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Modelling and assembly of the full vehicle   C HAPTER 15.1


            Table 15.1-3 MSC.ADAMS statements for lane change steering inputs

























             In a similar manner if we wanted to apply a sinusoidal  embedded step functions with some planning and care
           steering input with an amplitude of 30 degrees and  over syntax. Note that for a fixedsteering input a change in
           a frequency of 0.5 Hz we could use:                vehicle configuration will produce a change in response so
                                                              that the vehicle fails to follow a path.
             FUNCTION ¼ 30D * SINðTIME * 180DÞ                  For a closed loop steering manoeuvre a torque is applied
                                                              to the steering column, or a force to the steering rack if the
             For the lane change manoeuvre described earlier the  column is not modelled, that will vary during the simula-
           measured steering wheel angles from a test vehicle can be  tion so as to maintainthe vehicleon a predefined path. This
           extracted and input as a set of XY pairs, which can  requires a steering controller to process feedback of the
           be interpolated using a cubic spline fit. A time history  observeddeviationfromthepath(error)andtomodifythe
           plot for the steering inputs is shown in Fig. 15.1-42 for  torque accordingly as illustrated in Fig. 15.1-43.
           lane change manoeuvres at 70 and 100 km/h.
             By way of example the MSC.ADAMS statements
           which apply the steering motion to the steering column to  15.1.13 Driver behaviour
           body revolute joint and the spline data are shown in Table
           15.1-3 for a 100 km/h lane change. The x values are points  It becomes inevitable with any form of vehicle dynamics
           in time and the y values are the steering inputs in degrees.  modelling that the interaction of the operator with
           In the absence of measured data it is possible to construct  the vehicle is a source of both input and disturbance. In
           an open loop single or double lane change manoeuvre using  flight dynamics, the phenomenon of ‘PIO’ – pilot in-
           a combination of nested arithmetic IF functions with  duced oscillation – is widely known. This occurs when


                                   Torque applied to
                                   handwheel



                                                                                   Error










                                                         T   Fn (error)

           Fig. 15.1-43 Principle of a closed loop steering controller.


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