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Hard Disk Drive Servo Systems- P7
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Tham khảo tài liệu hard disk drive servo systems- p7, công nghệ thông tin, phần cứng phục vụ nhu cầu học tập, nghiên cứu và làm việc hiệu quả
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Hard Disk Drive Servo Systems- P711A Benchmark ProblemBefore ending this book, we post in this chapter a typical HDD servo control designproblem. The problem has been tackled in the previous chapters using several designmethods, such as PID, RPT, CNF, PTOS and MSC control. We feel that it can serve asan interesting and excellent benchmark example for testing other linear and nonlinearcontrol techniques. We recall that the complete dynamics model of a Maxtor (Model 51536U3) harddrive VCM actuator can be depicted as in Figure 11.1: Nominal plant Resonance modes Noise Figure 11.1. Block diagram of the dynamical model of the hard drive VCM actuatorThe nominal plant of the HDD VCM actuator is characterized by the followingsecond-order system: sat (11.1)and (11.2)where the control input is limited within V and is an unknown input dis-turbance with mV. For simplicity and for simulation purpose, we assumethat the unknown disturbance mV. The measurement output available for292 11 A Benchmark Problemcontrol, i.e. (in l um), is the measured displacement of the VCM R/W head and isgiven by Noise (11.3)where the transfer functions of the resonance modes are given by (11.4)with represents the variation of the resonance modes of the actualactuators whose resonant dynamics change from time to time and also from diskto disk in a batch of million drives. Note that many new hard drives in the marketnowadays might have resonance modes at much higher frequencies (such as thosefor the IBM microdrives studied in Chapter 9). But, structurewise, they are almostthe same. The output disturbance (in lum), which is mainly the repeatable runouts, isgiven by (11.5)and the measurement noise is assumed to be a zero-mean Gaussian white noise witha variance (um) . l The problem is to design a controller such that when it is applied to the VCMactuator system, the resulting closed-loop system is asymptotically stable and theactual displacement of the actuator, i.e. , tracks a reference um. The overall ldesign has to meet the following specifications: 1. the overshoot of the actual actuator output is less than 5%; 2. the mean of the steady-state error is zero; 3. the gain margin and phase margin of the overall design are, respectively ,greater than 6 dB and ; and 4. the maximum peaks of the sensitivity and complementary sensitivity functions are less than 6 dB. The results of Chapter 6 show that the 5% settling times of our design using theCNF control technique are, respectively, 0.80 ms in simulation and 0.85 ms in actualhardware implementation. We note that the simulation result can be further improvedif we do not consider actual hardware constraints in our design. For example, the 11 A Benchmark Problem 293CNF control law given below meets all design specifications and achieves a 5%settling time of 0.68 ms. It is obtained by using the toolkit of [55] under the optionof the pole-placement method with a damping ratio of and a natural frequency of2800 rad/sec together with a diagonal matrix diag . Thedynamic equation of the control law is given by sat (11.6) (11.7)where (11.8)and (11.9)with being given as in Equation 6.9. The simulation results obtained with given in Figures 11.2 to 11.4 showthat all the design specifications have been achieved. In particular, the resulting 5%settling time is 0.68 ms, the gain margin is 7.85 dB and the phase margin is 44.7 ,and finally, the maximum values of the sensitivity and complementary sensitivityfunctions are less than 5 dB. The overall control system can still produce a satisfac-tory result and satisfy all the design specifications by varying the resonance modeswith the value of changing from to . Nonetheless, we invite interested readers to challenge our design. Noting thatfor the track-following case, i.e. when um, the control signal is far below its lsaturation level. Because of the bandwidth constraint of the overall system, it is notpossible (and not necessary) to utilize the full scale of the control input to the actuatorin the track-following stage. However, in the track-seeking case or equivalently bysetting a larger target reference, say um, the very problem can serve as a lgood testbed for control techniques developed for systems with actuator saturation.Interested readers are referred to Chapter 7 for more information on track seeking ofHDD servo systems.294 11 A Benchmark Problem ...
Nội dung trích xuất từ tài liệu:
Hard Disk Drive Servo Systems- P711A Benchmark ProblemBefore ending this book, we post in this chapter a typical HDD servo control designproblem. The problem has been tackled in the previous chapters using several designmethods, such as PID, RPT, CNF, PTOS and MSC control. We feel that it can serve asan interesting and excellent benchmark example for testing other linear and nonlinearcontrol techniques. We recall that the complete dynamics model of a Maxtor (Model 51536U3) harddrive VCM actuator can be depicted as in Figure 11.1: Nominal plant Resonance modes Noise Figure 11.1. Block diagram of the dynamical model of the hard drive VCM actuatorThe nominal plant of the HDD VCM actuator is characterized by the followingsecond-order system: sat (11.1)and (11.2)where the control input is limited within V and is an unknown input dis-turbance with mV. For simplicity and for simulation purpose, we assumethat the unknown disturbance mV. The measurement output available for292 11 A Benchmark Problemcontrol, i.e. (in l um), is the measured displacement of the VCM R/W head and isgiven by Noise (11.3)where the transfer functions of the resonance modes are given by (11.4)with represents the variation of the resonance modes of the actualactuators whose resonant dynamics change from time to time and also from diskto disk in a batch of million drives. Note that many new hard drives in the marketnowadays might have resonance modes at much higher frequencies (such as thosefor the IBM microdrives studied in Chapter 9). But, structurewise, they are almostthe same. The output disturbance (in lum), which is mainly the repeatable runouts, isgiven by (11.5)and the measurement noise is assumed to be a zero-mean Gaussian white noise witha variance (um) . l The problem is to design a controller such that when it is applied to the VCMactuator system, the resulting closed-loop system is asymptotically stable and theactual displacement of the actuator, i.e. , tracks a reference um. The overall ldesign has to meet the following specifications: 1. the overshoot of the actual actuator output is less than 5%; 2. the mean of the steady-state error is zero; 3. the gain margin and phase margin of the overall design are, respectively ,greater than 6 dB and ; and 4. the maximum peaks of the sensitivity and complementary sensitivity functions are less than 6 dB. The results of Chapter 6 show that the 5% settling times of our design using theCNF control technique are, respectively, 0.80 ms in simulation and 0.85 ms in actualhardware implementation. We note that the simulation result can be further improvedif we do not consider actual hardware constraints in our design. For example, the 11 A Benchmark Problem 293CNF control law given below meets all design specifications and achieves a 5%settling time of 0.68 ms. It is obtained by using the toolkit of [55] under the optionof the pole-placement method with a damping ratio of and a natural frequency of2800 rad/sec together with a diagonal matrix diag . Thedynamic equation of the control law is given by sat (11.6) (11.7)where (11.8)and (11.9)with being given as in Equation 6.9. The simulation results obtained with given in Figures 11.2 to 11.4 showthat all the design specifications have been achieved. In particular, the resulting 5%settling time is 0.68 ms, the gain margin is 7.85 dB and the phase margin is 44.7 ,and finally, the maximum values of the sensitivity and complementary sensitivityfunctions are less than 5 dB. The overall control system can still produce a satisfac-tory result and satisfy all the design specifications by varying the resonance modeswith the value of changing from to . Nonetheless, we invite interested readers to challenge our design. Noting thatfor the track-following case, i.e. when um, the control signal is far below its lsaturation level. Because of the bandwidth constraint of the overall system, it is notpossible (and not necessary) to utilize the full scale of the control input to the actuatorin the track-following stage. However, in the track-seeking case or equivalently bysetting a larger target reference, say um, the very problem can serve as a lgood testbed for control techniques developed for systems with actuator saturation.Interested readers are referred to Chapter 7 for more information on track seeking ofHDD servo systems.294 11 A Benchmark Problem ...
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