Page 333 - Automotive Engineering Powertrain Chassis System and Vehicle Body
P. 333

CHAP TER 1 1. 1       Tyre characteristics and vehicle handling and stability


                                     X
                                                                          F
                                                l                          y1
                               Y            b
                                                      a                          M
                                  M                                                z1
                                    z2         -v
                                                       V                                         1
                                            2                                          F  =0
                                                                                        x2
                                                               1
                                       F x2
                                             r      u                x    F
                                                                           y2
                                  F                        M z1
                                   y2
                                                                                       F
                                              y          F y1                           x2
                                                                                                 2
               Fig. 11.1-9 Simple car model with side force characteristics for front and rear (driven) axle.

               force F x on the tyre or axle cornering force vs slip angle  The system depicted in Fig. 11.1-4 and described in
               characteristic (F y , a) may then be regarded (cf.  the preceding subsection performs a motion over a flat
               Fig. 11.1-9). The forces F y1 and F x1 and the moment  level road. Proper coordinates are the Cartesian co-
               M z1 are defined to act upon the single front wheel and  ordinates X and Yof reference point A, the yaw angle j of
               similarly we define F y2 etc. for the rear wheel.   the moving x axis with respect to the inertial X axis and
                                                                  finally the roll angle 4 about the roll axis. For motions
                                                                  near the X axis and thus small yaw angles, Eq.(11.1.25)is
               11.1.3.1 Differential equations for plane          adequate to derive the equations of motion. For cases
               vehicle motions                                    where j may attain large values, e.g. when moving along
                                                                  a circular path, it is preferred to use modified equations
               In this section, the differential equations for the three-  where the velocities u, v and r of the moving axes system
               degree-of-freedom vehicle model of Fig. 11.1-4 will be  are used as generalised motion variables in addition to the
               derived. In first instance, the fore and aft motion will also  coordinate 4. The relations between the two sets of
               be left free to vary. The resulting set of equations of  variables are (the dots referring to differentiation with
               motion may be of interest for the reader to further study  respect to time):
                                                                                  _
                                                                         _
               the vehicle’s dynamic response at somewhat higher fre-  u ¼ X cos j þ Y sin j
                                                                                   _
                                                                          _
               quencies where the roll dynamics of the vehicle body  v ¼ X sin j þ Y cos j                (11.1.26)
                                                                         _
               may become of importance. From these equations, the  r ¼ j
               equations for the simple two-degree-of-freedom model
               of Fig. 11.1-9 used in the subsequent section can be easily  The kinetic energy can be expressed in terms of u, v
               assessed. In Subsection 11.1.3.6 the equations for the car  and r. Preparation of the first terms of Eq.(11.1.25) for
               with trailer will be established. The possible instability of  the coordinates X, Y and j yields:
               the motion will be studied.                          vT    vT vu  vT vv    vT        vT
                 We will employ Lagrange’s equations to derive the     ¼       þ        ¼    cos j     sin j
                                                                                      _
                                                                     _
                                                                              _
               equations of motion. For a system with n degrees of  vX    vu vX   vv vX   vu        vv
               freedom n (generalised) coordinates q i are selected  vT  ¼  vT vu  þ  vT vv  ¼  vT  sin j þ  vT  cos j
                                                                     _
                                                                                      _
                                                                              _
               which are sufficient to completely describe the motion  vY  vu vY   vv vY   vu        vv
               while possible kinematic constraints remain satisfied.  vT  ¼  vT
               The moving system possesses kinetic energy T and     vj _  vr
               potential energy U. External generalised forces Q i asso-  vT  vT  vT
               ciated with the generalised coordinates q i may act on the  vj  ¼  vu v    vv u            (11.1.27)
               system and do work W. Internal forces acting from
               dampers to the system structure may be regarded      The yaw angle j may now be eliminated by multi-
               as external forces taking part in the total work W.  plying the final equations for X and Y successively with
               The equation of Lagrange for coordinate q i reads:  cos j and sin j and subsequently adding and subtracting
                                                                  them. The resulting equations represent the equilibrium
                 d vT   vT   vU                                   in the x and y (or u and v) directions, respectively.
                           þ     ¼ Q i                (11.1.25)
                 dt v_ q i  vq i  vq i                              We obtain the following set of modified Lagrangean
                                                                  equations for the first three variables u, v and r and

                    334
   328   329   330   331   332   333   334   335   336   337   338