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0066_Frame_C30  Page 33  Thursday, January 10, 2002  4:44 PM























                       FIGURE 30.8  Two degree-of-freedom PUMA 560 robotic
                       manipulator.

                       where


                                                  0.0000   0.0000   1.0000 0.0000
                                           A p =  0.0000   0.0000   0.0000 1.0000              (30.201)
                                                  31.7613  – 33.0086 0.0000 0.0000
                                                 – 56.9381 187.7089 0.0000 0.0000

                                                        0.0000      0.0000
                                                        0.0000      0.0000
                                                 B p =                                         (30.202)
                                                       1037.7259  – 3919.6674
                                                      – 3919.6674  2030.8306
                                                      C p =  [ I 2 × 2 0 2 × ]                 (30.203)
                                                                    2
                       The system poles are s = ±14.1050, s = ±4.5299. Eigenvector analysis shows that the fast instability at s =
                       14.1050 is primarily associated with the upper (shorter) link, while the slower instability at s = 4.5299 is
                       primarily associated with the lower (longer) link. The system does not possess any natural integrators
                       (i.e., no zero eigenvalues) and, as expected, the singular values σ i [P(jω)] are flat at low frequencies (see
                       Fig. 30.9).
                       Closed Loop Objectives
                       A controller to be implemented within a negative feedback loop is sought. The closed loop system should
                       exhibit the following properties: (1) closed loop stability, (2) zero steady state error to step reference com-
                       mands, (3) good low frequency reference command following (step commands followed with little
                       overshoot within 3 s), (4) good low frequency disturbance attenuation, (5) good high frequency noise
                       attenuation, (6) good stability robustness margins at the plant output.
                         Each step of the control system design process is now described. A central idea is the formation of a
                                                                                                     2
                       so-called design plant P d  from the original plant P. The design plant P d  is what is submitted to our H -
                       LQG/LTR design machinery.
                       Step 1: Augment Plant P with Integrators to Get Design Plant Pd == == [A, B, C]
                       In order to guarantee zero steady-state error to step reference commands, we begin by augmenting the
                       plant P = [A p , B p , C p ] with integrators—one in each control channel—to form the design plant P d  = [A,
                       B, C]; i.e., P d  = P(I 2×2 /s). This is done as follows:


                                                       A =  0 2×2 0 2×4                        (30.204)
                                                             B p  A p


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