Page 537 - Mechatronics with Experiments
P. 537

Printer: Yet to Come
                                                                                     October 9, 2014 8:41 254mm×178mm
            JWST499-c07
                        JWST499-Cetinkunt
                                                            ELECTROHYDRAULIC MOTION CONTROL SYSTEMS  523
                             7.8.1 Position Controlled Electrohydraulic Motion Axes
                             The controlled output, position (x), is determined by the commanded position (x cmd ) signal
                             and load force (F ). Using basic block diagram algebra, the transfer function from x cmd  and
                                           d
                             F to x can be calculated using the linear models for each component,
                               d
                                                            (         (   )       )
                                                       1               K pq
                                               X(s) =     ⋅ K ⋅ i(s) −      ⋅ F (s)            (7.313)
                                                              q
                                                                               d
                                                      A ⋅ s             A
                                                       c                 c
                                                         (
                                                      1
                                               X(s) =      K ⋅ K ⋅ (X cmd (s) − K ⋅ X(s))      (7.314)
                                                                sa
                                                            q
                                                                             fx
                                                     A ⋅ s
                                                      c
                                                           (    )      )
                                                             K pq
                                                          −       ⋅ F (s)                      (7.315)
                                                                     d
                                                              A
                                                               c
                                                                                (    )
                                                                                  K pq
                                      (A ⋅ s + K ⋅ K ⋅ K ) ⋅ X(s) = K ⋅ K ⋅ X cmd (s) −  ⋅ F (s)  (7.316)
                                        c
                                                       fx
                                                                     q
                                               sa
                                                   q
                                                                 sa
                                                                                         d
                                                                                  A c
                                                            (K ⋅ K ∕A )
                                                              sa
                                                                     c
                                                                  q
                                                 X(s) =+                   ⋅ X cmd (s)         (7.317)
                                                        s + (K ⋅ K ⋅ K ∕A )
                                                             sa
                                                                     fx
                                                                         c
                                                                 q
                                                            K ∕A 2 c
                                                             pq
                                                     −                   ⋅ F (s)               (7.318)
                                                                           d
                                                      s + (K ⋅ K ⋅ K ∕A )
                                                                   fx
                                                               q
                                                                       c
                                                           sa
                             Using the last expression for the transfer function and the final value theorem for Laplace
                             transforms, we can determine the following key characteristics of the closed loop position
                             control system.
                                  Steady-state position following error in response to a step position command and no

                                  disturbance force condition, X cmd  = X ∕s and F (s) = 0
                                                                        d
                                                                o
                                                 lim x(t) = lim s ⋅ X(s)                       (7.319)
                                                 t→∞     s→0
                                                                   (K ⋅ K ∕A )
                                                                            c
                                                                         q
                                                                     sa
                                                       = lim s ⋅                  ⋅ X ∕s       (7.320)
                                                                                    o
                                                         s→0   (s + (K ⋅ K ⋅ K ∕A )
                                                                            fx
                                                                     sa
                                                                         q
                                                                                c
                                                       = (1∕K )X o                             (7.321)
                                                             fx
                                  When a constant displacement is commanded and there is no disturbance force, the
                                  actual position will be proportional to the commanded signal by the feedback sensor
                                  gain. By scaling the commanded signal, the effective ratio between the desired and
                                  actual position can be made to be unity. In other words, the output position is exactly
                                  equal to the commanded position in steady-state when the commanded position is a
                                  constant value.
                                  What is the maximum steady-state position error in response to a ramp command

                                  signal
                                                             X cmd (s) = V ∕s 2                (7.322)
                                                                       0
                                                               F (s) = 0                       (7.323)
                                                                d
                                  The tracking error transfer function is
                                               X (s) = X cmd (s) − K X(s)                      (7.324)
                                                               fx
                                                e
                                                                 K ⋅ K ⋅ K ∕A c
                                                                      sa
                                                                          q
                                                                  fx
                                                    = X   (s) −                  ⋅ X  (s)      (7.325)
                                                       cmd                         cmd
                                                              s + (K ⋅ K ⋅ K ∕A )
                                                                   sa   q  fx  c
                                                               s              2
                                                    =                    ⋅ V ∕s                (7.326)
                                                                           o
                                                      (s + K ⋅ K ⋅ K ∕A )
                                                           fx
                                                                       c
                                                                   q
                                                               sa
   532   533   534   535   536   537   538   539   540   541   542