Page 646 - Mechanical Engineers' Handbook (Volume 2)
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3 Frequency Compensation to Improve Overall Performance  637
































                                               Figure 15 Second-order lead compensation.


            3.2  Poorly Damped Systems
                           Section 3.1 discussed the benefits of lead compensation whose zeros are identical to the
                           dominant forward-loop poles of the system. Theoretically, this technique can be used for
                           any forward-loop transfer function. However, when the dominant forward-loop poles are
                           second order and poorly damped, practical considerations render the technique highly risky
                           in many cases. The basic problem is that the amplitude and phase of a poorly damped pair
                           of poles change very rapidly with frequency in the vicinity of the resonant peak. If the
                           compensator zeros are not precisely matched to the poles, the combined forward-loop transfer
                           function can easily exhibit 180  of phase lag in the vicinity of substantial local peaking.
                              To illustrate the potential stability problem, consider the system of Fig. 6b, with
                                                                                                2
                           0.10. Suppose that the lead compensator of Eq. (7) is added with       ,     0.10,   cp
                                                                                cz
                                                                                     2
                                                                                        cz
                             3  , and   cp    0.80. Theoretically, the forward loop is now dominated by the integrator
                               cz
                           and the compensator poles. Referring to Fig. 9d, it can be seen that a well-behaved response
                           can be obtained with a loop gain K u2    1.2  . However, suppose that   shifts to a lower
                                                               cz
                                                                                     2
                           value. For example, with an electrohydraulic servoactuator driving an inertial load, the ‘‘hy-
                           draulic resonance’’ can change 50% or more over the stroke range of the cylinder. Figure
                           16 shows how the closed-loop roots and the open-loop frequency response change with
                           variations in   .
                                      2
                              Note that a reduction of   to 0.89  will cause the closed-loop system to become
                                                    2
                                                             cz
                           unstable (0 dB at  180  phase). Even if the natural frequency of the forward-loop poles
                           does not change at all, the poles remain poorly damped in the closed-loop transfer function.
                           Although they are masked by the compensator zeros with regard to command inputs, they
                           may be excited by disturbance inputs to the system. The same general comments apply to
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