Position accuracy is influenced by imperfections in the position feedback system (such as a linear encoder), drive mechanism, guidance errors of the bearings, and deflection of the structure to which the stage is mounted. For more information, read also Straightness and Flatness of Air Bearings.

Position accuracy is also influenced by the location in space relative to the stage where the user’s payload or sensor is located. This location is called the “point of interest”, and the distance between this point and the stage is called an offset. Abbe error is the positioning error resulting from angular error motion of a stage’s moving part and the size of the offset. The greater the offset distance between the stage and the user’s point of interest, the greater the Abbe error. In the diagram shown below, the amount of pitch error from the stage combined with the length of the Abbe offset “h” will determine the Abbe error.

Under closed loop servo control, the stage is moved in fixed increments (typically 10mm – 50mm per step), and a measurement is taken at each point. The stage is moved through its full length of travel in both directions for multiple passes. The collected data is plotted and the overall accuracy is calculated. The accuracy and repeatability results are typically reported in microns.

This test is performed using the Renishaw XR20-W rotary axis calibrator mounted to the rotating stage table. The XR20-W consists of an integrated angular retroreflector mounted on a precision servo-controlled axis. The angular position of this axis, and the optics relative to the main body housing, is controlled by a very high accuracy encoder system with the scale directly machined onto the main bearing. The angular interferometer optic is placed at the end of the stage and is held stationary. The angular optic setup creates two beam paths. As the stage rotates, the XR20-W counter-rotates by the same amount. The angular error is calculated based residual rotation measures by the laser.  

In the same way that the linear accuracy data is collected, the stage is moved in fixed increments (typically 5° - 30° per step), and a measurement is taken at each point. The stage is moved through its full range of travel, in both directions, for multiple passes. The data that is collected is plotted and the overall errors are calculated. The results are typically reported in arc-seconds or microradians.

Using data from the position error measurements, a correction table can be generated and loaded into the ACS motion controller. The errors are corrected by changing the motion profile on the fly, according to the correction map, via a controller feature called Dynamic Error Compensation.

Shown below are typical position error plots for PIglide air bearing stages taken before and after the implementation of Dynamic Error Compensation using an ACS SPiiPlus Motion Controller. The final results that can be obtained with error compensation are limited only by the repeatability performance of the stage.

References:

• http://www.renishaw.com/en/xr20-w-rotary-axis-calibrator–15763
• https://www.zygo.com/library/papers/ISBN1439854815_Ch4.pdf

• High Performance Motion Control – Systems Approach Provides Nanometer Precision for Industrial Applications