Page 219 - Servo Motors and Industrial Control Theory
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Appendix C                                                      217

              differences. Note that this time there are four gains to be optimized. Similar to
              the previous case, plot the eigenvalues of the system matrix and observe the
              movement of the eigenvalues as gains are changed.
            8.  This problem shows the principle procedures for selecting a DC servo motor for
              a particular application. The problem may not be with data for a realistic applica-
              tion but it shows the principle calculations that must be carried out for a real case.
              The figure below shows a case where the wing of an aircraft must be controlled
              with high position accuracy. In order to control the angle of the aircraft wing
              the motor must be located vertically as shown below. A lead screw connects
              the motor to the wing with a gearbox with input output velocity ratio of 20. The
              weight of the wing can be superimposed on the wind force.

                                                    Pivots




                                          Lead screw
                                          Gearbox


                                      Motor




              The motor must be free to rotate slightly as the angle of the wing changes. The
              nut of lead screw is connected to the wing and it is free to slide in order to be
              able to control the angular position of the wing. This system is just an imaginary
              case and may not be a practical case. The mechanical part of the system has the
              following properties,
                 Length of lead screw = 0.7 m
                 Pitch of lead screw = 2.5 mm/rev
                 Gearbox speed ratio = 20
                 The weight and wind force applied to the wing = 5000 N
                 The mass of moving parts = 200 kg
              First assume that the transmission mechanism is rigid, the torque and load inertia
              referred to the motor. From the list of DC servo motors given below select one
              noting that the motor must at least overcome the external torque and the load
              inertia must not be much greater than the rotor inertia. The motor must also pro-
              vide additional torque to accelerate the wing. The angular movement of the wing
              might be from zero to maximum of ± 180°. It is not required to move the wing
              very fast but also it must not be too slow. From this reasoning you should have
              some ideas about the maximum speed of the motor.
              Usually when you buy a DC servo motor the power unit which matches the mo-
              tor is also given by manufacturer. The motor may also be brushless to maximize
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