This invention relates to positioning devices and, more particularly, to micro-positioning devices.
Various types of actuation systems, such as micro-positioners, translating stages, scanners, or actuated systems with gliding surfaces have been proposed to provide precise positioning of movable components.
One type of device that requires the precise positioning of a movable member is a scanning data storage device that includes one or more heads or tips that move relative to a storage media. Scanning probe storage devices have been proposed to provide small size, high capacity, low cost data storage devices. Actuators are used to effect relative movement between a storage media and an array of tips or heads. The heads and storage media can be located on wafers that are separated by a gap. To achieve a high areal data storage density, the relative displacement of the heads and the storage media should be precisely controlled.
Multiple tips are accessed simultaneously to meet data rate requirements, and these tips form a row of an overall head array. Data are written and read in tracks on the storage media. A row of tips is desirable for a simultaneous reading unit because uniform thermal expansion of the components does not generate off-track motion between tips in a row.
A servo system is used to control the relative position of the heads and the storage media. The servo system can be adversely affected by rotational movement of the media with respect to the head array. Only a small amount of rotation is required to misalign a row of tips, such that the first and last heads in the row are off-track.
In one example, the storage media is mounted on a movable sled supported by springs. Positioning of the media relative to the head array is accomplished using actuators providing linear actuation along the two in-plane axes. Torque can be generated by static misalignment of the geometric centroid and center of mass of the media-sled assembly. In addition, the misalignment can also cause linear dynamic disturbances to have rotational components. Another source of torque disturbance comes from the linear actuation forces or spring attachment points not being aligned with the media-sled assembly center of mass due to manufacturing tolerances. Even a relatively small offset can cause one of the actuators to generate a torque sufficient to cause unacceptable track misregistration (TMR). Other external disturbances include rotational and linear shock and vibration. Furthermore, the presence of head-media friction may result in a steady-state error at the end of a shock event. This steady-state error should also be addressed by the position control system.
While a balancing process during fabrication is likely, it is unlikely that this process will be accurate enough to create a completely balanced system. Given the low rotational stiffiness of existing media-sled assemblies and the extremely tight angular tolerance, relatively minor rotational disturbances can cause an undesirable amount of track misregistration.
It would be desirable to provide active control of the rotation of the movable member to meet system requirements.
In a first aspect, the invention provides an apparatus including a movable member, and first and second actuators coupled to the movable member at positions offset from a first axis that passes through a centroid of the movable member. A controller independently controls the first and second actuators to exert a first force on the movable member in a direction generally parallel to the first axis, thereby controlling both linear and rotational orientation of the movable member.
The apparatus can further include third and fourth actuators coupled to the movable member at positions offset from a second axis that passes through the centroid of the movable member, and the controller can independently control third and fourth actuators.
The apparatus can include one or more of electromagnetic actuators, piezoelectric actuators, electrorheological fluid actuators, electrostatic actuators, shape memory alloy actuators, or thermal actuators.
In another aspect, the invention provides an apparatus including a data storage media, an array of tips positioned adjacent to the data storage media, a movable member coupled to either the data storage media or the array of tips, and first and second actuators coupled to the movable member at positions offset from a first axis that passes through a centroid of the movable member. A controller independently controls the first and second actuators in response to position signals and/or servo information to exert a first force on the movable member in a direction generally parallel to the first axis.
The apparatus can further include third and fourth actuators coupled to the movable member at positions offset from a second axis that passes through the centroid of the movable member, and the controller can independently control third and fourth actuators. A plurality of posts can be included to define a distance between the data storage media and the tip substrate.
This invention provides an apparatus including actuators for moving a movable member in a plane. The actuators control both linear and rotational movement of the movable member. In another aspect, this invention provides data storage devices that include actuators for providing relative movement between a plurality of tips and an adjacent storage media.
Referring to the drawings,
Devices constructed in accordance with this invention include actuators for moving the movable member in a plane. When used in a data storage device, the invention can be used to move a storage media or array of tips to provide relative movement between the storage media and the array of tips.
The springs and magnetic keepers can act as heat dissipation elements. The springs can also be electrically connected to the actuators to serve as conductors that deliver current to the actuators.
In
Suspension assembly 86 includes spring assemblies 118 and 120. Spring assembly 118 is shown to include a first spring 122 extending between rigid member 94 and protrusion 114, and a second spring 124 extending between rigid member 96 and protrusion 114. Spring assembly 120 is shown to include a third spring 126 extending between rigid member 94 and protrusion 116, and a fourth spring 128 extending between rigid member 96 and protrusion 116.
In an alternative example, each spring assembly can include a single spring that passes through, is embedded in, or is otherwise attached to one of the protrusions. For example, springs 106 and 108 could be replaced by a single spring that is connected at its ends to the base and is connected at its center to protrusion 102. Similarly, each pair of springs in each spring assembly could be replaced by a single spring.
The ends or attachment points of the springs can be encapsulated in, or built into, plastic injection molded parts. They could alternatively be glued. The springs can be made of steel, although another metal, or silicon, would be a possible substitute. Silicon has the advantage that extremely high aspect ratios are achievable.
Protrusions 114 and 116 extend from central portions of opposite sides of the movable member and lie along a first axis 130 that passes through a centroid 134, or center of mass, of the movable member. Protrusions 102 and 104 extend from central portions of the bars 94 and 96 and lie along a second axis 132 that passes through the centroid 134, or center of mass, of the movable member. The second axis is substantially perpendicular to the first axis.
First and second actuators 138 and 140 are coupled to the movable member at points that are offset with respect to the first axis by a distance δ. Third and fourth actuators 142 and 144 are coupled to the bars at points that are offset with respect to the second axis by a distance δ. While the actuators in
In another example, the support assembly need not be attached to the movable member at points along an axis that passes through the centroid of the movable member. For instance, there could be two protrusions instead of one (such as 114) that are positioned symmetric about the axis of symmetry of the sled with one spring each on the support assembly terminating at each of the protrusions. It is desirable that the net support assembly spring forces are directed along the first and second axes to minimize sensitivity to rotational disturbances.
The actuators can be linear actuators. As used herein, linear actuators are actuators that produce a force that is in a direction substantially along a straight line. In the example of
All springs should be stiff in the Z-direction (i.e., perpendicular to the X-Y plane) and less stiff in the X or Y-direction.
The actuators could be mechanically coupled to the media-sled assembly in a variety of ways. In one example that uses an electromagnetic actuator, the actuator coils can be for instance attached (e.g., overmolded or glued) to the end of the protrusions 102, 104, 114 and 116. The coils would then be interposed between a magnet pair and a keeper surface on the opposite side as illustrated in
In one aspect, this invention provides rotational compensation by using offset linear actuators for actuation of the sled assembly in the X-Y plane in opposite directions with respect to the axis of symmetry of the sled assembly passing through its geometric centroid. By independently controlling a control input to each of the actuators, a control torque can be generated to compensate for rotational disturbances on the sled assembly while simultaneously achieving positioning in the X-Y plane.
The controller also provides control signals to the actuators 138, 140, 142 and 144. Independent control inputs to the actuators can be computed using a control algorithm that is based on feedback information of the rotation of the movable member, which can be referred to as a sled. In one example, the position sensors produce signals that are representative of the position of the movable member. These signals can be processed by the controller to determine the control signals to be supplied to the actuators. The position sensors can be used for both position and rotation detection.
The sled rotation could also be computed, for example, based on positional information at the four corners of the media sensed using wafer-to-wafer edge sensors, servo information embedded in the storage media near each tip, or a combination of the two approaches. Using the sensors in tandem allows estimation of, both linear X-Y position, as well as angular position of the media relative to the head array. The actuators that are positioned near each axis form an actuator pair. For example, actuators 138 and 140 form a first pair and actuators 142 and 144 form a second pair.
The two independent inputs to the actuator pair for tracking can be feedback-controlled to provide the required force for seeking or staying on track and at the same time can generate a control torque for compensating external torques and rotational disturbances. A rotary response control scheme could be implemented using offset actuators along either the scanning or tracking direction only. However, by using offset pairs of actuators in both scanning and tracking directions, the servo gain of the rotary response control scheme can be increased.
Briefly, the position sensors give a measurement of x, y, and θ, where θ is an angle of rotation. The device is desired to follow trajectories specified by Rx and Ry (alternatively referred to as Rtracking and Rscanning) with the θ trajectory equal to 0. The controller takes the error signals and determines correction signals to apply to the actuators. Conceptually, the controller is generating three true control signals (one for x, one for y, and one for θ) and then transforming them into four actuator inputs through the second operation in the controller block. The plant then has a dynamic response to the four control inputs, which shows up in the sensor measurements.
The use of an offset pair of linear actuators for rotational compensation of the sled assembly is applicable to any type of linear actuators including, but not limited to, electromagnetic, piezoelectric, ERF, electrostatic and thermal actuators. Appropriate control algorithms can be developed for any particular type of linear actuators so as to independently control the inputs to the offset pair of actuators in order to generate the required compensating torque.
For the example of
Tcontrol=(UT1−UT2)·δ+(US1−US2)·δ, (1)
where U is the force applied by the actuators, δ is the offset distance of the actuators from an adjacent axis, subscript T1 refers to a first actuator applying a force in the tracking direction, subscript T2 refers to a second actuator applying a force in the tracking direction, subscript S1 refers to a first actuator applying a force in the data or seek direction, subscript S2 refers to a second actuator applying a force in the data or seek direction. In one example, UT1 and UT2 are assumed positive in the positive X-direction and US1 and US2 are assumed positive in the positive Y-direction.
An external disturbance in general can be a combination of rotational and linear disturbances coupled with an imbalance of the center of mass. The total external disturbance coupled about the geometric centroid can be represented as
Texternal=Trot+FlinearX·dCMy+FlinearY·dCMx, (2)
where Texternal includes any kind of rotational disturbances in the form of pure moments, FlinearX is a force applied in a direction parallel to the X-direction, FlinearY is a force applied in a direction parallel to the Y-direction, dCMy is the Y-direction offset of the media-sled assembly center of mass from its geometric centroid, and dCMx is the X-direction offset of the media-sled assembly center of mass from its geometric centroid.
Then
I·α=Tcontrol+Texternal (3)
where α=d2 θ/d t2, and where I is the moment of inertia of the sled assembly, Tcontrol is the control input, Texternal is the vector sum total of external torque disturbances, α is the rotational acceleration of the sled assembly, and θ is the angular rotation of the media-sled assembly. It is desired to stabilize the rotation of the system such that θ→0 in the shortest possible time.
In addition, the actuation forces along the scanning and tracking directions at a given time need to have specific values, referred to as FXrequired and FYrequired. Therefore
UT1+UT2=FXrequired (4)
US1+US2=FYrequired (5)
The use of four offset actuators therefore provides some redundancy in the control. This can possibly be used to optimize some performance parameter related to the rotational dynamics and its control. One such objective function could be the power or control effort spent in compensating the rotational disturbance.
The use of offset actuators for rotational control eliminates the need for additional actuators for rotational control, resulting in significant cost savings and simplicity of the solution. By exploiting the redundancy in the controllable degrees of freedom, rotational control can be achieved optimally, while simultaneously minimizing the penalty on linear actuation force. The control scheme can be easily incorporated in a MIMO control framework that is required for control of linear XY-motion of the movable member. The invention can be applied to any XY-motion platform that requires positional accuracy.
Various actuator geometries can be used, including a pair of offset actuators along the scanning axis, a pair of offset actuators along the tracking axis, or pairs of offset actuators along both the scanning and tracking axes. The use of offset actuators for primary actuation of the sled assembly in the X-Y plane provides a cost-effective solution to the problem of controlling rotational disturbances in a probe-like device. Since only the primary actuators are used, the need for additional actuators for rotation control is eliminated, thus resulting in significant cost savings and reduced complexity of the mechanical architecture of the device.
The invention can achieve rotational control simultaneously with linear actuation of the sled along both X and Y-axes using the same set of actuators. The system exploits redundancy in the controllable degrees of freedom (e.g., up to four control inputs and three kinematic variables that need to be controlled) to optimize a suitable performance measure, for example, minimize the effort required for rotational control or minimize penalty on linear actuation force due to simultaneous rotational control using offset actuators.
Variations of the example of
While the above description relates to probe storage devices, this invention can also be applied to other devices that require movement in an X-Y plane, such as for example, atomic force microscope stages, magnetic recording drag testers, other general X-Y planar scanners, or X-Y motion platforms mounted on gimbals that have low in-plane stiffness requirements. In these applications, the movable member and suspensions might not be housed in an enclosure, but may be mounted in a case, base, frame, or other mounting structure.
The invention is not limited to any particular type of suspension assembly for the movable member. For example, the assembly of
Whereas particular embodiments have been described herein for the purpose of illustrating the invention and not for the purpose of limiting the same, it will be appreciated by those of ordinary skill in the art that numerous variations of the details, materials, and arrangement of parts may be made within the principle and scope of the invention without departing from the invention as described in the appended claims.
Number | Name | Date | Kind |
---|---|---|---|
5266988 | Washisu | Nov 1993 | A |
5329122 | Sakai et al. | Jul 1994 | A |
5426631 | Miyazaki et al. | Jun 1995 | A |
5536988 | Zhang et al. | Jul 1996 | A |
5557596 | Gibson et al. | Sep 1996 | A |
5615143 | MacDonald et al. | Mar 1997 | A |
5679952 | Lutwyche et al. | Oct 1997 | A |
5680387 | Yamano et al. | Oct 1997 | A |
5751684 | Takeda et al. | May 1998 | A |
5801472 | Wada et al. | Sep 1998 | A |
5834864 | Hesterman et al. | Nov 1998 | A |
5883742 | Kamata | Mar 1999 | A |
6029009 | Imura | Feb 2000 | A |
6154611 | Washisu | Nov 2000 | A |
6310342 | Braunstein et al. | Oct 2001 | B1 |
6369400 | Haeberle et al. | Apr 2002 | B1 |
6397008 | Kuwana et al. | May 2002 | B2 |
6459088 | Yasuda et al. | Oct 2002 | B1 |
6484602 | Dagalakis et al. | Nov 2002 | B1 |
6507553 | Kley | Jan 2003 | B2 |
6509620 | Hartwell et al. | Jan 2003 | B2 |
6509670 | Jeong et al. | Jan 2003 | B2 |
6512313 | Choi et al. | Jan 2003 | B2 |
6545385 | Miller et al. | Apr 2003 | B2 |
6587408 | Jacobson et al. | Jul 2003 | B1 |
6638625 | Draeger | Oct 2003 | B1 |
6724712 | Kley | Apr 2004 | B2 |
6735163 | Marshall | May 2004 | B2 |
6784771 | Fan | Aug 2004 | B1 |
6822933 | Ives | Nov 2004 | B2 |
6882019 | Walmsley et al. | Apr 2005 | B2 |
6925047 | Ives | Aug 2005 | B2 |
6996051 | Ives et al. | Feb 2006 | B2 |
7030964 | Akutsu et al. | Apr 2006 | B2 |
7057997 | Birecki et al. | Jun 2006 | B2 |
7142077 | Baeck et al. | Nov 2006 | B2 |
7148549 | Ives et al. | Dec 2006 | B2 |
7440687 | Seo | Oct 2008 | B2 |
20010004420 | Kuwana et al. | Jun 2001 | A1 |
20030201856 | Harney | Oct 2003 | A1 |
20040155737 | Wakatsuki et al. | Aug 2004 | A1 |
20040174237 | Matsumoto | Sep 2004 | A1 |
20050040919 | Baeck et al. | Feb 2005 | A1 |
20050046504 | Xiaoyu et al. | Mar 2005 | A1 |
20050128616 | Johns et al. | Jun 2005 | A1 |
20050190684 | Kley | Sep 2005 | A1 |
20060018645 | Stavely | Jan 2006 | A1 |
20060023606 | Lutwyche et al. | Feb 2006 | A1 |
Number | Date | Country | |
---|---|---|---|
20080297289 A1 | Dec 2008 | US |