Page 636 - Mechanical Engineers' Handbook (Volume 2)
P. 636

2 Fundamentals of Closed-Loop Performance  627

                           the closed-loop transfer function consists of a first-order and a second-order lag. The break
                           frequency of the first-order lag increases with 1oop gain, while the second-order damping
                           ratio rapidly decreases. In both loop closures, there are clearly trade-offs between closed-
                           loop bandwidth and stability.
                              There are numerous methods for quantifying the relationships between bandwidth and
                           stability. Closed-loop frequency responses to command inputs are shown for both basic forms
                           in Figs. 8 and 9, while Figs. 10 and 11 present the corresponding step responses. Useful
                           numerical measures of stability are phase margin, gain margin, and damping ratio of the
                           closed-loop complex pair. These are given in Figs. 12 and 13. Note that the gain margin for
                           Fig. 12 is infinite.
                              Referring to Fig. 6, closed-loop responses to disturbance inputs can be written as
                                                 U 1     G d   s(  s   1)                       (10)
                                                                 1
                                                               2
                                                 D   K (  /K )s   (1/K )s   1
                                                       u1  1  u1       u1
                           and
                                                              2
                                                           2
                                          U    G         s[s /    (2  /  )s   1]
                                           2     d            2     2  2                        (11)
                                                   3
                                                                      2
                                          D    K (s /K   )   (2  /K   )s   (1/K )s   1
                                                        2
                                                               2
                                                      u22
                                                                             u2
                                                u2
                                                                  u22
                              To determine the final dynamic form of these responses, it is necessary to have a transfer
                           function for G . This transfer function can be obtained from the physical model of the system,
                                      d
                           by deriving the response of the controlled variable to the disturbance input with the controller
                           output equal to zero. As an example, consider a dc motor driving an inertial load and having
                           a short electrical time constant. For an integrating velocity loop, the disturbance transfer
                           function has the form

























                                           Figure 8 Closed-loop frequency responses for U 1 /U c .
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