1. Field of the Invention
The present invention relates to calculating a position error signal used in hard disk drives.
2. Background Information
Hard disk drives contain a plurality of magnetic heads that are coupled to rotating disks. The heads write and read information by magnetizing and sensing the magnetic fields of the disk surfaces. Each head is attached to a flexure arm to create a subassembly commonly referred to as a head gimbal assembly (“HGA”). The HGA's are suspended from an actuator arm. The actuator arm has a voice coil motor that can move the heads across the surfaces of the disks.
Information is typically stored in radial tracks that extend across the surface of each disk. Each track is typically divided into a number of segments or sectors. The voice coil motor and actuator arm can move the heads to different tracks of the disks.
Each sector may also have a servo field 5 located adjacent to a data field 6. The servo field 5 contains a plurality of servo bits A, B, C and D that are read and utilized in a servo routine to position the head 7 relative to the track. By way of example, the servo routine may utilize the algorithm of ((A-B)-(C-D)) to create a position error signal (“PES”). The PES is used to create a drive signal for the voice coil motor to position the head on the track. The system can monitor the PES and inhibit a write operation if the PES value exceeds a certain threshold. The PES is also used to perform seek routines to move the heads from one track to another track.
The PES is typically calculated from the total loop gain of the servo. Unfortunately, the total loop gain does not provide the most accurate PES values, which may lead to undesirable write operations or an improper termination of a write operation.
A hard disk drive with a controller that determines a position error signal gain based on a total servo loop gain and a function defined by a slope of a line of A and B servo bits measured at N off-track positions.
Described is a hard disk drive with a controller that determines a position error signal gain. The position error signal gain is determined from a total servo loop gain and a function that is defined by a slope of a line of A and B servo bits measured at N off-track positions. The function determines an actual plant gain and thus provides a more accurate position error signal gain.
Referring to the drawings more particularly by reference numbers,
The disk drive 10 may include a plurality of heads 20 located adjacent to the disks 12. As shown in
Referring to
The hard disk drive 10 may include a printed circuit board assembly 38 that includes one or more integrated circuits 40 coupled to a printed circuit board 42. The printed circuit board 40 is coupled to the voice coil 32, heads 20 and spindle motor 14 by wires (not shown).
The read/write channel circuit 58 is connected to a controller 64 through read and write channels 66 and 68, respectively, and read and write gates 70 and 72, respectively. The read gate 70 is enabled when data is to be read from the disks 12. The write gate 72 is enabled when writing data to the disks 12. The controller 64 may be a digital signal processor that operates in accordance with a software routine, including a routine(s) to write and read data from the disks 12. The read/write channel circuit 58 and controller 64 may also be connected to a motor control circuit 74 which controls the voice coil motor 36 and spindle motor 14. The controller 64 may be connected to a non-volatile memory device 76. By way of example, the device 76 may be a read only memory (“ROM”) that contains instructions that are read by the controller 64.
Each sector of a disk track typically has servo bits A, B, C and D as shown in
If derivatives of the function f(x) are known then the inverse function can be found through integration as shown by the equation below:
Assuming a boundary condition of:
ƒ−1(Y)=X
Then,
Rearranging equation (3) the plant gain is:
The function f(x) is selected to be a profile of the difference between A and B servo bursts measured at N different increments between −X and X. The profile is shown in
A-B burst values are measured at each off-track position (e.g. yAB,1; yAB,2; yAB,n) Block 128 generates A-B burst profile slopes Δu/ΔyAB,1 for each track increment (e.g. Δu/ΔyAB,1; (Δu/ΔyAB,2; Δu/ΔyAB,n). Block 130 calculates a plant gain in accordance with the following equation:
Block 132 computes a position error signal gain from the product of blocks 126 and 130 (i.e. KplantΔu/Δydemod). The position error signal gain can be used to center a head on a track. The PES gain can also be used to perform a servo routine.
While certain exemplary embodiments have been described and shown in the accompanying drawings, it is to be understood that such embodiments are merely illustrative of and not restrictive on the broad invention, and that this invention not be limited to the specific constructions and arrangements shown and described, since various other modifications may occur to those ordinarily skilled in the art.
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Number | Date | Country | |
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20100053799 A1 | Mar 2010 | US |