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Publication numberUS20060213362 A1
Publication typeApplication
Application numberUS 10/566,765
PCT numberPCT/IB2004/051316
Publication dateSep 28, 2006
Filing dateJul 28, 2004
Priority dateAug 4, 2003
Also published asCN1829948A, EP1654605A1, WO2005013027A1
Publication number10566765, 566765, PCT/2004/51316, PCT/IB/2004/051316, PCT/IB/2004/51316, PCT/IB/4/051316, PCT/IB/4/51316, PCT/IB2004/051316, PCT/IB2004/51316, PCT/IB2004051316, PCT/IB200451316, PCT/IB4/051316, PCT/IB4/51316, PCT/IB4051316, PCT/IB451316, US 2006/0213362 A1, US 2006/213362 A1, US 20060213362 A1, US 20060213362A1, US 2006213362 A1, US 2006213362A1, US-A1-20060213362, US-A1-2006213362, US2006/0213362A1, US2006/213362A1, US20060213362 A1, US20060213362A1, US2006213362 A1, US2006213362A1
InventorsMarcel Heertjes, Michael Vervoordeldonk
Original AssigneeKoninklijke Philips Electronics N.V.
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Lorentz motor control system for a payload
US 20060213362 A1
Abstract
Control arrangement for and method of controlling a plurality of Lorenz motors (1, 2) actuating a payload (4) where the payload has a center of gravity (12). Height signals (z1, z2) are received from sensors sensing heights of said payload. At least one rotation angle of the center of gravity about a horizontal axis is calculated from these height signals (z1, z2) and from this at least one rotation angle control signals (C1, C2) for the Lorenz motors (1, 2) are calculated such that a predetermined rotational stiffness for supporting the payload (4) is achieved.
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Claims(5)
1. Control arrangement for controlling a plurality of Lorenz motors (1, 2) actuating a payload (4), the payload having a center of gravity (12), the control arrangement comprising a controller (8) for receiving height signals (z1, z2) from sensors sensing heights of said payload and for calculating control signals (C1, C2) for said Lorenz motors from said height signals, characterized in that said controller (8) is arranged to calculate from these height signals (z1, z2) at least one rotation angle of the center of gravity about a horizontal axis and calculate from this at least one rotation angle said control signals (C1, C2) for said Lorenz motors (1, 2) such that a predetermined rotational stiffness for supporting said payload (4) is achieved.
2. Control arrangement according to claim 1, wherein said controller (8) is arranged to control three or four Lorenz motors.
3. Method of controlling a plurality of Lorenz motors (1, 2) actuating a payload (4), the payload having a center of gravity (12), comprising receiving height signals (z1, z2) from sensors sensing heights of said payload and calculating control signals (C1, C2) for said Lorenz motors from said height signals, characterized by calculating from these height signals (z1, z2) at least one rotation angle of the center of gravity about a horizontal axis and calculating from this at least one rotation angle said control signals (C1, C2) for said Lorenz motors (1, 2) such that a predetermined rotational stiffness for supporting said payload (4) is achieved.
4. Computer program product comprising instructions and data to be loaded by a computer, and after being loaded allowing the computer to perform the method according to claim 3.
5. Data carrier comprising a computer program product according to claim 4.
Description

The invention relates to a control arrangement for controlling a plurality of Lorenz motors actuating a payload, the payload having a center of gravity, the control arrangement comprising a controller for receiving height signals from sensors sensing heights of said payload and for calculating control signals for said Lorenz motors from said height signals.

It is known to support a payload with a plurality of, e.g. three or four, mounts. The mounts may each comprise an airmount and one or two Lorenz motors. Instead of airmounts, other type of “springs” may be used The payload has a center of gravity that may or may not be above the airmounts. In dependence on the design of the airmounts, the critical height of the center of gravity of the payload where the payload gets unbalanced may be lower or higher. Therefore, strict rules apply with respect to allowable upper limit of the height of the center of gravity above the airmounts. As is known to persons skilled in the art, the softer the airmounts or the smaller the base, i.e., distance between the airmounts, the lower the critical height. And, the higher the actual height of the center of gravity of the payload, the higher the airmounts or the greater the distance between the airmounts must be designed.

Another way to cope with this problem, as is also known from the prior art, is to apply some additional horizontal springs engaging side surfaces of the payload and walls opposite to the side surfaces. These springs increase rotational Oddness of the payload and keep it from instability with respect to tilt

However, there may be locations where there is little room building in additional horizontal springs and an additional frame therefore. Moreover, this maybe an expensive solution. When one wishes to replace existing airmounts by softer airmounts the base may already be fixed, etc.

A typical example is a suspension of an electron microscope or (parts) of a lithographic apparatus. For improved floor vibration isolation, softer airmounts are preferred. The height of the center of gravity of such an apparatus requires airmounts to be located higher or to be located further apart from one another. However, increasing the heights of the airmounts may form obstacles to an operator of the apparatus, and increasing the base may not be allowable, e.g., due to a conflict with an electronics cabinet or to commercial reasons.

Therefore, it is an object of the invention to provide an improved control of the mounts such that the sensitivity of a payload to gravitational instability is reduced without substantially increasing vertical stiffness.

To that end, the invention provides a control arrangement as defined at the outset, characterized in that said controller is arranged to calculate from these height signals at least one rotation angle of the center of gravity about a horizontal axis and calculate from this at least one rotation angle said control signals for said Lorenz motors such that a predetermined rotational stiffness for supporting said payload is achieved.

Thus a multiple-input-multiple-output controller is applied that calculates at least one rotation component of the center of gravity of the payload and controls the Lorenz motors to provide additional rotational stiffness without increase of vertical stress. It is possible to improve the gravitational stability. The payload may have a higher center of gravity than in prior art systems, without the system becoming unstable.

In an embodiment, the invention relates to a method of controlling a plurality of Lorenz motors actuating a payload, the payload having a center of gravity, comprising receiving height signals from sensors sensing heights of said payload and calculating control signals for said Lorenz motors from said height signals, characterized by calculating from these height signals at least one rotation angle of the center of gravity about a horizontal axis and calculating from this at least one rotation angle said control signals for said Lorenz motors such that a predetermined rotational stiffness for supporting said payload is achieved.

Moreover, the invention relates to a computer program product comprising instructions and data to be loaded by a computer, and after being loaded allowing the computer to perform the method as defined above.

Finally, the invention relates to a data carrier comprising such a computer program product.

The invention will be explained with reference to some drawings that are only intended to illustrate the invention and not to limit its scope. The scope is defined by the annexed claims and their technical equivalents only.

FIG. 1 shows a payload supported by a plurality of mounts;

FIG. 2 shows a general, schematic block diagram of a multiple-input-multiple output control arrangement for the Lorenz motors.

FIG. 1 shows a payload 4 supported by a plurality of mounts. The payload 4 has a center of gravity 12. The mounts comprise airmounts 15, 16, and Lorenz motors 1, 2. For sake of simplicity, FIG. 1 shows two airmounts 15, 16 and two Lorenz motors 1, 2, however, there will mostly be three or four airmounts and at least one Lorenz motor per airmount The airmounts support the payload 4 whereas the Lorenz motors 1, 2 are actuated to apply forces as part of a control concept to create vertical servo stiffness and/or servo damping. Additionally, there may be one or more extra Lorenz motors arranged to apply horizontal forces as part of a control concept to create horizontal servo stiffness and/or servo damping, as is evident to persons skilled in the art. These latter Lorenz motors are not of interest to the present invention.

The distance between the Lorenz motors is l.

An x, y, z-axes system is defined having an origin at a predetermined location. A rotation φ is defined as a rotation about the x-axis. The center of gravity 12 is at height h above the Lorenz motors 1, 2.

FIG. 2 shows a control arrangement for control of the two Lorenz motors 1, 2. The control arrangement shown comprises two sensors 6, 7 for sensing heights z1, z2, respectively. The sensors 6, 7 feed back height signals z1, z2 to a controller 8. The controller 8 calculates control signals C1, C2 from these height signals z1, z2 for the Lorenz motors 1, 2, respectively. FIG. 2 is simplified in the sense that it shows only two sensors 6, 7, and two input signals and two output signals for the controller 8. In most cases, three z-sensors will be used that provide information as to z, q and a rotation around the y-axis.

For the two Lorenz motors embodiment shown in FIG. 1, the following control concept performed by controller 8 is proposed.

derive angle φ from z1, and z2, e.g., from (z1−z2)/l

calculate a torque T from angle φ: T=−kφ, where k is a measure of rotational stiffness in Nm/rad

calculate control signals C1, C2 from torque T: C1=−T/a, and C2=T/b, where a and b are constants the values of which can be chosen freely but have equal sign.

In an embodiment, a low pass filter may be applied. Then, the torque T is calculated from T=−k.φ.H1p, where H1p is the low pass filter transfer function.

In a 3 dimensional environment, the general idea is as follows: feed back the height position signals from all height sensors used to the controller 8, calculate rotation angles about the x-axis and the y-axis from these height position signals, calculate control signals for all Lorenz motors used from these rotation angles such that a predetermined rotational stiffness is achieved, without substantially creating additional vertical stiffness.

As is evident to persons skilled in the art, there may be applied other types of mounts than airmounts, e.g., springs. Moreover, When the airmounts 15, 16 are applied, they will be provided with supply lines to supply air to them. Then, air is supplied by suitable pressure sources also controlled by the controller 8. It is to be understood that the controller 8 is shown as one single unit. However, the controller 8 may be implemented by multiple computers acting together, e.g., in a master slave configuration. The suitable software may distributed via data carriers or any other suitable way. Moreover, the controller for the pneumatics part may be independent from the controller for the Lorenz motors.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US7816875Jan 24, 2008Oct 19, 2010Viking Access Systems, LlcHigh torque gearless actuation at low speeds for swing gate, roll-up gate, slide gate, and vehicular barrier operators
US7816879Feb 19, 2008Oct 19, 2010Viking Access Systems, LlcHigh torque movable barrier actuation at low speeds utilizing a hub motor
Classifications
U.S. Classification91/6
International ClassificationF01B25/02, F16F15/00, G03F7/20, F16F7/10, F16F15/03
Cooperative ClassificationG03F7/70758, G03F7/709, G03F7/70816, F16F7/1011, F16F15/005, F16F15/03
European ClassificationG03F7/70P2B, G03F7/70P6F, G03F7/70N8, F16F15/03, F16F7/10A2, F16F15/00P
Legal Events
DateCodeEventDescription
Jan 31, 2006ASAssignment
Owner name: KONINKLIJKE PHILIPS ELECTRONICS, N.V., NETHERLANDS
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:HEERTJES, MARCEL FRANCOIS;VERVOORDELDONK, MICHAEL JOHANNES;REEL/FRAME:017511/0317
Effective date: 20050226