- About this Journal ·
- Abstracting and Indexing ·
- Advance Access ·
- Aims and Scope ·
- Annual Issues ·
- Article Processing Charges ·
- Articles in Press ·
- Author Guidelines ·
- Bibliographic Information ·
- Citations to this Journal ·
- Contact Information ·
- Editorial Board ·
- Editorial Workflow ·
- Free eTOC Alerts ·
- Publication Ethics ·
- Reviewers Acknowledgment ·
- Submit a Manuscript ·
- Subscription Information ·
- Table of Contents

Smart Materials Research

Volume 2012 (2012), Article ID 920747, 7 pages

http://dx.doi.org/10.1155/2012/920747

## Active Vibration Control of a Microactuator for the Hard Disk Drive Using Self-Sensing Actuation

^{1}Department of Human and Information Systems Engineering, Gifu University, 1-1 Yanagido, Gifu 501-1193, Japan^{2}Department of Mechanical and Systems Engineering, Gifu University, 1-1 Yanagido, Gifu 501-1193, Japan^{3}Department of Machines and Metals, Nagoya Municipal Industrial Research Institute, 3-4-41 Rokuban, Atsuta, Nagoya 456-0058, Japan

Received 18 November 2011; Accepted 15 January 2012

Academic Editor: Tao Li

Copyright © 2012 Minoru Sasaki et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

#### Abstract

This paper presents the self-sensing control of a microactuator for hard disk drives. The microactuator uses a PZT actuator pair installed on the suspension assembly. The self-sensing microactuator forms a combined sensing and actuation mechanism. Direct velocity feedback and positive position feedback are used in this paper. Our experimental results show that both strategies are effective in suppressing vibrational modes and successfully demonstrate the feasibility of using a self-sensing actuator on an HDD suspension assembly.

#### 1. Introduction

A suspension assembly in a hard disk drive (HDD) is subject to excitation by many disturbances, including the airflow due to the rapidly spinning disks, and noncircular track motion of the head and slider due to resonance in the components. A servo system that can cope with these problems requires a very high servo bandwidth and position error signal sampling frequency. In conventional servo systems, the sampling frequency is limited by data storage efficiency. The desire to more effectively suppress the effect of disturbances has led many researchers to propose the addition of more sensors and actuators. One example which has been proposed is to use a piezoelectric actuator on the suspension in a dual-stage system with one of the two strips as the sensor and the other as the actuator [1, 2]. This, however, reduces the effectiveness of the actuator by half and is not efficient. An alternate approach is to use it as a self-sensing microactuator [3–9], which is the subject of this paper. For dual-stage servo system, the performance of self-sensing actuator systems exceeds that of other vibration compensation systems.

We implemented two active strategies in order to experimentally demonstrate the effectiveness of a self-sensing system in structural vibration control. The strategies are direct velocity feedback (DVF) and positive position feedback (PPF). DVF, also known as strain rate feedback (SRF) has been used in the active damping of a flexible space structure [10]. In DVF, the structural velocity coordinate is fed back to the compensator and the compensator velocity coordinate multiplied by a negative gain is applied to the structure. DVF has a wide active damping region and can stabilize more than one mode given sufficient bandwidth. In PPF, the structural position coordinate is fed directly to the compensator where a scalar gain is applied and the result sent to the structure [11, 12]. PPF offers quick damping for a particular mode provided the modal characteristics are known. PPF is also easy to implement. Song and Agrawal experimentally demonstrated that it is robust against a varying modal frequency [13]. Pang et al. [14] used the self-sensing technique for active-mode damping in the dual-stage servo system. Chan and Liao [15] used self-tuning adaptive compensation with the self-sensing actuation. We try to demonstrate two active vibration control methods using two types of the sensing signal. This paper is very different from previous publications.

In this paper, we demonstrate the use of these control methods with self-sensing actuators to actively damp vibrations in an HDD suspension assembly. Experimental results have shown that PPF and DVF control methods are effective in actively increasing damping in an HDD suspension assembly using self-sensing PZT actuators.

#### 2. Microactuator for HDD

Figure 1 shows a suspension assembly from a dual-stage HDD servo. A suspension based microactuator uses a PZT actuator pair located between the suspension and the base plate. A slider is installed at the tip of the suspension. When a control voltage is applied to the PZT pair, one of them expands while the other contracts in the direction. As a result, the slider moves in the direction. The PZT actuator achieves large displacements of the head element by using the length of the suspension as a radius arm. However, the resonance frequency of the suspension limits the servo bandwidth. The configuration of the assembly seems to make it amenable to control using self-sensing actuation. We investigate this in the following sections.

#### 3. Self-Sensing Actuation

A piezoelectric self-sensing actuator is a piezoelectric transducer used simultaneously as a sensor and an actuator. The key is capacitance. If the capacitance of a piezoelectric device is known [4], applying the same voltage to a capacitor of the same value and subtracting its electrical response from that of the piezoelectric yields the signal due to the piezoelectric’s mechanical response. A bridge circuit using additional resisters and a capacitor is used to obtain the time rate of change of strain (velocity).

A CR bridge circuit is shown in Figure 2. The difference between the output voltages and gives the sensor voltage . In terms of the Laplace transform, we have

If the values of the components are adjusted, so that

The first term is vanishes, giving us the Laplace transform of the sensor voltage in terms of the transform of the piezoelectric voltage as seen in (3): Taking the inverse Laplace transform gives the time domain equation (4): where the dot indicates the time derivative and is the frequency of the input voltage, and the value of and have been chosen to satisfy (4). The charge developed on the sensor can be found from Thus, a distributed piezoelectric sensor with a rate of strain sensing bridge can measure the total angular deflection velocity of the piezoelectric beam at a point . The constant is determined by the size and material of the piezoelectric elements [3–9]. Taking account of the bridge circuit, applied input voltage of the microactuator is

The CC bridge circuit corresponding to the self-sensing actuator is shown in Figure 3. An analogous development starts with (7): Using the simplifying component values in (8) gives an expression for the Laplace transform of sensor voltage . Taking the inverse Laplace transform and limiting ourselves to lower frequencies leads to an equation for the input voltage of the actuator (12). when . The charge developed on the sensor can be found from Thus a distributed piezoelectric sensor with a strain sensing bridge can measure the total angular deflection of the piezoelectric beam at a point [3–9]. Taking account of the bridge circuit, applied input voltage of the microactuator is

#### 4. Experimental Setup

Figure 4 shows the setup for our experiments. The experiments were carried out on a spin test stand. An input control voltage is calculated by a DSP every 0.01 millisecond and applied to the bridge circuit through a D/A converter and a piezo driver. Sensor voltage from the bridge circuit is passed through a differential amplifier and A/D converter to the input of the DSP. For monitoring purpose only, a laser doppler vibrometer (LDV) was used to obtain measurements of tip displacement and velocity.

Figure 5 shows the measured frequency response of the slider tip displacement to an applied control voltage with and without the spinning disk. Figure 6 shows the frequency response of the strain rate sensor. Figure 7 shows the frequency response of strain sensor. In these figures, the red line indicates the response with the spinning disk while the blue line is without the spinning disk. There are four major vibration modes of the suspension assembly while on the spinning disk. There are three suspension bending modes: B1 at 2.7 kHz; B2 at 5.4 kHz, B3 at 9.8 kHz. The fourth major mode is a sway mode: S at 9.2 kHz. The suspension bending modes are vibrations in the vertical direction. The sway mode is the PZT microactuator actuation mode and is a vibration in the horizontal direction. With the disk rotating, the third suspension mode (B3) combines with the sway mode (S). When the experiment is done with a rotating magnetic disk, the suspension modes disappear and the sway mode appears alone as shown in Figure 5.

Corresponding results are shown in Figures 6 and 7, where on the spinning disk, only the sway mode is observed. In these figures, the signals are similar to a velocity signal and a position signal.

#### 5. Direct Velocity Feedback Control

Estimating the modal states of a distributed structure in order to apply modal feedback control is difficult. The problem of observation spillover is potentially more serious than the problem of control spillover as it can lead to instability. Hence, a method not requiring modal state estimation is desired. One such method is direct output feedback control where the sensors are collocated with the actuators and a given actuator force is a function of the sensor output at the same point. The self-sensing piezo actuator is a perfect candidate for this control method. DVF is a form of this control method and it stabilizes all vibrational modes.

Figure 8 shows a block diagram of the DVF control system. The microactuator, controlled with collocated velocity feedback giving the strain rate, is unconditionally stable at all frequencies [4]. With the feedback gain at , the transfer function for the phase lead compensator is

We implemented real-time DVF on the suspension assembly. Figure 8 shows the actuator input voltage. The input voltage of the actuator is rectangular wave at 5 V in 500 Hz. The DVF controlled time response is compared to the vibrations of the uncontrolled system (Figure 9). Under control, suspension assembly vibrations taper off within 0.2 milli seconds of the input signal becoming constant. This is shown in Figure 10. A 20 dB drop in the energy of the sway mode accompanied the damping of the vibrations, as shown in Figures 11 and 12.

#### 6. Positive Position Feedback Control

Positive position feedback (PPF) control was first proposed by Goh and Caughey for collocated sensors and actuators. Fanson and Caughey later demonstrated PPF control in space structures. PPF control is done by feeding the structural coordinate directly to compensator where a positive gain is applied before the signal is sent back to the structure. PPF offers quick damping of a particular mode provided the modal characteristics are known. The scalar equation governing a single mode of the vibration of a structure and the PPF controller is where the natural frequency and the damping ratio of the compensator are , respectively. The frequency [kHz] is slightly lower than the target frequency [12]. A block diagram of the PPF control system appears in Figure 13. It was implemented using the same experiment setup described in Section 4. The mode targeted for control was the sway mode (S) at 9.2 kHz. The control was done in real time with a sampling period of 0.01 milliseconds.

Figure 14 shows the uncontrolled and controlled vibrations of the suspension assembly for comparison. Under PPF control, the vibrations damp out within 0.3 milliseconds of the input signal becoming constant. The sensor output from 0 to 2 milliseconds is shown in Figure 15. Under active control, the energy of vibrations drops by 15 dB. PPF control damps down vibrations slightly faster than DVF control. With PPF control, maximum damping is achieved when the controller is tuned to the natural frequency of the structure (Figures 16 and 17). As a counterexample, under PPF, the frequency response of tip displacement at 6 kHz increases by 10 dB. However, the power spectrum density comparison in Figure 18 shows no peak at 6 kHz, implying that PPF control does not affect vibrations at that frequency.

#### 7. Conclusions

Our experiments successfully demonstrate vibration suppression of a hard drive suspension assembly using signals from a self-sensing actuator by Direct Velocity Feedback (DVF) control and Positive Position Feedback (PPF) control. The self-sensing actuator is a piezoelectric transducer acting simultaneously as sensor and actuator mounted on the suspension itself. The sensor generates an estimate of the strain signal and its derivative. In particular, the DVF method was able to attenuate the suspension assembly’s dominant sway mode of vibration by 20 dB. Both DVF and PPF were successful at damping suspension assembly vibrations. Both strategies are good enough for use in real hard disk drives.

#### References

- Y. Li, R. Horowitz, and R. Evans, “Vibration control of a PZT actuated suspension dual-stage servo system using a PZT sensor,”
*IEEE Transactions on Magnetics*, vol. 39, no. 2, pp. 932–937, 2003. View at Publisher · View at Google Scholar · View at Scopus - Y. Li, F. Marcassa, R. Horowitz, R. Oboe, and R. Evans, “Track-following control with active vibration damping of a PZT-actuated suspension dual-stage servo system,” in
*Proceedings of the American Control Conference*, vol. 3, pp. 2553–2559, Denver, Colo, USA, 2003. - H. Yamada, M. Sasaki, and Y. Nam, “Control of a micro-actuator for hard disk drives using self-sensing actuator,”
*International Journal of Applied Electromagnetics and Mechanics*, vol. 24, no. 3-4, pp. 247–259, 2006. View at Google Scholar · View at Scopus - J. J. Dosch, D. J. Inman, and E. Garcia, “Self-sensing piezoelectric actuator for collocated control,”
*Journal of Intelligent Material Systems and Structures*, vol. 3, no. 1, pp. 166–185, 1992. View at Google Scholar · View at Scopus - Y. Nam and M. Sasaki, “Strain rate self-sensing for a cantilevered piezoelectric beam,”
*KSME International Journal*, vol. 16, no. 3, pp. 310–319, 2002. View at Google Scholar · View at Scopus - M. Okugawa and M. Sasaki, “System identification and controller design of a self-sensing piezoelectric cantilever structure,”
*Journal of Intelligent Material Systems and Structures*, vol. 13, no. 4, pp. 241–252, 2002. View at Publisher · View at Google Scholar · View at Scopus - Y. Nam, J. Yoon, and M. Sasaki, “End point motion estimation of a cantilevered piezoelectric beam,”
*JSME International Journal Series C*, vol. 45, no. 3, pp. 722–729, 2002. View at Google Scholar - H. Yamada, M. Sasaki, and Y. Nam, “Active vibration control of a micro-actuator for hard disk drives using self-sensing actuator,”
*Journal of Intelligent Material Systems and Structures*, vol. 19, no. 1, pp. 113–123, 2008. View at Publisher · View at Google Scholar · View at Scopus - M. Sasaki, K. Fujihara, Y. Nam, S. Ito, and Y. Inoue, “Two-degree-of-freedom control of a self-sensing micro-actuator for HDD,”
*International Journal of Applied Electromagnetics and Mechanics*, vol. 36, no. 1-2, pp. 159–166, 2011. View at Publisher · View at Google Scholar - M. J. Balas, “Direct velocity feedback control of large space structure,”
*Journal of Guidance, Control, and Dynamics*, vol. 2, no. 3, pp. 252–253, 1979. View at Google Scholar · View at Scopus - C. J. Goh and T. K. Caughey, “On the stability problem caused by finite actuator dynamics in the collocated control of large space structure,”
*International Journal of Control*, vol. 41, no. 3, pp. 787–802, 1985. View at Google Scholar · View at Scopus - J. L. Fanson and T. K. Caughey, “Positive position feedback control for large space structures,”
*American Institute of Aeronautics and Astronautics Journal*, vol. 28, no. 4, pp. 717–724, 1990. View at Google Scholar - G. Song and B. N. Agrawal, “Vibration suppression of flexible spacecraft during attitude control,”
*Acta Astronautica*, vol. 49, no. 2, pp. 73–83, 2001. View at Publisher · View at Google Scholar · View at Scopus - C. K. Pang, G. Guo, B. M. Chen, and T. H. Lee, “Self-sensing actuation for nanopositioning and active-mode damping in dual-stage HDDs,”
*IEEE/ASME Transactions on Mechatronics*, vol. 11, no. 3, pp. 328–338, 2006. View at Publisher · View at Google Scholar · View at Scopus - K. W. Chan and W. H. Liao, “Self-sensing actuators for adaptive vibration control of hard disk drives,” in
*Proceedings of the IEEE/ASME International Conference on Advanced Intelligent Mechatronics (AIM '08)*, pp. 665–670, August 2008. View at Publisher · View at Google Scholar · View at Scopus