Apparatus for Reducing Vibration Inputs to a Device and/or for Positioning the Device

1. Field of the Invention

This invention relates to an apparatus for improving the operational performance of a machine, device or the like, and, more particularly, to an such apparatus for compensating for positioning, pointing and/or orientation errors caused by defections of structural members and components of a high performance machine or device and/or for reducing vibration inputs to such machine or device and/or for micro-positioning such machine or device so as to improve the operational performance thereof.

2. Description of the Prior Art

Typically, high performance machines, devices, components or the like, may have to perform or maneuver at relatively high speeds and/or accelerations and/or may be subjected to input disturbances. To attain such high speeds and/or accelerations, it is desirable to make these machines light weight. A by product of the weight reduction is the added structural flexibility even though relatively light weight and relatively stiff materials, such as, advanced composites and ceramics are utilized. Such machines or devices may include ultra-high speed and accuracy machine tools, positioning tables, precise pointing devices such as gun barrels, spacecrafts and rotorcrafts, robotic manipulators, cranes, quality control and measurement systems, machinery used in the electronics industry such as probes, lead bonding, laser and x-ray litiography, and so forth, and similar high performance products and computer controlled machines.

When operating at relatively high speeds and/or accelerations, the above-described machines may have structures and/or components that behave as relatively flexible. Such relatively flexible structures may adverse affect the operational performance, that is, the attainable level of operating speed and/or acceleration, and/or positioning accuracy and/or orientation accuracy and/or pointing accuracy of such machines or devices. Further, as a result of such flexibilities, such machines or devices may have vibration stabilization and control problems which could adversely affect the performance of the machines. Further, insufficient vibration damping may also adversely affect the positioning, pointing or orientation accuracy of such machines or devices by requiring a relatively long settling time for such vibration to "settle out". Therefore, desired or required positioning, pointing or orientation (or tracking) accuracies or settling times may not be achievable, thus resulting in relatively poor operational performance.

As an example, consider the situation in which it is desired to point a gun barrel of a turret weapon system. During aggressive maneuvering and firing, the gun barrel behaves as a relatively flexible beam. Such flexibility can result in structural vibration which ultimately affects the pointing accuracy of the tip of the gun barrel. Although the turret weapon system may have a main actuator(s) for providing movements, such main actuator is not located at the tip of the gun barrel. As a result, the main actuator drives the tip of the gun barrel through the relatively flexible gun barrel, that is, the actuator is non-collocated with the tip of the gun barrel. As a result of such non-collocation and/or non-linearities (such as, stiction, friction, backlash, non-linear elasticity due to drive train, and so forth) between the tip of the gun barrel and the main actuator, it is relatively difficult, if not impossible, to achieve high pointing accuracy. Furthermore, the main actuator may also not have the required bandwidth to correct for the structural modes of vibration particularly those affecting pointing accuracy.

As another example, consider positioning and/or orientation of an end-effector of a robotic manipulator. In this situation, at relatively high operating speeds and/or accelerations, the links between the joint actuator(s) and the end-effector behaves as a flexible member. As such, in this situation, the joint actuator(s) is non-collocated with the end-effector. Similarly, in this situation, the excitation of a structural mode or modes due to the vibration thereof may seriously affect the positioning or orientation accuracy so as to adversely affect the operational performance of the robotic manipulator.

Therefore, as is to be appreciated, it is desirable to compensate for adverse effects of deflections in structural members and components due to the above-described vibration and structural flexibility of such machines, devices or components so as to improve the operational performance thereof. In an attempt to improve such operational performance, various control techniques or systems have been suggested or utilized. However, such control systems normally result in only a limited amount of improvement in the operational performance of the respective machine or device.

Further, high performance machines, devices or the like may be subjected to externally generated vibration (which may be high frequency vibration) which may adversely affect the operational performance of such machines or devices. In an attempt to reduce such vibration, vibration isolation systems have been developed which may reduce the vibration inputs to a machine or device along one direction. However, such vibration isolation systems may not adequately reduce or attenuate vibration inputs if such vibration inputs are along two or more directions. Additionally, such vibration isolation systems may have limited bandwidth.

Thus, the prior art has failed to provide an apparatus for compensating for positioning, pointing and orientation errors caused by deflections of structural members and components of high performance machines or devices and for reducing vibration inputs to a device. As such, the prior art has failed to provide an apparatus for improving the operational performance of high performance machines, devices and components.

An object of the present invention is to provide an apparatus for improving the operational performance of a machine, device or the like which overcomes the problems associated with the prior art.

More specifically, it is an object of the present invention to provide a compensating apparatus coupled to a deflectable member of a machine, device or the like having at least one active-type actuator which is adapted to exert a relatively high corrective moment and/or force and/or torque on the deflectable member so as to compensate for the deflection thereof.

Yet another object of the present invention is to provide a compensating apparatus as aforesaid which is adapted to provide a relatively fast response time.

A still further object of the present invention is to provide a compensating apparatus as aforesaid in which the active-type actuator(s) are at least partially thermally isolated from the deflectable member.

A further object of the present invention is to provide a compensating apparatus having one or more active-type actuators attached to a flexible member at one or more positions to act as a quasi-distributed actuator.

Yet another object of the present invention is to provide a compensating apparatus as aforesaid which may operate in either an open-loop or closed-loop manner.

A still further object of the present invention is to provide an apparatus for reducing vibration inputs to a device in at least two directions.

Yet still another object of the present invention is to provide an apparatus for reducing vibration inputs as aforesaid having at least one module each including a plurality of active-type actuators and adapted to reduce vibration inputs to the device in at least two directions.

Another object of the present invention is to provide an apparatus for reducing vibration inputs as aforesaid in which two or more modules may be easily combined so as to reduce vibration inputs to the device in more than two selected directions.

A yet another object of the present invention is to provide an apparatus for positioning a device having a plurality of modules each including a plurality of active-type actuators.

In accordance with one aspect of the present invention, an apparatus for compensating for deflection of a deflectable member is provided which comprises first and second support members each coupled to the deflectable member, and a plurality of actuator devices each coupled to the first and second support members and arranged at a respective predetermined distance from the deflectable member for exerting a moment on the deflectable member so as to compensate for the deflection of the deflectable member.

In accordance with another aspect of the present invention, an apparatus for compensating for deflection of a deflectable member is provided which comprises a detecting device for detecting at least one of deflection of the deflectable member and a derivative thereof and for producing a detection signal therefrom, a control device for generating a control signal in response to the detection signal, first and second support members each coupled to the deflectable member, and a plurality of actuator devices each coupled to the first and second support members and arranged at a respective predetermined distance from the deflectable member for exerting a moment on the deflectable member in response to the control signal so as to compensate for the deflection of the deflectable member.

In accordance with still another aspect of the present invention, an apparatus for reducing vibration inputs to a device is provided which comprises a detecting device for detecting vibration along at least two directions of the device and for supplying therefrom a vibration signal corresponding to the detected vibration, a control device for generating a control signal in response to the vibration signal, a support member for supporting the device, and a plurality of actuator devices each coupled to the support member for moving the device in response to the control signal so as to reduce the vibration inputs to the device in at least two directions.

In accordance with a still further aspect of the present invention, an apparatus for positioning a device is provided which comprises a plurality of modules each having a support member and a plurality of actuator devices coupled thereto for moving the device in at least one of a translational and rotational direction, the modules being arranged in series with one another so as to move the device in more than one direction so as to position the device.

Other objects, features and advantages according to the present invention will become apparent from the following detailed description of the illustrated embodiments when read in conjunction with the accompanying drawings in which corresponding components are identified by the same reference numerals.

FIG. 1 is a perspective diagram of an apparatus for compensating for deflection of a deflectable member according to an embodiment of the present invention;

FIG. 2 is a perspective diagram of a portion of the apparatus of FIG. 1;

FIG. 3 is a cross-sectional view of the portion of the apparatus of FIG. 2;

FIG. 4A is a diagram of an alternative connecting member utilized in an attachment disc of the portion of the apparatus of FIG. 3;

FIG. 4B is a diagram of a beam which may be utilized in the connecting member of FIG. 4A;

FIG. 5 is a cross-sectional view of the apparatus of FIG. 1 having a modification thereto taken along lines B--B of FIG. 6 and to which reference will be made in explaining the installation of such apparatus;

FIG. 6 is a top view of the apparatus of FIG. 1 as viewed from A--A of FIG. 5 without stiffening Webs;

FIG. 7 is a perspective view illustrating an apparatus for compensating for deflection of a deflectable member in accordance with another embodiment of the present invention;

FIG. 8 is a perspective view illustrating an apparatus for compensating for deflection of a deflectable member in accordance with another embodiment of the present invention;

FIG. 9 is a perspective view of an apparatus for reducing vibration inputs to a device and/or for positioning a device according to another embodiment of the present invention;

FIGS. 10A and 10B are perspective views of modules which may be utilized in the apparatus of FIG. 9;

FIG. 11 is a perspective view of another module which may be utilized in the apparatus of FIG. 10; and

FIG. 12 is a flow diagram to which reference will be made in describing an algorithm which may be utilized by an apparatus of the present invention.

An apparatus for compensating for deflection will be initially described below with reference to FIGS. 1-8 and 12. Thereafter, an apparatus for reducing vibration inputs and/or positioning a device will be described with reference to FIGS. 8-11.

FIG. 1 illustrates a compensating apparatus 10 according to an embodiment of the present invention. Such compensating apparatus 10 is adapted to compensate for deflection of a barrel, rod, or beam 12 which, for example, may be a gun barrel of an armored tank, beams utilized as structural members of manipulators or cranes, machine tools, or the like. As shown compensating attachment device 8 and a servo control device 32. The compensating attachment device 8 includes a first attachment disc 14, a second attachment disc 20, a plurality of actuators 16, a plurality of support columns 18, and a deflection detector 30. Each of the first and second attachment discs 14 and 20, respectively, includes inner and outer rings. That is, the first attachment disc 14 includes a first inner ring 22 and a first outer ring 24, and the second attachment disc 20 includes a second inner ring 26 and a second outer ring 28. The first and second inner rings 22 and 26, respectively, are preferably secured to the beam 12.

The actuators 16 are preferably active-type devices each having a piezoelectric ceramic based material, such as, a lead-zirconate-titanate (PZT) based material such as PZT-5H manufactured by Morgan Matroc Inc. Each such piezoelectric ceramic type device includes a movable portion or activating rod 162 (FIG. 5) which, in response to a control signal supplied from the servo control device 32 as hereinafter more fully described, is adapted to move an amount represented by the control signal in a translational direction D, that is, in a direction substantially parallel to the longitudinal axis of the respective actuator. Further, such piezoelectric ceramic type actuators are relatively rigid, have a relatively low weight and a fast dynamic response and are relatively stable. Furthermore, PZT based materials may produce a relatively large output power due to an inherent relatively large electro-mechanical coupling coefficient. However, such actuators may be relatively brittle and susceptible to fracture failure. As a result, the actuators are preferably preloaded so as to prevent the operation thereof under tensile stress and the actuators are arranged so as to minimize non-axial loading, as hereinafter more fully described.

Polycrystalline ceramics, which are relatively hard and dense, are preferred since the chemical and physical properties associated therewith may be tailored. Further, such polycrystalline ceramics are relatively immune to atmospheric conditions. Furthermore, although the actuators 16 were previously described as having piezoelectric ceramic based material, other types of active materials, such as, Terfornal D, shape memory alloys, electrorheological fluids, polymer biomaterials, magnetorestrictive materials and so forth, may be utilized.

Each of the actuators 16 is respectively coupled to one of the support columns 18. The actuators 16 are further coupled to an outer portion of the first attachment disc 14 such as the first outer ring 24. The support columns 18 are further coupled to an outer portion of the second attachment disc 20, such as the second outer ring 28.

The support columns 18 are adapted to provide the desired axial spacing between the first and second attachment discs 14 and 20, respectively. That is, such desired spacing may be obtained by utilizing different length support columns or by adjusting the length of such support column with shims or similar such devices.

Although the actuators 16 and the support columns 18 are arranged herein as previously described, the present invention is not so limited. That is, the actuators 16 and the support columns 18 may be alternately arranged. For example, all of the actuators 16 may be coupled to the second attachment disc 20, whereupon the support columns 18 are coupled to the first attachment disc 14. As another example, one or more of the actuators 16 may be coupled to the first attachment disc 14 and the remaining actuators coupled to the second attachment disc 20, whereupon the respective support columns 18 are correspondingly coupled to the respective opposite ones of the first and second attachment discs.

Each of the actuators 16 and its respective support column 18 forms an actuator/support column 17 which is located at a distance R from the beam 12 as shown in FIG. 1. Further, each of the actuators/support columns 17 is preferably arranged in the compensating attachment device 8 such that the respective longitudinal axis through the center thereof is substantially parallel to the longitudinal axis through the center of the beam 12.

Although the compensating attachment device 8 shown in FIG. 1 includes four actuators/support columns 17 (although only three are actually shown a fourth is hidden by the beam 12), the present apparatus is not so limited and may include any number of such actuators and support columns. Further, although each of the actuators/support columns 17 include only one actuator, the present invention is not so limited and may include two or more such actuators. Alternatively, each actuator/support column may include more than one type of actuators. For example, an actuator/support column may include a piezoelectric ceramic with Terfonal D based actuator and a hydraulic-type actuator, in which the piezoelectric ceramic actuator is adapted to compensate for relatively high frequency low amplitude displacements while the hydraulic-type actuator is adapted to compensate for relatively low frequency high amplitude displacements.

The deflection detector or sensor 30 is coupled to the beam 12. Such sensor 30 is adapted to sense the deflection of the beam and to supply a signal indicating such beam deflection, by way of a lead 31, to the servo control device 32. Alternatively, the sensor 30 may sense a derivative of the deflection of the barrel 12. For example, the sensor 30 may sense the velocity or rate of change of the beam deflection (first derivative), the acceleration of the beam (second derivative), the jerk (third derivative) and so forth. Accordingly, such sensors may be accelerometers, strain gages and so forth. Further, although only one sensor is illustrated in the compensating apparatus 10, the present invention is not so limited and more than one sensor may be utilized. Furthermore, the sensor(s) 30 need not be coupled to the beam 12, but may alternatively be coupled to other portions of the compensating attachment device 8 such as the first end second attachment discs 14 and 20.

The above-described PZT based material may generate a voltage due to a strain produced by, for example, tensile or compressive forces. Such property enables a PZT based material device to function as both an actuator and a sensor. As a result, the sensor(s) 30 may be omitted and, in place thereof, one or more of the actuators may be utilized to sense the deflection (or a derivative thereof) of the beam 12 and to supply a signal indicating such deflection (or derivative) to the servo control device 32.

The servo control device 32 is adapted to receive an output signal from the sensor 30 and, in response thereto, to provide a control signal(s) to the appropriate one or ones of the actuators 16. More specifically, the servo control device 32 may include a processing device 34 which processes the received signal in accordance with a predetermined algorithm, which may be stored within a memory (not shown) included in the servo control device. The processed signal from the processing device 34 is utilized to form the control signal or signals which are supplied, by way of leads 33, to the one or ones of the actuators 16 which preferably most effectively counteracts the detected deflection. The servo control device 32 could be constructed so as to operate in either a digital or analog manner. As is to be appreciated, if the amount of computations is relatively large or if such computations are relatively complex, then it may be preferred for the servo control device 32 to operate in a digital manner.

The above-mentioned predetermined algorithm may operate as illustrated in FIG. 12. More specifically, as shown therein, signals from the sensor or sensors are read at step S100. Alternatively, if a piezoelectric ceramic-type actuator is used as a sensor(s), then signals from such actuator(s) are read. Thereafter, processing proceeds to step S200 in which the quantity to be controlled is computed or determined from the signals of the sensor(s). For example, the orientation or acceleration of the end or tip of a gun or beam may be computed, the position of the end or tip of the beam, and the derivatives thereof. Processing then proceeds to step S300 in which the appropriate one(s) of the actuators to be activated is determined and in which the computed quantity to be controlled is utilized to compute or generate the appropriate control signal or signals. In such computation, a previous control signal(s) and/or previous sensor data (i.e., historical data) may be utilized to formulate the current control signal. Further, such computation may be performed in an adaptive manner. For example, for vibration damping in a beam, the control system usually provides an actuating moment which is 180 degrees out-of-phase with the beam vibrations. As is to be appreciated, this phase shift may be achieved in numerous ways. Thereafter, processing proceeds to step S400 whereat the generated control signal(s) are supplied to the appropriate one or ones of the actuators.

At least one of the first and second attachment discs 14 and 20, respectively, may include one or more disc plates 40 as illustrated in FIGS. 2 and 3. That is, such attachment disc(s) may include the corresponding inner and outer rings, which are formed of a rigid type material, and may further include at least one, and preferably at least two, disc plates 40 connected therebetween. Such disc plate 40 may be constructed from a relatively thin steel, or appropriate spring-like material, and may be formed so as to have a disc-like shape. Alternatively, the disc plate or connecting member 40 may be configured or formed of a plurality of beams 102 each arranged in a radial manner as, for example, shown in FIG. 4A. Further, such attachment disc(s) may have layers 42 of heat resistant and/or high damping material arranged between one or more adjacent ones of the disc plates as shown, for example, in FIG. 3 and as more fully described hereinafter.

The placement or positioning of the compensating attachment device 8 of the compensating apparatus 10, that is, the first and second attachment discs 14 and 20, the actuators 16 and the support columns 18, may depend upon a number of considerations. For example, such placement may depend on the space available and/or the vibrational modes to be damped. Further, more than one compensating attachment device 8 or compensating apparatus 10 may be coupled to the beam 12, or similar member, each located so as to counteract a vibrational mode of the beam 12. Alternatively, a plurality of compensating attachment devices 8 may be stacked together on the beam 12 in a multi-stage arrangement. In such stacked or multi-stage arrangement, adjacent compensating attachment devices may have a common attachment disc. Additionally, since not all of the vibrational modes may have an appreciable effect on the operational performance or pointing inaccuracies (e.g., the barrel rotation relative to the undeformed longitudinal axis of the gun barrel) of the system or device, the compensating attachment device 8 may be located so as to transfer or spill over the modal energy from one mode to that of another.

FIGS. 5 and 6 illustrate the compensating attachment device 8 and one of the actuators 16 in greater detail. FIG. 5 further illustrates a device for preloading the actuators.

As shown in FIG. 5, the compensating attachment device 8 generally includes first and second attachment discs 14 and 20, friction collars or inner rings 22 and 26, actuator/support column 17 which includes the actuator 16 and the support column 18, and a spherical joint 160. The first and second attachment discs 14 and 20 may include stiffening webs 150 which are generally arranged between an outer portion of the discs and the friction collars. Such stiffening webs, which may be arranged or configured in a manner well known in the art, are adapted to provide a desired amount of stiffness to the first and second attachment discs 14 and 20. The friction collars 22 and 26 are used to couple the respective attachment discs to the beam 12 as hereinafter more fully described.

Each actuator 16 is connected, by use of attachment screws 172, to the support column 18 which, in turn, is connected to the second outer ring 28 of the second attachment disc 20 by use of attachment screws 174. The actuating rod 162 of the actuator 16 is coupled to the first outer ring 24 by the spherical joint 160. As a result, the outer rings of the compensating attachment device are coupled together by the actuator/support column 17. Further, although only one actuator/support column 17 is shown in FIG. 5, the present invention is not so limited and as shown in FIG. 1 more than one such actuator/support column and preferably at least three such actuator/support columns may be utilized.

Each actuator 16 includes the actuating rod 162, preloading springs 164, and a piezo actuator stack or material 168 arranged within an actuator casing 166 as shown in FIG. 5. In operation, each actuator 16 is preloaded by use of the preloading springs 164 and therefore are in compression. Upon being activated, such as by applying a voltage signal thereto, the piezo actuator stack 168 will move up or down along the D direction.

As previously described, the actuators may be preloaded. Such preloading may be accomplished by use of preloading and holding rods 158 and preloading nuts 156 as illustrated in FIGS. 5 and 6. More specifically, one end of each of the preloading and holding rods 158 is respectively threaded into one of threaded holes 159 of the second attachment disc 20, and the other end of each of the preloading and holding rods is inserted into one of through holes 186 located in a respective recess 187 and the preloading nuts 156 are threaded onto such end of the rods 158. By tighting the preloading nuts 156, the spacing between the first and second attachment discs 14 and 20 is reduced, thereby moving the actuating rods 162 further into the actuator casings 166 and preloading the piezo stack actuators 168 of the actuators 16. By selectively tightening the preloading nuts 156, the piezo stack actuators 168 may be preloaded to a desired amount. Although only one preloading and holding rod 158 and preloading nut 156 are shown in FIG. 5, more than one such devices may be utilized in preloading the actuators as, for example, indicated by the arrangement of holes 186 for the preloading and holding rods and the preloading nuts as shown in FIG. 6, which illustrates a view A--A of the compensating attachment device 8 without the stiffening webs 150.

As is to be appreciated, upon preloading the actuators 16 as previously described, the preloading and holding rods 158 and the preloading nuts 156 are removed from the compensating attachment device 8.

Further, as previously described, the piezoelectric ceramic type actuators 16 are preferably arranged so as to minimize or prevent non-axial loading or bending loading thereon. More specifically, the actuators 16 may be coupled to the first attachment disc 14 by way of the spherical joint 160, which may be of a ball and socket type. Such ball and socket arrangement may include a ball 161 coupled to the upper portion of the actuating rod 162 and a socket or mating member 163 arranged in the lower surface of the first outer ring 24 of the first attachment disc 14. In such arrangement, the ball 161 is inserted within the socket 163 so as to pivotably support the ball and the members attached thereto. Alternatively, the spherical joint 160 may be a flexure joint which permits a desired rotational range with minimal resistance or other similar such devices.

The operation of the compensating apparatus 10 will now be described.

Upon a deflection of the beam 12, such as due to the firing of the gun barrel or an external distrubance or the like, the sensor 30 detects such deflection or a derivative thereof and supplies a signal corresponding thereto to the servo control device 32 by way of the leads 31. The processing device 34 of the servo control device 32 processes the received signal in accordance with the algorithm previously stored in the memory thereof and, as a result, the servo control device generates a control signal which is supplied by way of the leads 33 to the appropriate one or ones of the actuators 16.

As an example, suppose that the beam 12 has deflected to the left (as viewed facing FIG. 1). In this situation, the sensor 30 detects such deflection or a derivative thereof and supplies a corresponding signal to the servo control device 32, whereupon a corresponding control signal is generated and supplied therefrom. Since the beam 12 has deflected to the left, the control signal only activates actuator 16a so as to elongate the same. Alternatively, a control signal may be supplied to actuator 16a so as to elongate the same and to actuator 16b so as to shorten the same. As a result, the movable portion or actuating rod 162 (FIG. 5) of the actuators 16a and/or 16b moves an amount corresponding to the detected beam deflection (or a derivative thereof) and its history and/or the history of the control signals in a direction D which is substantially parallel to the longitudinal axes of the actuators 16a and 16b (and to the longitudinal axis of the beam 12) so as to cause a force to be exerted on the corresponding portion of the first and second attachment discs 14 and 20. Such force causes a moment equal to a product of the force and the distance R (i.e., force.times.distance R), to be exerted on the beam 12. (As is to be appreciated, depending upon the configuration, a force or a torque may be applied.) As a result, the beam 12 is moved in a direction substantially opposite to that of the deflection so as to compensate for such deflection and return the beam to its original position and/or point a tip of the beam to its undeformed direction, such as in the case of a gun barrel.

In the above-described example, since the compensating apparatus 10 includes four actuators 16, only either actuator 16a and/or actuator 16b is activated to compensate for the deflection of the beam 12 to the left. However, as is to be appreciated, if the compensating apparatus 10 includes a different number of actuators or if the deflection of the beam 12 is in a direction which may not be readily compensated by only either actuators 16a and/or 16b or if the actuators are arranged differently from that shown in FIG. 1, then a different combination of actuators may be activated to compensate for such deflection.

To activate the appropriate one or ones of the actuators 16, a respective control signal may only be supplied to each of the desired actuators. In this situation, the actuators not receiving a respective control signal are not activated. Alternatively, the control signal may be supplied to each of the actuators, that is, both the actuators desired to be activated and those not so desired. However, in this latter situation, the control signal identifies the desired actuator or actuators. For example, the control signal may contain an identification code which identifies the desired actuator(s). In this situation, each actuator has a respective identification code associated therewith and includes a device (not shown) for decoding the coded control signal and determining if the decoded identification code included therein matches that of the respective actuator whereupon, if a match is determined, the control signal is passed to the respective actuator so as to activate the same, and if a non-match condition exists, the control signal is not passed to the respective actuator and accordingly such actuator is not activated.

As is to be appreciated, if the beam 12 is vibrating, for example, in a periodic motion, the compensating apparatus 10 is adapted to counteract or compensate for such vibration in a manner similar to that described above. That is, the compensating apparatus 10 and, in particular, the actuators 16 and the servo control device 32, have a relatively fast response time. As a result, the compensating apparatus 10 permits a counteraction or compensation of the beam 12 to periodically occur. Alternatively, the compensating apparatus 10 may continuously compensate for the deflections of the beam 12.

In a similar manner, the piezo stacks 168 of the actuators 16 may be activated to achieve positioning or pointing of the beam 12. As an example, during the firing of a gun, the compensating attachment device(s) may be arranged on the gun barrel and controlled so as to enable the gun barrel to be pointed in a desired direction at the time of firing such gun.

As previously described, at least one of the first and second attachment discs 14 and 20 may include the disc plates 40 (FIG. 3) having a disc or beam shape and constructed of relatively thin steel. Such arrangement may minimize adverse effects from movement of the beam 12, such as may occur in the case of a gun barrel in which the thermal effects caused by the firing of the gun may cause the gun barrel to move axially in a cyclic manner. More specifically, as shown in FIG. 3 and as previously described, the inner ring 22 is rigidly attached to the beam 12. During movement of the beam 12 which may occur during thermal expansion thereof, the inner ring 22 can move a relatively small amount in the longitudinal direction of the beam 12 relative to the outer ring 24 without a significant amount of resistance from the disc plates 40. Such axial displacement of the inner ring 22 relative to the outer ring 24 may occur since the disc plates 40 are merely subjected to bending loads to which they offer relatively small resistance.

Although the attachment disc illustrated in FIG. 3 may permit axial displacement of the inner ring 22 as previously described, such disc provides a relatively high resistance to movements which may occur in performing the compensating operation. Such movements may include rotations of the inner ring 22 relative to the outer ring 24 about axes which are perpendicular to the longitudinal axis of the beam 12. These rotations may cause radial displacements in the disc plates 40 (or axial displacements in the beams 102 if beams are used as the plates 40) to which the disc plates (beams) offer a relatively high resistance. If additional axial compliance is desired, beam members 102 having narrow end portions 104 as shown in FIG. 4B may be utilized.

Further, the positioning of the actuators 16 at a distance R (FIG. 1), reduces or minimizes the heat transfer from the beam 12 to the actuators. As is to be appreciated, the beam 12, which may be a gun barrel as previously described, may reach relatively high temperatures as for example during a firing operation. However, the distance from the beam 12 to the actuator 16, along with the heat resistant material 42 of the attachment disc, provides a relatively high thermal resistance which reduces the heat transfer from the beam 12 to the actuators. As a result, the actuators 16, which as previously described may be the piezoelectric ceramic-type actuators whose performance may be adversely affected by exposure to relatively high temperatures, are at least partially thermally isolated from the beam 12 and accordingly may not be exposed to such relatively high temperatures. Accordingly, the performance of the actuators 16 may not be adversely affected. When required, additional radiational thermal resistance can be provided in the form of radiation shields between the-beam and the actuators (e.g., such shields may be mirrored-like surface plates such as polished aluminum).

Furthermore, the arrangement of the attachment disc of FIG. 3 having the damping material as previously described, reduces vibration of the beam 12 so as to act as a passive damper. Further, such arrangement reduces the vibration of flexible discs or beam elements of the attachment discs and increases its resonant frequency.

The disc plates 40 (FIGS. 2 and 3) and beams 102 (FIGS. 4A and 4B) are preferably designed so as to minimize buckling of such disc plates and beams. Such design techniques are well known and, as such, will not be described herein.

The compensating attachment device 8 may be configured to enable easy attachment to and removal from the beam 12. For example, each compensating attachment device 8 may include more than one section or portions, such as the two portions 180 and 182 as shown in FIG. 6. More specifically, the portions 180 and 182 respectively include friction collar portions 152 and 153 which form the respective inner ring and which are arranged around the beam 12 and secured thereto by use of a plurality of collar bolts 154. That is, the collar bolts 154 are inserted through clearance holes (not shown) located in the friction collar portion 153 adjacent to recess portions 155 into threaded holes 258 (FIG. 5) in the friction collar portion 152. Further, grooved sleeves may be utilized to provide an accurate and rigid mounting of the compensating attachment device to the beam 12. Alternatively, the compensating attachment device may be secured by friction and/or through adhesives and/or brazing and/or welding and the like when the anticipated vibration levels and frequency permits.

In addition to compensating for the deflections of a barrel or beam, the present invention may be utilized for compensating for the deflections of other shaped or types of members, such as a beam or column 201 by utilizing a compensating apparatus 200 as illustrated in FIG. 7. As shown therein, the compensating apparatus 200 generally includes one or more compensating attachment devices 208 and/or 209 and a servo control device 232. The compensating attachment devices 208 and 209 may be coupled to the beam 200 by use of screws, rivets, and the like (not shown) or alternatively may be welded, bonded or similarly secured thereto. The compensating attachment device 208 includes a first end member 214, a middle or intermediate member 219, and a second end member 220 which are secured together and arranged in a U-shape manner as shown in FIG. 7. An actuator 216, which may be similar to the actuator 16, is coupled to a support member 217 which, in turn, may be similar to support column 18. The actuator 216 and the support member 217 form an actuator/support member 221 which is arranged between the first and second end members 214 and 220, respectively. The compensating attachment device 209 is substantially similar to the compensating attachment device 208 except that the device 209 does not include the middle member 219. The servo control device includes a processing device 234 and is adapted to receive a signal corresponding to a deflection or the resulting positioning or pointing error of the beam 201 or a derivative thereof from a sensor(s) 230 by way of a lead(s) 231 and process such received signal so as to produce a control signal which is supplied to the appropriate one or ones of the actuators 216 by way of leads 233. Such operation of the servo control device 232 is substantially similar to that of the servo control device 32 and, accordingly will not be further described herein.

Thus, upon deflection or vibration of the beam 201, the appropriate one(s) of the actuators 216 are activated which causes a force to be exerted on the respective one(s) of the first and second end plates 214 and 220, respectively. As a result, a moment is exerted on the beam 201 which counteracts or compensates for the deflection or motion of the beam 201.

As previously described, the compensating apparatus 200 may include one or more compensating attachment devices (such as one or more of either compensating devices 208 or 209). Further, such compensating attachment devices may be arranged in one or more groups (with any number of such compensating attachment devices being in each group) in any desired manner. Furthermore, such devices may be arranged so as to transfer modal energy from one vibration mode to another, or alternatively to damp the energy of a selected number of such modes. Since not all of the vibration modes may have a significant contribution to the motion of the beam or the resulting inaccuracies caused thereby, the compensating attachment device(s) may be located on the beam 201 so as to counteract a desired one or ones of vibration modes.

Furthermore, a plurality of compensating attachment devices may be coupled together in a series manner on the beam 201. Alternatively, a multi-stage compensating apparatus 300 as shown in FIG. 8 may be utilized. Such compensating apparatus 300 includes a supporting member 301 having a plurality of supporting ends 302 and a base member 304, and a plurality of actuators 316 arranged between adjacent ones of the supporting ends. Each such actuator and its respective supporting ends forms a single stage, such as one of stages A, B, . . . and so forth. The compensating apparatus 300 is secured to the beam 201 (FIG. 7), or other member, by use of adhesive, screws, rivots or the like and acts as a quasi-distributed actuator for the beam member. In this situation, the deflection (and/or orientation and/or pointing and/or positioning and/or derivatives thereof) of the beam is sensed by utilizing at least one sensor and, preferably, at least one sensor for each actuator is utilized. Such sensing may be accomplished by measuring the change in length or strain of the respective actuator and/or force and/or a strain at the base member 304 or force at the support ends 302 of the actuator 316. Further, such sensors may be placed at any desired locations. A quasi-distributed actuator and sensor is then obtained. Although not shown in FIG. 8, the actuators may be coupled to and controlled by a servo control device such as the servo control device 32 or 232. Accordingly, as a result of a detected deflection or derivative thereof, the appropriate one(s) of the actuators 316 may be activated so as to cause a force to be exerted on the corresponding supporting ends which causes a moment to be exerted on the beam thereby counteracting or compensating for the deflection of the beam in a manner similar to that previously described with reference to the compensating apparatus 200. Further, more than one multi-stage compensating apparatus 300 may be utilized on the beam 12. Each of such multi-stage compensating apparatus may have any number of stages.

Thus, the above-described compensating attachment devices 8, 208 and 209 and the multi-stage compensating device of FIG. 8 may be arranged or located directly on a flexible structure or component of a high performance machine or device. As a result of such location of the present compensating devices, problems due to non-collocation between the compensating device and the portion of the high performance machine which is desired to be pointed, positioned or orientated and problems due to non-linearities (such as stiction, friction, backlash, non-linear elasticity due to drive train, and so forth) therebetween may be avoided. Further, such present compensating devices may be arranged so as to counteract a vibration mode or modes of the flexible structure or component or to transfer the modal energy from one mode to that of another.

Although the above embodiments have been described as including a servo control device thereby enabling the respective compensating apparatus to operate in a closed loop manner, the present invention is not so limited. That is, such apparatus may operate without a servo control device in an open loop manner. As an example, consider the situation wherein the input disturbances or deflections are periodic and the pertinent values, such as amplitude and frequency, of such disturbances or deflections are known. In this situation, a feedforward or a predetermined compensation control signal can be applied to the appropriate one or ones of the actuators in an open loop manner so as to compensate for such deflection. Further, such open loop driven apparatus may be utilized to deflect or move a device so as to damp or excite the device in a predetermined manner.

Other embodiments of the present invention will now be described with reference to FIGS. 9-11. Such embodiments may be utilized to reduce vibration inputs to a device and/or to accurately position a device.

A vibration isolation apparatus 400 is illustrated in FIG. 9. As shown therein, such vibration isolation apparatus generally includes a servo control device 432 and modules 403 and 405.

The module 403, as illustrated in FIG. 10A, includes an upper plate 404, a plurality of actuators 416, and a base plate 402. Each of the actuators 416, which may be similar to the previously described actuators 16 (FIG. 1), are securely coupled between the upper plate 404 and the base plate 402. Further, the actuators 416 are arranged such that a movable portion thereof, such as the actuating rod 162 (FIG. 5), is movable along a direction Z (FIG. 9) which is preferably perpendicular to the upper plate 404 and the base plate 402. Preferably, at least three actuators 416 are utilized, although a lesser number could also be used. The upper plate 404 includes a plurality of holes 406, which may be threaded holes. The base plate 402 includes a plurality of holes (not shown) which may correspond to holes 414 (FIG. 11). The device (not shown) which is desired to be vibration isolated is secured to upper or top surface of the upper plate 404 by use of the holes 406. The other end of the vibration isolation apparatus is grounded or attached to the base of the machine using the apparatus or such similar location

Although the upper plate 404 and the base plate 402 are preferably located relatively close together, the present invention is not so limited. That is, support columns, similar to the support columns 18 (FIG. 1), may be utilized when additional spacing between the upper and base plates is desired. Alternatively, an actuator 417 which may be a motor, such as a linear motor, or a hydraulic, pneumatic or electric actuator, or other similar type of linear actuator may be utilized. That is, as illustrated in FIG. 10B, one such actuator 417 is respectively coupled to the each of the actuators 416. Such arrangement of actuators 416 and 417 may increase the permissible range of displacement of the module 403 and/or may more easily provide for movements having relatively low frequency high amplitude displacements and high frequency low amplitude displacements, in a manner similar to that previously described with reference to the actuator/support column 17 of FIG. 1.

The vibration isolation apparatus 400 may be utilized for isolating a platform, such as, a bed or cot for transporting a patient in an ambulance so as to prevent further injuries during the transporting of the patient, payload platform for rockets and spacecrafts particularly those under micro-gravity constraints from accelerations and/or shocks, and a mounting base for a gun turret system from variations in terrain and structural vibrations, and so forth.

By activating one or ones of the actuators 416, the module 403 may provide axial displacements, that is, displacements along the Z direction, and/or rotational movements about axes perpendicular to it, such as the X and Y axes.

The module 405, as illustrated in FIG. 11, includes a base plate 408, side supports 410, a plurality of actuators 436, and an actuated block 412. As shown in FIG. 11, the actuators 436 are arranged in two groups. That is, two of the actuators 436 are arranged between one of the side supports 410 and the actuated block 412, and two other actuators are arranged between the other of the side supports and the actuated block 412. Further, each of the actuators 436 are arranged such that a movable or active portion thereof is movable along a F direction. The actuated block may include a plurality of holes 414, such as threaded holes, which may be utilized to secure the module 405 to the base plate 402 of the module 403 or to the device desired to be vibration isolated. The side supports 410 are securely fastened to the base plate 408. Alternatively, the side supports 410 and the base plate 408 may be formed as a single unit.

By activating one or ones of the actuators 436, the module 405 may provide rotational movements and/or lateral movements or displacements. More specifically, by activating diagonal ones of the actuators 436, the module may be rotationally moved about an axis through the center of the module, that is, the Z axis. On the other hand, by similarly activating the actuators 436 in at least one of the groups, a displacement or movement along the F direction is obtained.

Referring back to FIG. 9, the servo control device 432 includes a processing device 434 which operates in a manner similar to that of the servo control device 32 (FIG. 1). That is, the vibration input to the device (not shown) mounted on the upper plate 404 is sensed by a sensor 430 and a signal corresponding thereto is supplied therefrom to the servo control device 432 by way of a lead 431. The processing device 434 processes the received signal in accordance with a predetermined algorithm which may be similar to that previously described with reference to FIG. 12 and, based upon the results therefrom, a control signal is supplied from the servo control device to the appropriate one(s) of the actuators 416 and 436 (FIG. 11) by way of leads 433. As a result, the respective one or ones of the modules 403 and 405 are caused to move or rotate so as to counteract or compensate for the detected vibration input.

As is to be appreciated, the vibration isolation apparatus 400 permits five degrees-of-freedom, that is, the module 403 permits three degrees-of-freedom and the module 405 permits two degrees-of-freedom. More specifically, the module 403 permits movement in the Z direction by similarly activating each of the actuators 416, and permits rotation about either of the X or Y directions by activating appropriate one(s) of the activators 416. The module 405 permits rotation about the Z direction by activating diagonal one(s) of the actuators 436, and permits movement along the F direction (which may correspond to either of the X or Y axes) by similarly activating at least one group of the actuators 436, as previously described.

Further, although the vibration isolation apparatus 400 includes two modules 403 and 405 as previously described, the present invention is not so limited. That is, the present vibration isolation apparatus may include any number of such modules. As is to be appreciated, by selectively choosing one or more modules, a vibration isolation apparatus may be provided which can permit any number of degrees-of-freedom and/or can provide increased lateral and/or axial and/or rotational movement. For example, by adding another module 405 to the apparatus 400 of FIG. 9, which is rotated 90 degrees about the Z direction relative to the other module 405, enables six degrees-of-freedom. Further, by adding another module to this arrangement, increased movements along the X, Y and/or Z directions may be obtained. That is, suppose it is desired to permit a movement of 2N along the Z direction and the actuators 416 have a total travel of only N. In this situation, two of modules 403 may be utilized, each permitting a movement of N for a total movement of 2N. As another example, by utilizing two of the modules 405, in which one is rotated 90 degrees about the Z direction relative to the other, enables movements in the X and Y directions and further permits an increased allowable range of rotation about the Z direction.

The above-described vibration isolation apparatus may be utilized to provide micro-positioning of a device attached thereto at a relatively high bandwidth. Such apparatus may accommodate large motions with a high degree of accuracy to achieve micro-positioning. In this situation, the vibration closed loop feedback arrangement in the apparatus 400 of FIG. 9 is not utilized and such apparatus is merely adjusted to the desired position by activating the appropriate one or ones of the actuators 416 and/or 436. Such micro-positioning may be performed in conjunction with vibration isolation and/or damping. For example, in the situation of a gun turret system, this apparatus may not only be used as a vibration isolation apparatus as previously described, but may also be simultaneously used as a micro-positioner to correct orientation and/or pointing of the gun barrel of the gun turret system.

Accordingly, the present invention provides an apparatus for compensating for deflections of a member so as to compensate for pointing, positional and orientational inaccuracies or errors. Further, the present invention provides an apparatus for isolating a device from externally generated vibrations. Such present apparatus are highly accurate and relatively stable, and have a relatively fast response time and a relatively large bandwidth so as to accommodate a large range of motion. Furthermore, the present invention provides an apparatus for positioning a device with a relatively high degree of accuracy throughout a large range of motion.

Although illustrative embodiments of the present invention and modifications thereof have been described in detail herein, it is to be understood that this invention is not limited to these precise embodiments and modifications, and that other modifications and variations may be affected therein by one skilled in the art without departing from the scope and spirit of the invention as defined by the appended claims.