Page 779 - Mechanical Engineers' Handbook (Volume 2)
P. 779

770   Control System Design Using State-Space Methods

                          require the feedback of the system state x as well as the disturbance state z (Fig. 6). The

                          state estimation methods described in Section 5 can be used to generate these state estimates
                          from available measurements. The extension of this disturbance accommodation approach to
                          discrete-time systems has also been considered by Johnson. 20
                             The formulation of disturbance state models and their incorporation in controller design
                          result in controller features familiar from more classical approaches to disturbance suppres-
                          sion. Examples are integral control for constant disturbances, notch filter control for sinu-
                          soidal disturbances, and disturbance feedforward if some components of the disturbance
                          inputs are measurable. 19  Hence, the disturbance accommodation controllers described here
                          may be viewed as generalizations of classical solutions to disturbance suppression. A similar
                          comment may be made concerning the mechanism for disturbance suppression inherent in
                                                                                   21
                          the robust servomechanism structure described by Davison and Ferguson. The robust con-
                          troller structure is described later in this section.


           4.2  Tracking Applications
                          Anderson and Moore, 10  Davison and Ferguson, 21  Trankle and Bryson, 22  and Tomizuka et
                          al. 23–26  have considered extensions of the LQR formulation to accommodate tracking appli-
                          cations. Anderson and Moore 10  have considered the servomechanism problem where the
                          linear system state equations are given by Eqs. (4) and (5) in Chapter 17 with D(t)   0 and
                          the class of desired trajectories y is given by
                                                    r



































                                        Figure 6 Disturbance state model, continuous-time system.
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