)<br />

2<br />

2<br />

The mass properties are specified by m which is the mass of the part and<br />

[I n ] which is the mass moment of inertia tensor for the part and given by<br />

⎡Ixx Ixy Ixz<br />

⎤<br />

⎢<br />

⎥<br />

[ In]<br />

⎢Iyx Iyy Iyz<br />

⎥<br />

(3.16)<br />

⎢I I I ⎥<br />

⎣ zx zy zz ⎦<br />

The terms and represent the reaction force components acting in the<br />

direction of the generalized co-ordinate q j . The term Q j represents the sum<br />

of the applied force components acting on the part and in the direction of the<br />

generalized co-ordinate q j . The equation can be simplified by introducing

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