Disk drive detecting head touchdown by applying DC+AC control signal to fly height actuator

Description

BACKGROUND

Disk drives comprise a disk and a head connected to a distal end of an actuator arm which is rotated about a pivot by a voice coil motor (VCM) to position the head radially over the disk. The disk comprises a plurality of radially spaced, concentric tracks for recording user data sectors and embedded servo sectors. The embedded servo sectors comprise head positioning information (e.g., a track address) which is read by the head and processed by a servo controller to control the actuator arm as it seeks from track to track.

An air bearing forms between the head and the disk due to the disk rotating at high speeds. Since the quality of the write/read signal depends on the fly height of the head, conventional heads (e.g., magnetoresistive heads) may comprise an actuator for controlling the fly height. Any suitable dynamic fly height (DFH) actuator may be employed, such as a heater which controls fly height through thermal expansion, or a piezoelectric (PZT) actuator. It is desirable to determine the appropriate setting for the DFH control signal (e.g., appropriate current applied to a heater) that achieves the target fly height for the head.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1A and 1B show a head actuated over a disk, wherein the head comprises a dynamic fly height (DFH) actuator operable to control a fly height of the head.

FIG. 1C is a flow diagram according to an embodiment of the present invention wherein a DFH control signal applied to the DFH actuator comprises a DC component and an AC component comprising an excitation frequency.

FIG. 1D shows a DFH control signal according to an embodiment of the present invention comprising a DC component and an AC component.

FIG. 2A shows an embodiment of the present invention wherein the DC component of the DFH control signal is incrementally increased until a touchdown event is detected in response to a touchdown metric at the excitation frequency.

FIG. 2B shows an embodiment of the present invention wherein the DFH control signal comprises a plurality of pulses, wherein each pulse comprises a DC component and an AC component.

FIG. 3 shows an embodiment of the present invention wherein a frequency of the AC component of the DFH control signal is high enough to attenuate a response of the DFH actuator.

FIG. 4A is a flow diagram according to an embodiment of the present invention for measuring a time constant of the DFH actuator based on a fly height metric, and thereby calibrating the attenuation of the DFH actuator response at the frequency of the AC component of the DFH control signal.

FIG. 4B shows an embodiment of the present invention for measuring the time constant of the DFH actuator based on a fly height metric.

FIG. 5A shows an embodiment of the present invention wherein the touchdown metric comprises a vector Z comprising a magnitude and a phase, wherein the phase of the vector Z is relative to a phase of the DFH control signal.

FIG. 5B is a flow diagram according to an embodiment of the present invention wherein a window of vector Zs is measured, a threshold is generated based on a standard deviation of the vector Zs, and a touchdown event is detected based on a current vector Zc and the threshold.

DETAILED DESCRIPTION

FIG. 1A shows a disk drive according to an embodiment of the present invention comprising a head 2 actuated over a disk 4, wherein the head 2 comprises a dynamic fly height (DFH) actuator 6 (FIG. 1B) operable to control a fly height of the head 2 over the disk 4. The disk drive further comprises control circuitry 8 operable to execute the flow diagram of FIG. 1C, wherein a DFH control signal 10 is applied to the DFH actuator to decrease the fly height of the head (bock 12), wherein the DFH control signal 10 comprises a DC component and an AC component comprising an excitation frequency (FIG. 1D). A touchdown metric is measured over an interval (block 14), and the head contacting the disk is detected in response to a frequency component of the touchdown metric at the excitation frequency (block 16).

In the embodiment of FIG. 1A, the disk 4 comprises embedded servo sectors 18₀-18_N that define a plurality of servo tracks 20, wherein data tracks are defined relative to the servo tracks (at the same or different radial density). The control circuitry 8 processes a read signal 22 emanating from the head 2 to demodulate the servo sectors 18₀-18_N into an estimated position. The estimated position is subtracted from a reference position to generate a position error signal (PES) representing an error between the actual position of the head and a target position relative to a target track. The PES is filtered using a suitable compensation filter to generate a control signal 24 applied to a voice coil motor (VCM) 26 which rotates an actuator arm 28 about a pivot in order to actuate the head 2 radially over the disk 4 in a direction that reduces the PES. The servo sectors 18₀-18_N may comprise any suitable position information, such as a track address for coarse positioning and servo bursts for fine positioning. The servo bursts may comprise any suitable pattern, such as an amplitude-based servo pattern (e.g., a quadrature servo pattern), or a suitable phase-based servo pattern.

Any suitable DFH actuator 6 may be employed in the embodiments of the present invention, such as a heater which controls fly height through thermal expansion, or a piezoelectric (PZT) actuator. In addition, the DFH control signal 10 applied to the DFH actuator 6 may comprise any suitable signal, such as a current or a voltage applied to the DFH actuator 6. In one embodiment, an operating setting for the DFH control signal 10 is generated based on the DFH control signal 10 that causes the head to contact the disk surface (touchdown). The accuracy of the operating setting is therefore dependent on the accuracy of the touchdown detection. Accordingly, in an embodiment of the present invention, employing a DFH control signal 10 comprising a DC component and an AC component improves the accuracy of the measured touchdown metric, thereby improving the accuracy of the operating setting for the DFH control signal 10.

The head 2 in the embodiment shown in FIG. 1B comprises a suitable write element 30 (e.g., a coil) and a suitable read element 32 (e.g., a magnetoresistive element). In one embodiment, the operating setting for the DFH control signal 10 may be configured for the write element 30 during write operations and configured differently for the read element 32 during read operations. Each write/read setting for the DFH control signal 10 may be configured by backing off the setting for the DFH control signal 10 that causes the touchdown event.

The DFH control signal 10 may comprise any suitable waveform, wherein in an embodiment shown in FIG. 2A, the DFH control signal 10 comprises an AC component added to a DC component. In the embodiment shown in FIG. 2A, the DC component is increased (without increasing the amplitude of the AC component) until the touchdown metric indicates a touchdown event. The DC component may be increased based on any suitable function, such as a step increase of the DC component as shown in FIG. 2A. The duration of each step may last any suitable interval, such as one or more revolutions of the disk, or a partial revolution of the disk.

In one embodiment, the frequency of the AC component may equal an integer multiple of the disk rotation frequency such that the AC component is substantially synchronous with the disk rotation frequency. In another embodiment, the frequency of the AC component may equal a non-integer multiple of the disk rotation frequency so that the AC component is intentionally non-synchronous with the disk rotation frequency. In yet another embodiment, the phase of the AC component may be dithered to achieve a non-synchronous relationship between the frequency of the AC component and the rotation frequency of the disk. In the embodiment shown in FIG. 2A, the phase of the AC component may be adjusted at each step increment of the DC component, or the phase of the AC component may be adjusted within the step interval.

When the DC component is increased sufficiently to cause the head to contact the disk, the touchdown event will manifest in a frequency component of the touchdown metric at the excitation frequency of the AC component. The touchdown metric may be evaluated at any excitation frequency of the AC component, such as at the fundamental frequency of the AC component or at a sub-harmonic or harmonic frequency of the AC component. In other embodiments, the touchdown event may be detected by evaluating the touchdown metric at multiple excitation frequencies, such as the fundamental and a harmonic frequency. Any suitable technique may be employed to measure the frequency component of the touchdown metric at the excitation frequency, such as by computing a Fourier transform at the excitation frequency.

Any suitable touchdown metric may be measured in the embodiments of the present invention, such as the current driving the spindle motor, a time period between consecutive servo sectors (wedge-to-wedge time), the PES generated by the servo control system for position the head over the disk, a control signal applied to a variable gain amplifier (VGA) that tracks an amplitude of the read signal, the amplitude of servo bursts, or a sensor signal emanating from a suitable touchdown sensor, such as a tunneling sensor, a tribo-current sensor, or an acoustic emission sensor. Regardless as to the touchdown metric, employing a DFH control signal comprising a DC component and an AC component causes a response in the touchdown metric at an excitation frequency of the AC component that more accurately reflects when the head contacts the disk, thereby achieving a more accurate target fly height during normal operations.

FIG. 2B illustrates an embodiment of the present invention wherein the DFH control signal comprises a plurality of pulses, wherein each pulse comprises a DC component and an AC component. In this embodiment, the DFH control signal is substantially zero for at least part of the interval while measuring the touchdown metric. Also in the embodiment of FIG. 2B, the DFH control signal comprises a first periodic signal (the periodic pulses) comprising a first frequency combined with a second periodic signal (the AC component added to each pulse) comprising a second frequency. The head contacting the disk is detected in response to a first frequency component of the touchdown metric at a first excitation frequency and a second frequency component of the touchdown metric at a second excitation frequency. Similar to the embodiments described above, the first and second excitation frequencies may comprise any suitable frequency, such as a fundamental frequency, a sub-harmonic frequency, or a harmonic frequency of the respective periodic signal.

In the embodiment of FIG. 2B, the pulses cycle at a frequency F1, whereas the AC component added to each pulse cycles at a frequency F2 significantly higher than F1. In one embodiment, the lower frequency pulses induce a response in the touchdown metric at a corresponding excitation frequency that indicates a particular type of touchdown event, such as a friction response of the head contacting the disk which is a relatively slow response. In contrast, the higher frequency AC component added to each pulse may induce a response in the touchdown metric indicative of a different type of response, such as the head bouncing on the disk which is typically a faster response. Accordingly, in this embodiment employing a DFH control signal comprising two periodic signals may enable the control circuitry to detect and discriminate between multiple types of touchdown events.

In one embodiment, the AC component of the DFH control signal may comprise a periodic signal generated at a predetermined frequency that is high enough to attenuate a response of the DFH actuator. This embodiment is illustrated in FIG. 3 wherein the response of the DFH actuator is attenuated by an attenuation factor depending on the frequency of the AC component of the DFH control signal. At low frequencies of the AC component, there is no attenuation in the response of the DFH actuator (the attenuation factor is unity). As the frequency of the AC component increases, the response of the DFH actuator rolls off similar to a low pass filter. In certain embodiments, it may be desirable to employ an AC component at a sufficiently high frequency 34 to detect particular types of touchdown events (e.g., head bounce). However, since a high frequency 34 AC component may attenuate the response of the DFH actuator, in one embodiment the resulting attenuation is taken into account when selecting the operating setting(s) for the DFH control signal. For example, if the frequency of the AC component causes a twenty-five percent attenuation of the DFH actuator response, the operating setting for the DFH control signal is further reduced based on this attenuation factor since the operating DFH control signal is typically generated at a lower frequency that causes less (or no) attenuation of the DFH actuator response.

Any suitable technique may be employed to measure the frequency response of the DFH actuator. In one embodiment illustrated in the flow diagram of FIG. 4A, a transient signal is applied to the DFH actuator (block 36), a fly height metric is measured (block 38), and a time constant of the DFH actuator is measured in response to the measured fly height metric (block 40). The measured time constant may then be used to estimate the bandwidth of the DFH actuator, which in turn may be used to estimate the attenuation factor at the frequency of the AC component in the DFH control signal.

Any suitable transient signal may be applied to the DFH actuator at block 36, wherein in an embodiment shown in FIG. 4B, a square wave is applied to the DFH actuator. A resulting fly height metric is measured over one or more disk revolutions (or partial disk revolution) that may include some level of noise due, for example, to topography variations of the disk surface. The fly height metric is measured over one or more disk revolutions (or partial disk revolution) without applying the square wave to the DFH actuator in order to measure the noise (topography variations) which is subtracted from the noisy fly height metric to generate a fly height metric that more accurately reflects the response of the DFH actuator. The time constant of the DFH actuator is then estimated by measuring the time required for the fly height metric to decay by a predetermined percentage as shown in FIG. 4B. In one embodiment, the decay time may be measured for multiple square wave cycles, and then averaged to improve the accuracy of the estimated time constant.

Any suitable fly height metric may be measured when estimating the time constant of the DFH actuator. In one embodiment, the fly height metric is generated in response to the read signal, such as an amplitude of the read signal, or the gain setting of a variable gain amplifier that attempts to maintain the amplitude of the read signal constant at the input to a read channel. In other embodiments, a fly height metric may be generated by writing a periodic pattern on the disk, and then evaluating the fundamental and harmonics of the resulting read signal (a harmonic ratio technique based on the Wallace spacing equation). In yet other embodiments, a suitable fly height sensor, such as a thermoresistive sensor, capacitive sensor, or tunneling sensor, may be employed that transduces the fly height into a suitable signal representing the fly height metric.

FIG. 5A illustrates an embodiment of the present invention wherein the touchdown metric measured at block 14 of FIG. 1C comprises a vector Z having a magnitude and a phase, wherein the phase of the vector Z is relative to a phase of the DFH control signal 10. Evaluating the touchdown metric as a complex value (vector) relative to the DFH control signal 10 may provide a more accurate estimation of when a touchdown event occurs. That is, the phase of the touchdown metric relative to the DFH control signal 10 may provide additional information about when touchdown occurs, as well as help differentiate between different types of touchdown events. In one embodiment, a moving window of vectors Zs is evaluated to compute a standard deviation for the vectors, and then a touchdown threshold is computed based on the standard deviation.

This embodiment is understood with reference to the flow diagram shown in FIG. 5B, wherein a plurality of the vectors Zs is measured over a window of time (block 42). A mean Zm of the vectors Zs is computed (block 44) which is used to compute the standard deviation of the vectors Zs. A threshold Th is then computed based on the standard deviation (block 46). When a current vector Zc is measured (block 48), a touchdown event is detected based on the current vector Zc and the threshold Th (block 50). For example, in one embodiment the threshold Th may be computed at block 46 as four times the standard deviation, and a touchdown event may be detected if a difference between the magnitude of the current vector Zc and the magnitude of the mean vector Zm exceeds the threshold Th at block 50. If a touchdown event is not detected at block 50, the window of Zs is updated based on the current vector Zc (block 52). The DFH control signal is then modified (block 54) such as by increasing the DC component, and the flow diagram is repeated starting from block 44 until a touchdown event is detected at block 56. In one embodiment, the DFH control signal may be adjusted at block 54 at a lower frequency rather than at every measured touchdown metric. For example, the DFH control signal may be adjusted after measuring N vectors without detecting a touchdown event at block 50.

Any suitable control circuitry may be employed to implement the flow diagrams in the embodiments of the present invention, such as any suitable integrated circuit or circuits. For example, the control circuitry may be implemented within a read channel integrated circuit, or in a component separate from the read channel, such as a disk controller, or certain operations described above may be performed by a read channel and others by a disk controller. In one embodiment, the read channel and disk controller are implemented as separate integrated circuits, and in an alternative embodiment they are fabricated into a single integrated circuit or system on a chip (SOC). In addition, the control circuitry may include a suitable preamp circuit implemented as a separate integrated circuit, integrated into the read channel or disk controller circuit, or integrated into a SOC.

In one embodiment, the control circuitry comprises a microprocessor executing instructions, the instructions being operable to cause the microprocessor to perform the flow diagrams described herein. The instructions may be stored in any computer-readable medium. In one embodiment, they may be stored on a non-volatile semiconductor memory external to the microprocessor, or integrated with the microprocessor in a SOC. In another embodiment, the instructions are stored on the disk and read into a volatile semiconductor memory when the disk drive is powered on. In yet another embodiment, the control circuitry comprises suitable logic circuitry, such as state machine circuitry.