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Multibody systems simulation software 95<br />

Table 3.1<br />

Basic constraint element equations<br />

Constraint Full equation Abbreviated form<br />

Atpoint { a } 1 ({R i } 1 {r I } 1 ) ({R j } 1 {r J } 1 ) {d IJ } 1<br />

Inplane d [({R i } 1 {r I } 1 ) ({R j } 1 {r J } 1 )] • {a J } 1 {d IJ } 1 • {a J } 1<br />

Perpendicular p {a I } 1 • {a J } 1 {a I } 1 • {a J } 1<br />

Angular arctan ({x i } 1 • {y j } 1 /{x i } 1 • {x j } 1 ) IJ<br />

Table 3.2<br />

Force contributions for basic constraint elements<br />

Constraint Part i force Part j force<br />

Atpoint {} {}<br />

Inplane [A 1j ]{a J } j d [A 1j ]{a J } j d<br />

Perpendicular 0 0<br />

Angular 0 0<br />

Table 3.3<br />

Moment contributions for basic constraint elements<br />

Constraint Part i moment Part j moment<br />

Atpoint [B i ] T {r I } i [A i1 ] [B j ] T {r J } i [A j1 ]<br />

Inplane [B i ] T {r I } i [A ij ]{a J } j d [B j ] T {a J } j [A j1 ]({R i } 1 [A 1i ]{r I } i {R j } 1 ) d<br />

Perpendicular [B i ] T {a I } i [A ij ]{a J } j p [B j ] T {a J } j [A ji ]{a I } i p<br />

Angular [B i ] T {z i } i [B j ] T {z j } j <br />

In applying this constraint it is assumed that other system constraints will<br />

maintain the z-axes of the two parts to remain parallel as shown in Figure 3.16.<br />

The moment acting on part i is given by {z i } 1 and on part j by {z j } 1 .<br />

Transforming into the Euler axis system for each part gives a moment in<br />

the co-ordinate system for part i equal to [B i ] T {z i } i and on part j by<br />

[B j ] T {z j } j .<br />

The equations associated with each of the four basic constraint elements<br />

are summarized in Table 3.1.<br />

The force and moment contributions to each part in the generalized<br />

co-ordinates are summarized in Table 3.2 and Table 3.3.<br />

3.2.7 Standard joints<br />

As stated there are a number of mechanical type joints that may be used to<br />

constrain the motion of bodies. Examples of some of the most commonly<br />

used joints are shown in Figure 3.17.<br />

Of the joints shown in Figure 3.17 the spherical, revolute, translational,<br />

cylindrical and universal will figure most prominently in this text, particularly<br />

with regard to the modelling of suspension systems. The concept of an<br />

I marker on one part connecting to a J marker on another part is used again<br />

for joint elements. An example of the syntax used to define a joint in<br />

MSC.ADAMS is shown below:<br />

JOINT/02,I0602,J0902,SPH

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