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192 Multibody Systems Approach to Vehicle Dynamics<br />

EIG0000003 Mode 1 Frequency 1.1943 (Hz)<br />

EIG0000003 Mode 2 Frequency 11.1645 (Hz)<br />

Fig. 4.57 MSC.ADAMS prediction of the modes of vibration of the simplified<br />

quarter vehicle model<br />

An MSC.ADAMS model consisting exactly of the model as sketched<br />

above can be used to calculate undamped linear modes in a more exact<br />

fashion, giving two modes of vibration as might be expected but slightly<br />

differing numerical results.<br />

The modal solution uses the ADAMS/Linear product, which in turn uses<br />

numerical perturbation methods to estimate mass and stiffness matrices<br />

about an operating point before solving for eigenvalues in the normal fashion.<br />

For purely mechanical systems such as the one modelled it can be<br />

relied upon to give good quality results. However, for systems where forces<br />

are time dependent and are modelled in specific ways (e.g. as differential<br />

equations for modelling turbocharger behaviour as described in Chapter 6,<br />

or tyre relaxation length modelling) then the results are not necessarily<br />

reliable at the time of writing and must be examined on an individual basis<br />

before confidence is placed in them. MSC.ADAMS and other software<br />

packages are subject to ongoing modification and development and so<br />

functionality of this nature should be evaluated periodically; such evaluations<br />

should be part of the software commissioning process within individual<br />

organizations, particularly if critical decisions are to be based on<br />

software output.<br />

The estimates given above are a simplification of the real analytical solution<br />

to the system. Such a solution is obtained using the equations of<br />

motion taking x b and x t in this example to represent the vertical displacements<br />

of the body and tyre respectively. The equations are written by<br />

inspection thus:<br />

mx˙˙ k( x) k ( x x)<br />

(4.72)<br />

t t t t b b t<br />

mx˙˙ k( xx)<br />

b b b t b<br />

These can be arranged more conveniently as:<br />

mx˙˙ x( k k ) x ( k )<br />

t t t t b b b<br />

mx˙˙ x( k) x(<br />

k)<br />

b b t b b b<br />

(4.73)<br />

(4.74)<br />

(4.75)

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