WO1997041564A1 - Method for detecting transient write errors in a disk drive - Google Patents

Method for detecting transient write errors in a disk drive Download PDF

Info

Publication number
WO1997041564A1
WO1997041564A1 PCT/US1997/006541 US9706541W WO9741564A1 WO 1997041564 A1 WO1997041564 A1 WO 1997041564A1 US 9706541 W US9706541 W US 9706541W WO 9741564 A1 WO9741564 A1 WO 9741564A1
Authority
WO
WIPO (PCT)
Prior art keywords
disk
data
read
signal
recited
Prior art date
Application number
PCT/US1997/006541
Other languages
French (fr)
Inventor
Yiping Ma
Original Assignee
Iomega Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Iomega Corporation filed Critical Iomega Corporation
Publication of WO1997041564A1 publication Critical patent/WO1997041564A1/en

Links

Classifications

    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B20/00Signal processing not specific to the method of recording or reproducing; Circuits therefor
    • G11B20/10Digital recording or reproducing
    • G11B20/18Error detection or correction; Testing, e.g. of drop-outs
    • G11B20/1816Testing
    • G11B20/182Testing using test patterns
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B19/00Driving, starting, stopping record carriers not specifically of filamentary or web form, or of supports therefor; Control thereof; Control of operating function ; Driving both disc and head
    • G11B19/02Control of operating function, e.g. switching from recording to reproducing
    • G11B19/04Arrangements for preventing, inhibiting, or warning against double recording on the same blank or against other recording or reproducing malfunctions
    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B33/00Constructional parts, details or accessories not provided for in the other groups of this subclass
    • G11B33/14Reducing influence of physical parameters, e.g. temperature change, moisture, dust

Definitions

  • This invention relates generally to storage subsystems for computer systems.
  • this invention relates to methods for detecting errors during write operations in disk drives, especially those caused by transient increases in flying height.
  • a method for verifying the integrity of data written to a disk in a disk drive system that comprises the following steps.
  • a data section is written to disk. Periodically, during the write operation, a pre-recorded signal is read from the disk. If the pre-recorded signal is substantially different from a predetermined value, an error on the previous write may have occurred. Thus, the data section previously written to the disk is read back. If the data section read from the disk is substantially different from the data section that was intended to be written to the disk, an error condition results.
  • FIGURE 1 is a diagram depicting an exemplary disk and arm assembly wherein the method of the present invention may be employed
  • FIGURE 2 is a chart illustrating the relationship between head flying height and signal strength
  • FIGURE 3 is a graphical representation of an exemplary signal of a portion of data from the disk
  • FIGURE 4 is a graphical representation of the exemplary signal showing signal degradation in a track section caused by increased flying height;
  • FIGURE 5 is a graphical representation of the effect of flying height on reading and writing data; and, FIGURE 6 is a flow chart of a presently preferred embodiment of the method of the present invention.
  • FIGURE 1 is a representation of a disk drive mechanism wherein the operation of the present invention may be illustrated. As shown, a disk 12 rotates about a spindle motor axis 14. The surface of the disk 12 is receptive to electromagnetic signals for storing data. Read/write electronics, embedded within slider bearing 16 generates an electromagnetic signal to write data and read an electromagnetic signal from the disk surface to read data.
  • the slider bearing 16 with embedded read/write electronics is also referred to herein as a read/write head 16.
  • the read/write head 16 is attached to arm 18.
  • the head 16 and arm 18 assembly are attached to suspension 20.
  • Spring tension urges the arm 18 and read/write head 16 against the surface of the disk 12.
  • spindle motor shown as spindle axis line 14
  • air pressure develops between the read/write head 16 and the surface of disk 12 and lifts the read/write head 16 off of the surface of the disk 12.
  • the gap that thereby develops between the surface of disk 12 and the read/write head 16 is referred to as the "flying height.”
  • FIGURE 2 graphs the normalized strength of the electromagnetic signal on the disk surface versus the flying height of the read/write head 16.
  • Line 22 plots the relationship between these two variables. Significantly, there is an inverse relationship between the two variables. Thus, increases in flying height correspond to decreases in normalized signal strength.
  • the flying height between the read/write head 16 and the surface of disk 12 reaches approximately between .04 and .1 ⁇ m, depending on the disk drive system, for a properly functioning full spinning disk 12. As illustrated in FIGURE 2 by line 22, such a flying height corresponds to approximately 80 percent of the normalized signal strength.
  • the flying height increases, the signal read will weaken, possibly resulting in read errors.
  • the flying height increase is transient, the data section can be re-read and the data recovered. In other words, the signal on the surface of the disk 12 was written properly, but a transient increase in flying height caused the read/write head 16 to deviate too far from the surface to properly read the data. As illustrated in FIGURE 2, as the flying height exceeds .4 ⁇ m the signal strength rapidly diminishes to zero.
  • the format divides the surface of the disk 12 into tracks and subdivides those tracks into sectors.
  • the surface of disk 12 is divided into tracks by pre-recording servo marks along each track. For example, there may sixty or more servo marks per track, i.e., a servo mark every six degrees.
  • the read/write head 16 uses these servo marks during operation of the disk drive to locate tracks. Thereafter, the read/write head 16 can lock onto tracks by following the servo marks. During an additional format process, which may be separate from track formatting, the track is subdivided into sectors.
  • each sector 33 is demarcated along the track with a header 36 and a trailer 38 that is recorded onto the disk surface.
  • the header contains overhead information, such as constant density recording ("cdr") field (indicating how many bytes to the next servo field) , track id field (identifying all sectors on the same logical track) , sector id field (identifying a particular sector) and id error correction code field (containing an error correction code for cdr, track id and sector id fields) .
  • the number of sectors per track may vary, e.g., the innermost track may have 90 sectors per track, while the outermost track has 150 sectors per track. However, the number of servo fields remains the same for each track. For example, servo marks may appear every 6 degrees around each track. Servo marks contain a grey code (containing the physical track number) , and norm and quad fields (indicating the head distance from the track center) .
  • disk 12 After disk 12 has been properly formatted, it is ready for use, such that data may be read from and written to its surface in data sections within each sector. While the read/write head 16 is reading and writing data to the disk 12, the arm 18 must follow the tracks that were written to the surface of the disk 12 during formatting. The arm 18 via the head 16 thus reads the servo marks to ensure that the tracks are closely followed during operation.
  • the head 16 continues to read the servo marks to ensure proper track following and to read the sector identifiers to find the proper location for data. Additionally, during the write operation, the head continues to read every grey code, servo mark, id mark, cdr field and track id. The signal read back will translate to a specific predetermined value. If any of the value do not match the predetermined value, an error condition results. Also certain values are checked against the error correction code field. If a mismatch occurs the an attempt is made to correct the data using the error correction code field.
  • the norm and quad fields of the servo marks are checked against a predetermined amplitude. If a mismatch occurs a position error will be reported indicating how far the heads are from the center of the track.
  • transient changes in head flying height during writes to disk 12 could result in a permanent signal loss. That is, as the flying height increases, the signal recorded on the media decreases. Thus, if the flying height crosses a threshold point, which may vary based on such factors as recording media and head type, the signal would not be recoverable on subsequent read operations. Unfortunately in such a case, the error may not be discovered until much later and permanent data loss could result .
  • a feature of the present invention detects and corrects write errors caused by transient increases in flying height with a minimal impact on drive performance.
  • This feature exploits the need for the drive to continue to read information, such as servo marks, from the disk 12 even during write operations. Therefore, flying height increases that persist while the read/write head is flying above portions of the disk 12 having pre-recorded signals, such as a servo mark, are detected and corrected.
  • some information, such as servo marks was written and verified prior to the use of the disk 12, read signal degradation detected during track following and sector seeking likely resulted from flying height increases.
  • the data previously written is re-read and verified. As a result, a high quality write operation can be performed while only verifying a minimal amount of data.
  • FIGURES 3 and 4 graphically present linear representations of track sections 30 from the disk 12.
  • signal strength has been graphed along the y axis and time has been graphed along the x axis.
  • data sections 32a, 32b were written normally, i.e., while no changes in flying height were experienced.
  • the pre-recorded signals such as the servo mark 34, the sector headers 36a, 36b and the sector trailer 38 have substantially the same signal strength as the data sections recorded during subsequent write operations.
  • FIGURE 4 presents a similar track section 30 written while experiencing a change in flying height.
  • the signal strength degrades in the data sections 32a, 32b of FIGURE 4. That signal weakness corresponds to an increase in head flying height during the write operation.
  • the pre-recorded information such as servo marks 34 and sector headers 36a, 36b remain at pre-recorded signal levels.
  • the data recorded therein will likely be unreadable and unrecoverable if it remains uncorrected.
  • the read/write head 16 by testing the strength of the pre ⁇ recorded signal, e.g., servo marks 34 and sector identifiers (embedded within sector headers 36) , while writing to the data sections 32, transient changes in flying height can be detected.
  • the pre-recorded signals 34, 36, and 38 remain at pre-recorded signal strength, a read of those signals during the increase m flying height would likely result in diminished signal strength and read errors.
  • the read/write head 16 while data is written to the disk 12, the read/write head 16 must constantly determine its current location. As noted above, this determination is conventionally performed by reading servo marks 34 and sector identifiers.
  • the process begins with a request to write a block of data to the disk 12, starting at a particular track and sector location (Step 100) .
  • an error flag is initialized to zero (step 102) . This flag is used, as will be further described below, to indicate whether a potential write error has occurred.
  • the arm 18 moves the head 16 to the proper track by seeking to and following the servo marks.
  • a servo mark is read (step 104) . According to an aspect of the present invention, if the flying height of the head 16 is to high an error will occur during the read of the servo mark.
  • the servo mark read is tested (step 106) . If an error occurred during that read of the servo mark (step 104) , the error flag is set. If, on the other hand, no error occurred, the process continues.
  • the head scans the track for the proper sector to receive the data. Accordingly, the sector identifier is read (step 110) . Any errors occurring during the read of the sector identifier result in the setting of the error flag. As with the servo mark read, excessive flying height during the read of the sector identifier will also result in a read error. Thus, the read of the sector identifier is tested for errors (step 112) . If the read of the sector identifier resulted in an error, the error flag is set (Step 114) .
  • the data is written to the data section of the sector (step 116) (i.e., assuming the error is recoverable via an error correction code) . If the write is not complete, i.e., more data remains to be written to different sectors, the process continues (steps 118, 120) . Otherwise, the write is complete and the error flag is checked (steps 118, 122) . If no read error occurred, the operation is complete. However, if the error flag is set indicating a read error, all the data previously written during this write request is read back for verification (step 124) . As a final step in the event of an error, the sectors with faulty data are re-written or the error is reported (step 128) .

Abstract

A method for reducing write errors in a disk drive system is presented. When the flying height of a read/write head above a disk surface becomes too great, the signal strength diminishes and data write errors will occur. Often these increases in flying height are transient. Flying height increases are determined by detecting servo mark and sector information read errors. Recently written data is verified after detection of flying height induced errors.

Description

METHOD FOR DETECTING TRANSIENT WRITE ERRORS IN A DISK DRIVE
Field of the Invention
This invention relates generally to storage subsystems for computer systems. In particular, this invention relates to methods for detecting errors during write operations in disk drives, especially those caused by transient increases in flying height.
Background of the Invention
Maximizing the reliability of the data in disk drives is a key objective of disk drive designers.
Unfortunately, that objective often conflicts with the similarly important need for performance. That is, by increasing the reliability performance measures, such as the data transfer rate, could suffer. For example, when data is written to the disk drive, the success of the write operation, i.e., whether the media accepted the data is unknown. One sure way to guarantee the success of a write operation is by re-reading the recorded data after each write operation. However, a technique that requires all data written to be read as well would severely degrade the performance of the drive. On the other hand, such verification would ensure high reliability of the data.
As explained above, these conflicting demands are particularly relevant during write operations. By contrast, if an error occurs during a read operation, the offending section of data can be re-read. However, errors occurring during write operations are more likely to result in permanent data loss .
Write errors are often transient. That is, if the error was detected and the write re-attempted the write would be successful. For example, write errors caused by dust particles might be corrected if re-attempted. Such contaminants could temporarily displace the recording mechanism, which results in an error during the write operation. Significantly, these transient write errors are particularly prevalent in removable media disk drives. Applicants have recognized that during the use of such removable media drives, the media is repeatedly removed and reinserted, increasing the likelihood of contaminants entering the cartridge. Thus, there is a need for a method to detect transient write errors and to ensure a more reliable write operation while minimizing any performance penalty.
Summary of the Invention
A method is presented for verifying the integrity of data written to a disk in a disk drive system that comprises the following steps.
A data section is written to disk. Periodically, during the write operation, a pre-recorded signal is read from the disk. If the pre-recorded signal is substantially different from a predetermined value, an error on the previous write may have occurred. Thus, the data section previously written to the disk is read back. If the data section read from the disk is substantially different from the data section that was intended to be written to the disk, an error condition results.
According to an aspect of the invention, if an error condition occurs the data section is re-written.
Brief Description of the Drawings
The foregoing summary, as well as the following detailed description of the preferred embodiments, is better understood when read in conjunction with the appended drawings. For the purpose of illustrating the invention, there is shown in the drawings embodiments that are presently preferred, it being understood, however, that the invention is not limited to the specific methods and instrumentalities disclosed.
In the drawings :
FIGURE 1 is a diagram depicting an exemplary disk and arm assembly wherein the method of the present invention may be employed;
FIGURE 2 is a chart illustrating the relationship between head flying height and signal strength;
FIGURE 3 is a graphical representation of an exemplary signal of a portion of data from the disk; FIGURE 4 is a graphical representation of the exemplary signal showing signal degradation in a track section caused by increased flying height;
FIGURE 5 is a graphical representation of the effect of flying height on reading and writing data; and, FIGURE 6 is a flow chart of a presently preferred embodiment of the method of the present invention.
Detailed Description of the Invention
A preferred embodiment of the invention will now be described with reference to the FIGURES 1-6. Those of ordinary skill in the art should appreciate that the description given herein with respect to those figures is for exemplary purposes only and is not intended in any way to limit the scope of the invention. For example, the number of sectors and servo marks used are merely to illustrate and are not intended to limit the invention. FIGURE 1 is a representation of a disk drive mechanism wherein the operation of the present invention may be illustrated. As shown, a disk 12 rotates about a spindle motor axis 14. The surface of the disk 12 is receptive to electromagnetic signals for storing data. Read/write electronics, embedded within slider bearing 16 generates an electromagnetic signal to write data and read an electromagnetic signal from the disk surface to read data. The slider bearing 16 with embedded read/write electronics is also referred to herein as a read/write head 16. The read/write head 16 is attached to arm 18. The head 16 and arm 18 assembly are attached to suspension 20. To access selected data sections, the arm 18 with attached read/write head 16 moves over the surface of disk 12 both reading and writing data as required. Spring tension (not shown) urges the arm 18 and read/write head 16 against the surface of the disk 12. When the spindle motor (shown as spindle axis line 14) spins the disk 12 at full speed, air pressure develops between the read/write head 16 and the surface of disk 12 and lifts the read/write head 16 off of the surface of the disk 12. The gap that thereby develops between the surface of disk 12 and the read/write head 16 is referred to as the "flying height."
FIGURE 2, graphs the normalized strength of the electromagnetic signal on the disk surface versus the flying height of the read/write head 16. Line 22 plots the relationship between these two variables. Significantly, there is an inverse relationship between the two variables. Thus, increases in flying height correspond to decreases in normalized signal strength. The flying height between the read/write head 16 and the surface of disk 12 reaches approximately between .04 and .1 μm, depending on the disk drive system, for a properly functioning full spinning disk 12. As illustrated in FIGURE 2 by line 22, such a flying height corresponds to approximately 80 percent of the normalized signal strength. During a read operation, if the flying height increases, the signal read will weaken, possibly resulting in read errors. If the flying height increase is transient, the data section can be re-read and the data recovered. In other words, the signal on the surface of the disk 12 was written properly, but a transient increase in flying height caused the read/write head 16 to deviate too far from the surface to properly read the data. As illustrated in FIGURE 2, as the flying height exceeds .4 μm the signal strength rapidly diminishes to zero.
Before data can be read or written to disk 12, that disk must be formatted. The format divides the surface of the disk 12 into tracks and subdivides those tracks into sectors. The surface of disk 12 is divided into tracks by pre-recording servo marks along each track. For example, there may sixty or more servo marks per track, i.e., a servo mark every six degrees. The read/write head
16 uses these servo marks during operation of the disk drive to locate tracks. Thereafter, the read/write head 16 can lock onto tracks by following the servo marks. During an additional format process, which may be separate from track formatting, the track is subdivided into sectors.
As shown in FIGURE 3, each sector 33 is demarcated along the track with a header 36 and a trailer 38 that is recorded onto the disk surface. The header contains overhead information, such as constant density recording ("cdr") field (indicating how many bytes to the next servo field) , track id field (identifying all sectors on the same logical track) , sector id field (identifying a particular sector) and id error correction code field (containing an error correction code for cdr, track id and sector id fields) . The number of sectors per track may vary, e.g., the innermost track may have 90 sectors per track, while the outermost track has 150 sectors per track. However, the number of servo fields remains the same for each track. For example, servo marks may appear every 6 degrees around each track. Servo marks contain a grey code (containing the physical track number) , and norm and quad fields (indicating the head distance from the track center) .
After disk 12 has been properly formatted, it is ready for use, such that data may be read from and written to its surface in data sections within each sector. While the read/write head 16 is reading and writing data to the disk 12, the arm 18 must follow the tracks that were written to the surface of the disk 12 during formatting. The arm 18 via the head 16 thus reads the servo marks to ensure that the tracks are closely followed during operation.
Significantly, during a write operation, the head 16 continues to read the servo marks to ensure proper track following and to read the sector identifiers to find the proper location for data. Additionally, during the write operation, the head continues to read every grey code, servo mark, id mark, cdr field and track id. The signal read back will translate to a specific predetermined value. If any of the value do not match the predetermined value, an error condition results. Also certain values are checked against the error correction code field. If a mismatch occurs the an attempt is made to correct the data using the error correction code field.
The norm and quad fields of the servo marks are checked against a predetermined amplitude. If a mismatch occurs a position error will be reported indicating how far the heads are from the center of the track. As should be appreciated from FIGURE 2, transient changes in head flying height during writes to disk 12 could result in a permanent signal loss. That is, as the flying height increases, the signal recorded on the media decreases. Thus, if the flying height crosses a threshold point, which may vary based on such factors as recording media and head type, the signal would not be recoverable on subsequent read operations. Unfortunately in such a case, the error may not be discovered until much later and permanent data loss could result . A feature of the present invention detects and corrects write errors caused by transient increases in flying height with a minimal impact on drive performance. This feature exploits the need for the drive to continue to read information, such as servo marks, from the disk 12 even during write operations. Therefore, flying height increases that persist while the read/write head is flying above portions of the disk 12 having pre-recorded signals, such as a servo mark, are detected and corrected. In particular, since some information, such as servo marks, was written and verified prior to the use of the disk 12, read signal degradation detected during track following and sector seeking likely resulted from flying height increases. In a presently preferred embodiment of the present invention, the data previously written is re-read and verified. As a result, a high quality write operation can be performed while only verifying a minimal amount of data. To further illustrate the effect of transient increases in flying height during write operations, FIGURES 3 and 4 graphically present linear representations of track sections 30 from the disk 12. In both FIGURES, signal strength has been graphed along the y axis and time has been graphed along the x axis. Referring to FIGURE 3, data sections 32a, 32b were written normally, i.e., while no changes in flying height were experienced. Significantly, the pre-recorded signals such as the servo mark 34, the sector headers 36a, 36b and the sector trailer 38 have substantially the same signal strength as the data sections recorded during subsequent write operations. By contrast, FIGURE 4 presents a similar track section 30 written while experiencing a change in flying height. By comparison to the signal strength depicted in Figure 3, the signal strength degrades in the data sections 32a, 32b of FIGURE 4. That signal weakness corresponds to an increase in head flying height during the write operation. Importantly, even though the signal strength of the data 32a has diminished, the pre-recorded information, such as servo marks 34 and sector headers 36a, 36b remain at pre-recorded signal levels. As a result of the poor signal strength in the data sections 32a, 32b, the data recorded therein will likely be unreadable and unrecoverable if it remains uncorrected.
According to a presently preferred embodiment of the present invention, by testing the strength of the pre¬ recorded signal, e.g., servo marks 34 and sector identifiers (embedded within sector headers 36) , while writing to the data sections 32, transient changes in flying height can be detected. Although the pre-recorded signals 34, 36, and 38 remain at pre-recorded signal strength, a read of those signals during the increase m flying height would likely result in diminished signal strength and read errors. As best illustrated in FIGURE 5, while data is written to the disk 12, the read/write head 16 must constantly determine its current location. As noted above, this determination is conventionally performed by reading servo marks 34 and sector identifiers. Significantly, if such a read is made while experiencing an increase in flying height, those signals, e.g., 34, 36, will appear weak. Correspondingly, the write operation to data sections 32 will likely have resulted in a weak signal. Thus, an error detected on a read of the servo mark 34 and the sector identifier within the sector header 36a indicates that the nearby data 32a should be verified.
Referring now to FIGURE 6, a presently preferred embodiment of the process of the present invention will be described in detail. The process begins with a request to write a block of data to the disk 12, starting at a particular track and sector location (Step 100) . Before beginning the write, an error flag is initialized to zero (step 102) . This flag is used, as will be further described below, to indicate whether a potential write error has occurred. After the initialization, the arm 18 moves the head 16 to the proper track by seeking to and following the servo marks. Thus, a servo mark is read (step 104) . According to an aspect of the present invention, if the flying height of the head 16 is to high an error will occur during the read of the servo mark. Accordingly, the servo mark read is tested (step 106) . If an error occurred during that read of the servo mark (step 104) , the error flag is set. If, on the other hand, no error occurred, the process continues. Next, the head scans the track for the proper sector to receive the data. Accordingly, the sector identifier is read (step 110) . Any errors occurring during the read of the sector identifier result in the setting of the error flag. As with the servo mark read, excessive flying height during the read of the sector identifier will also result in a read error. Thus, the read of the sector identifier is tested for errors (step 112) . If the read of the sector identifier resulted in an error, the error flag is set (Step 114) .
According to the presently preferred embodiment, whether or not an error occurred during one of the reads indicated above, the data is written to the data section of the sector (step 116) (i.e., assuming the error is recoverable via an error correction code) . If the write is not complete, i.e., more data remains to be written to different sectors, the process continues (steps 118, 120) . Otherwise, the write is complete and the error flag is checked (steps 118, 122) . If no read error occurred, the operation is complete. However, if the error flag is set indicating a read error, all the data previously written during this write request is read back for verification (step 124) . As a final step in the event of an error, the sectors with faulty data are re-written or the error is reported (step 128) .
Those skilled in the art will readily appreciate that many modifications are possible within the scope of the present invention. For example, the techniques described herein are not limited to completing the entire write operation before testing for errors, after detecting the read error verification could take place immediately. Moreover, other types of prerecorded data rather than the servo mark and the sector identifier may be used to test for flying height errors, those used herein are merely those that are presently preferred. Accordingly, the scope of the invention is not intended to be limited by the preferred embodiment described above but only by the appended claims.

Claims

WHAT IS CLAIMED IS:
1. A method of verifying the integrity of data written to a disk in a disk drive system, comprising the steps of : (a) writing a first data section to a portion of the disk;
(b) periodically reading a pre-recorded signal from the disk;
(c) if said pre-recorded signal is substantially different from a predetermined value, reading the first data section written to the disk; and
(d) if said first data section read from the disk is substantially different from said first data section written to the disk, generating an error condition.
2. A method as recited in claim 1 wherein the step of generating an error condition comprises the further step of re-writing the first data section to disk.
3. A method as recited in claim 1 wherein the step of generating an error condition comprises the further step of reporting an error condition.
4. A method as recited in claim 1 further comprising the step of preparing a disk with said pre¬ recorded signal having a predetermined value.
5. A method as recited in claim 4 wherein said pre-recorded signal is a servo mark.
6. A method as recited in claim 4 wherein said pre-recorded signal is a sector identification.
7. A method as recited in claim 4 wherein said pre-recorded signal is at least one of a sector identification and a servo mark.
8. A method of selectively verifying data written to a disk in a disk drive system, comprising the steps of :
(a) receiving a request to write data to disk;
(b) writing at least one portion of said data to disk;
(c) reading at least one signal arranged on said disk substantially subsequent to said at least one portion of said data such that an error reading said at least one signal indicates that the step of writing said at least one portion of said data may have been erroneous;
(d) comparing said at least one signal to a predetermined value; (e) if said at least one signal is substantially different from said predetermined value, reading said first portion of said data;
(f) comparing said at least one portion of said data read from the disk to a corresponding at least one portion of said data written to said disk; and,
(g) if said at least one portion of said data read from said disk is substantially different from said corresponding at least one portion of said data written to said disk, generating an error condition.
9. A method as recited in claim 8 wherein said step of generating an error condition comprises the step of re-writing said at least one portion of said data to disk.
10. A method as recited in claim 8 wherein said step of generating an error condition comprises the step of generating a message indicating a write error.
11. A method as recited in claim 8 wherein said at least one signal is a servo mark.
12. A method as recited in claim 8 wherein said at least one signal is a sector identifier.
13. A method as recited in claim 8 wherein said at least one signal is at least one of a servo mark and a sector identifier.
PCT/US1997/006541 1996-04-26 1997-04-16 Method for detecting transient write errors in a disk drive WO1997041564A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/639,176 US5588007A (en) 1996-04-26 1996-04-26 Method for detecting transient write errors in a disk drive
US08/639,176 1996-04-26

Publications (1)

Publication Number Publication Date
WO1997041564A1 true WO1997041564A1 (en) 1997-11-06

Family

ID=24563044

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1997/006541 WO1997041564A1 (en) 1996-04-26 1997-04-16 Method for detecting transient write errors in a disk drive

Country Status (3)

Country Link
US (1) US5588007A (en)
TW (1) TW403898B (en)
WO (1) WO1997041564A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1026683A1 (en) * 1999-02-08 2000-08-09 Hewlett-Packard Company System and method for ensuring the integrity of stored data
US6411458B1 (en) 1999-04-23 2002-06-25 Western Digital Technologies, Inc. Disk drive employing method of monitoring transducer flying height to retire defective data site on recording surface
GB2385978B (en) * 2001-05-22 2004-11-24 Seagate Technology Llc Low amplitude skip write detector

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5961656A (en) * 1995-10-31 1999-10-05 Sun Microsystems, Inc. Method and apparatus for testing memory devices under load
KR100412344B1 (en) * 1997-04-08 2004-02-14 삼성전자주식회사 Method for controlling data write according to head flying height
US5935261A (en) * 1997-06-05 1999-08-10 International Business Machines Corporation Method and apparatus for detecting handling damage in a disk drive
US6459544B1 (en) 1998-11-20 2002-10-01 Bruce M. Harper Removable cartridge for data-storage medium
US6426928B1 (en) 1999-03-31 2002-07-30 International Business Machines Corporation Ability to distinguish true disk write errors
KR20010101145A (en) * 1999-10-07 2001-11-14 로리 비. 키팅 Method for detecting transient write errors in a disk drive and for differentiating transient write errors from permanent media damage
US6578164B1 (en) 2000-07-12 2003-06-10 Iomega Corporation Method for detecting transient write errors in a disk drive having a dual transducer slider
JP3688986B2 (en) * 2000-09-11 2005-08-31 ヒタチグローバルストレージテクノロジーズネザーランドビーブイ Rotating storage device and control method thereof
US6762893B2 (en) 2000-09-28 2004-07-13 Seagate Technology Llc Skip write detection apparatus and method
WO2002035541A2 (en) * 2000-10-23 2002-05-02 Iomega Corporation Method for detecting transient write errors in a disk drive by detecting thermal interference during write process
US6854022B1 (en) 2002-02-22 2005-02-08 Western Digital Technologies, Inc. Disk drive using rotational position optimization algorithm to facilitate write verify operations
US20040100712A1 (en) * 2002-11-27 2004-05-27 Riospring, Inc. Handling data fault and retry in writing/reading data to/from a disk
US7076604B1 (en) 2002-12-24 2006-07-11 Western Digital Technologies, Inc. Disk drive employing a disk command data structure for tracking a write verify status of a write command
US7102845B2 (en) * 2003-10-20 2006-09-05 Quantum Corporation Servo methods and systems using existing data structures and medium edge position
US7139152B2 (en) * 2003-10-20 2006-11-21 Quantum Corporation Servo methods and systems using existing data structures and optical masks
US7085095B2 (en) * 2003-10-20 2006-08-01 Quantum Corporation Electromagnetic void-sensing probes and position control systems
US7136255B2 (en) * 2003-10-20 2006-11-14 Quantum Corporation Servo methods and systems using masked medium edge position sensors
US7116514B2 (en) 2003-10-20 2006-10-03 Quantum Corporation Methods and systems for magnetic recording
US7149050B2 (en) * 2003-10-20 2006-12-12 Quantum Corporation Diffractive position sensors and control systems
US7130138B2 (en) * 2003-12-15 2006-10-31 Seagate Technology Llc Environmental stress protection scheme for a data storage device
US7184233B2 (en) * 2004-06-04 2007-02-27 Quantum Corporation Dual source tracking servo systems and associated methods
TWI276089B (en) * 2004-07-19 2007-03-11 Mediatek Inc Method and device for detecting the defect of an optical disc
US20060103968A1 (en) * 2004-11-12 2006-05-18 Jurneke Joe K Dynamic skew compensation systems and associated methods
US7499235B2 (en) * 2005-03-18 2009-03-03 Quantum Corporation Auto-servo tape system and associated recording head
KR100712510B1 (en) * 2005-05-09 2007-04-27 삼성전자주식회사 Write strength control method of hard disc drive and recording medium adapted the same
US7826169B2 (en) 2007-04-25 2010-11-02 Quantum Corporation Servo error detection and compensation utilizing virtual data tracking servo methods
US7774540B2 (en) * 2007-12-26 2010-08-10 Hitachi Global Storage Technologies Netherlands B.V. Storage system and method for opportunistic write-verify
US20100157750A1 (en) * 2008-12-24 2010-06-24 Shih-Hsin Chen Defect detecting method and system for optical disc
US8924775B1 (en) * 2012-09-25 2014-12-30 Western Digital Technologies, Inc. Methods, devices and systems for tracking and relocating intermittently defective disk sectors to prevent indefinite recycling thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4398228A (en) * 1981-04-28 1983-08-09 Iomega Corporation Method of avoiding resonance in servo controlled apparatus
US4982295A (en) * 1988-01-28 1991-01-01 Mitsumi Electric Co., Ltd. Method for centering a read/write head of a magnetic data storage apparatus on a track of a magnetic disk
US5377058A (en) * 1992-12-31 1994-12-27 International Business Machines Corporation Fly height servo control of read/write head suspension
US5465182A (en) * 1992-05-06 1995-11-07 Fujitsu Limited Recording method of servo information
US5471351A (en) * 1993-07-09 1995-11-28 Fujitsu Limited Method and apparatus of verifying accurate writing through comparisons of written and read data

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5371638A (en) * 1992-06-24 1994-12-06 Digital Equipment Corporation Servo method and apparatus for very high track density magnetic recording by adjusting head position based on servo information read from adjacent track

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4398228A (en) * 1981-04-28 1983-08-09 Iomega Corporation Method of avoiding resonance in servo controlled apparatus
US4982295A (en) * 1988-01-28 1991-01-01 Mitsumi Electric Co., Ltd. Method for centering a read/write head of a magnetic data storage apparatus on a track of a magnetic disk
US5465182A (en) * 1992-05-06 1995-11-07 Fujitsu Limited Recording method of servo information
US5377058A (en) * 1992-12-31 1994-12-27 International Business Machines Corporation Fly height servo control of read/write head suspension
US5471351A (en) * 1993-07-09 1995-11-28 Fujitsu Limited Method and apparatus of verifying accurate writing through comparisons of written and read data

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1026683A1 (en) * 1999-02-08 2000-08-09 Hewlett-Packard Company System and method for ensuring the integrity of stored data
US6266677B1 (en) 1999-02-08 2001-07-24 Hewlett Packard Company System and method for ensuring the integrity of stored data
US6411458B1 (en) 1999-04-23 2002-06-25 Western Digital Technologies, Inc. Disk drive employing method of monitoring transducer flying height to retire defective data site on recording surface
GB2385978B (en) * 2001-05-22 2004-11-24 Seagate Technology Llc Low amplitude skip write detector

Also Published As

Publication number Publication date
TW403898B (en) 2000-09-01
US5588007A (en) 1996-12-24

Similar Documents

Publication Publication Date Title
US5588007A (en) Method for detecting transient write errors in a disk drive
EP0194640B1 (en) Information recording and reproducing apparatus
US6650495B2 (en) Recording error history embedded rewriteable media
US4821254A (en) Information recording and reproducing apparatus which detects deterioration of a medium in each sector before recording
EP0164746B1 (en) Optical information recording and reproducing apparatus and optical disc
US5596460A (en) System and method for encoding a servo address
US5889631A (en) Detecting a track tear servo defect condition in a hard disc drive
US7206990B2 (en) Data sector error handling mechanism
US6765748B2 (en) Method of interleaving servo information fields for track following and seeking and a recording medium including interleaved servo information fields
US20050201015A1 (en) Data transfer device and method
US6539496B1 (en) Method for preventing repeating non-recoverable read errors at same physical location on data storage media
US6993688B2 (en) Data sector error tracking and correction mechanism
US6104558A (en) System and method of encoding an index mark into a servo address
US5917669A (en) Method for transferring operational data between stations during a disk format process
US6975467B1 (en) Method and apparatus for high fly write detection in a disk drive
WO2001027924A1 (en) Method for detecting transient write errors in a disk drive and for differentiating transient write errors from permanent media damage
EP0994476A1 (en) Magnetic disk apparatus with lower probability of occurrence of read errors due to scratch or the like on magnetic disk surface
US20050073761A1 (en) Media drive, processing method for recording data onto a medium, processing method for data read from a medium, and method for controlling a process for reading data from a medium
US20030182605A1 (en) Process and device for identifying and designating radially-oriented patterns of defects on a data-storage medium
JP2830850B2 (en) Protection method for off-track in magnetic disk device and magnetic disk device
US20110222182A1 (en) Disk device and write method
KR100288286B1 (en) Sero control method upon the error of a certain track and the error of servo timing
JPH09213014A (en) Information recording method
JPH03245365A (en) Magnetic storage device

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): CA JP SG

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
NENP Non-entry into the national phase

Ref country code: JP

Ref document number: 97538966

Format of ref document f/p: F

NENP Non-entry into the national phase

Ref country code: CA

122 Ep: pct application non-entry in european phase