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Modelling and analysis of suspension systems 229 BUSH BUSH SPHERICAL SPHERICAL (a) REVOLUTE (b) SPHERICAL INLINE (c) Fig. 4.74 Wishbone mount modelling strategies: (a) wishbone mounted by two bushes; (b) wishbone mounted by two spherical joints; (c) wishbone mounted by a single revolute joint; (d) wishbone mounted by a spherical joint and inline joint primitive. (d) is that the wishbone initially has 6 degrees of freedom and the two spherical joints remove three each leaving for the wishbone body a local balance of zero degrees of freedom. This is clearly not valid as in the absence of friction or other forces the wishbone is not physically constrained from rotating about an axis through the two spherical joints. This is a classic MBS modelling problem where we have introduced a redundant constraint or overconstrained the model. It should also be noted that this is the root of our requirement for two more equations for the manual analysis, each equation being related to the local overconstraint of each wishbone. Early versions of MBS programs such as MSC.ADAMS were rather unforgiving in these circumstances and any attempt to solve such a model would cause the solver to fail with the appropriate error messages. More modern versions are able to identify and remove redundant constraints allowing a solution to proceed. While this undoubtedly adds to the convenience of model construction it does isolate less experienced users from the underlying theory and modelling issues we are currently discussing. In any event if the required outcome is to predict loads at the mount points the removal of the redundant constraints, although not affecting the kinematics, cannot be relied on to distribute correctly the forces to the mounts. In Figure 4.74(c) the two wishbone mount connections are represented by a single revolute joint. This is the method suggested earlier as a suitable start for predicting the suspension kinematics but will again not be useful for prediction the mount reaction forces. In this model the single revolute joint will carry the combined translational reaction forces at both mounts with additional moment reactions that would not exist in the real system. The final representation shown in Figure 4.74(d) allows a model that uses rigid constraint elements and can predict reaction forces at each mount without using the ‘as is’ approach of including the bush compliances or introducing redundant constraints. This is achieved by modelling one
230 Multibody Systems Approach to Vehicle Dynamics mount with a spherical joint and modelling the other mount with an inline joint primitive, as described earlier in Chapter 3. The inline primitive constrains 2 degrees of freedom to maintain the mount position on the axis through the two mount locations. This constraint does not prevent translation along the axis through the mounts, this ‘thrust’ being reacted by the single spherical joint. Thus this selection of rigid constraints provides us with a solution that is not overconstrained. Although the MBS approach would best utilize the model with two bushes to predict the mount reaction forces the model in Figure 4.74(d) provides us with an understanding of the overconstraint problem and a methodology we can adapt to progress the vector-based analytical solution. If we return now to the analytical solution and consider the lower wishbone Body 2, we can see in Figure 4.75 that a comparable approach to the use of the MBS inline joint primitive constraint is to ensure that the line of action of one of the mount reaction forces, say {F F21 } 1 , is perpendicular to the axis E–F through the two wishbone mounts. Thus we can derive the final two equations needed to progress the analytical solution using the familiar approach with the vector dot product to constrain the reaction force at the mount to be perpendicular to an axis through the mounts at, say, point B for the upper wishbone and point F for the lower wishbone: {F F21 } 1 • {R EF } 1 0 (4.267) {F B31 } 1 • {R AB } 1 0 (4.268) Having established the 20 equations required for solution, it is possible to set up the equations starting with the force equilibrium of Body 2: ∑{F 2 } 1 {0} 1 (4.269) {F E21 } 1 {F F21 } 1 {F G24 } 1 {0} 1 (4.270) ⎡F ⎢ ⎢ F ⎣⎢ F E21x E21y E21z ⎤ ⎡FF21x⎤ ⎡FG24x⎤ ⎡0⎤ ⎥ ⎢ F ⎥ ⎢ F21y F ⎥ ⎥ ⎢ ⎥ ⎢ G24y⎥ ⎢ 0 ⎥ N ⎢ ⎥ ⎦⎥ ⎣⎢ FF21z⎦⎥ ⎣⎢ FG24z⎦⎥ ⎣⎢ 0⎦⎥ (4.271) The summation of forces in (4.271) leads to the first set of three equations: Equation 1 F E21x F F21x F G24x 0 (4.272) {F F21 } 1 SPHERICAL INLINE F • {F E21 } 1 • E Fig. 4.75 MBS approach Analytical approach Comparable MBS and analytical wishbone mounting models
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230 Multibody Systems Approach to Vehicle Dynamics<br />
mount with a spherical joint and modelling the other mount with an inline<br />
joint primitive, as described earlier in Chapter 3. The inline primitive constrains<br />
2 degrees of freedom to maintain the mount position on the axis<br />
through the two mount locations. This constraint does not prevent translation<br />
along the axis through the mounts, this ‘thrust’ being reacted by the<br />
single spherical joint. Thus this selection of rigid constraints provides us<br />
with a solution that is not overconstrained. Although the MBS approach<br />
would best utilize the model with two bushes to predict the mount reaction<br />
forces the model in Figure 4.74(d) provides us with an understanding of the<br />
overconstraint problem and a methodology we can adapt to progress the<br />
vector-based analytical solution.<br />
If we return now to the analytical solution and consider the lower wishbone<br />
Body 2, we can see in Figure 4.75 that a comparable approach to the use of<br />
the MBS inline joint primitive constraint is to ensure that the line of action<br />
of one of the mount reaction forces, say {F F21 } 1 , is perpendicular to the<br />
axis E–F through the two wishbone mounts.<br />
Thus we can derive the final two equations needed to progress the analytical<br />
solution using the familiar approach with the vector dot product to constrain<br />
the reaction force at the mount to be perpendicular to an axis through<br />
the mounts at, say, point B for the upper wishbone and point F for the lower<br />
wishbone:<br />
{F F21 } 1 • {R EF } 1 0 (4.267)<br />
{F B31 } 1 • {R AB } 1 0 (4.268)<br />
Having established the 20 equations required for solution, it is possible to<br />
set up the equations starting with the force equilibrium of Body 2:<br />
∑{F 2 } 1 {0} 1 (4.269)<br />
{F E21 } 1 {F F21 } 1 {F G24 } 1 {0} 1 (4.270)<br />
⎡F<br />
⎢<br />
⎢<br />
F<br />
⎣⎢<br />
F<br />
E21x<br />
E21y<br />
E21z<br />
⎤ ⎡FF21x⎤<br />
⎡FG24x⎤<br />
⎡0⎤<br />
⎥ ⎢<br />
F<br />
⎥ ⎢<br />
F21y<br />
F<br />
⎥<br />
⎥<br />
<br />
⎢ ⎥<br />
<br />
⎢ G24y⎥<br />
<br />
⎢<br />
0<br />
⎥<br />
N<br />
⎢ ⎥<br />
⎦⎥<br />
⎣⎢<br />
FF21z⎦⎥<br />
⎣⎢<br />
FG24z⎦⎥<br />
⎣⎢<br />
0⎦⎥<br />
(4.271)<br />
The summation of forces in (4.271) leads to the first set of three equations:<br />
Equation 1 F E21x F F21x F G24x 0 (4.272)<br />
{F F21 } 1<br />
SPHERICAL<br />
INLINE<br />
F<br />
•<br />
{F E21 } 1<br />
•<br />
E<br />
Fig. 4.75<br />
MBS approach<br />
Analytical approach<br />
Comparable MBS and analytical wishbone mounting models