Page 340 - Automotive Engineering Powertrain Chassis System and Vehicle Body
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Tyre characteristics and vehicle handling and stability  C HAPTER 11.1

             As indicated in the figure, the complex root is char-  which expression may be readily obtained with the aid of
           acterised by the natural frequency u o of the undamped  Eqs.(11.1.46) and (11.1.47).
           system (D ¼ 0), the damping ratio z and the resulting  The parameter influence has been indicated in the
           actual natural frequency u n . Expressions for these  figure. The results correspond qualitatively well with the
           quantities in terms of the model parameters are rather  90% response times found in vehicle model simulation
           complex. However, if we take into account that in  studies. A remarkable result is that for an understeered
           normal cases jsj  l and q z k z ½ l we may simplify  automobile the response time is smaller than for an
           these expressions and find the following useful formulae:
                                                              oversteered car.
           The natural frequency of the undamped system:
                                                              Forced linear vibrations
                             2
                  K      C          h  2
              2
             u ¼     z        , 1 þ  V            (11.1.70)   The conversion of the equations of motion (11.1.46)
              o
                  M     mV         gl
                                                              into the standard state space representation is useful
           The damping ratio:                                 when the linear system properties are the subject of in-
                                                              vestigation. The system at hand is of the second order
                   D         1                                and hence possesses two state variables for which we
             z ¼       z r ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi    (11.1.71)
                 2Mu o         h  2                           choose: v and r. The system is subjected to a single input
                           1 þ  V
                               gl                             signal: the steer angle d. Various variables may be of in-
                                                              terest to analyse the vehicle’s response to steering input
           The natural frequency:                             oscillations. The following quantities are selected to il-
                                                              lustrate the method and to study the dynamic behaviour
                                  2                           of the vehicle: the lateral acceleration a y of the centre of
              2     2     2    C   h
             u ¼ u ð1   z Þz                      (11.1.72)   gravity of the vehicle, the yaw rate r and the vehicle slip
                    o
              n
                               m   gl
                                                              angle b defined at the centre of gravity. In matrix nota-
                                                              tion, the equation becomes:
             The influence of parameters has been indicated in
           Fig. 11.1-13. An arrow pointing upwards represents an  _ x ¼ Ax þ Bu                       (11.1.74)
           increase of the quantity in the same column of the   y ¼ Cx þ Du
           matrix.
             The yaw rate response to a step change in steer angle is  with
           typified by the rise time t r indicated in Fig. 11.1-14 and    !
           expressed in terms of the parameters as follows:            _ v
                                                                 _ x ¼   ;  u ¼ d;
                                                                       _ r
                                  2
                    r ss        mk V                                 0   1    0       1               (11.1.75)
             t r ¼       ¼                                             a y      _ v þ Vr
                   vr               h  2
                                                                     B
                                                                              B
                                                                         C
                           aC 1 l 1 þ  V                        y ¼ @ r A ¼ @      r  C
                                                                                      A
                   vt t¼0           gl
                             2
                          mk V                                         b         v=V
              ¼                                   (11.1.73)
                a               C 1
                      2
                   C 1 l þ b   a    mV 2                      and
                 l              C 2













           Fig. 11.1-13 The influence of parameters on natural frequency and damping.


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