The present disclosure relates to evaluation of a distance measuring device. Such a distance measuring device might be an interferometer (IFM) or an absolute distance meter (ADM). Such a distance measuring device may be a stand-alone distance meter, or it may be incorporated into another device such as a laser tracker, total station, or time-of-flight (TOF) scanner.
A laser tracker is a particular type of coordinate-measuring device that tracks the retroreflector target with one or more beams it emits, which may include light from a laser or non-laser light source. Coordinate-measuring devices closely related to the laser tracker are the TOF scanner and the total station. The TOF scanner steps one or more beams of light to points on a surface. It picks up light reflected from the surface and in response determines a distance and two angles to each surface point. A total station is a 3D measuring device most often used in surveying applications. It may be used to measure the coordinates of a diffusely scattering target or a retroreflective target. Hereinafter, the term laser tracker is used in a broad sense to include laser scanners and total stations and to include dimensional measuring devices that emit laser or non-laser light.
In many cases, a laser tracker sends a beam of light to a retroreflector target. A common type of retroreflector target is the spherically mounted retroreflector (SMR), which comprises a cube-corner retroreflector embedded within a metal sphere. The cube-corner retroreflector comprises three mutually perpendicular mirrors. The vertex, which is the common point of intersection of the three mirrors, is located at the center of the sphere. Because of this placement of the cube corner within the sphere, the perpendicular distance from the vertex to any surface of the SMR rests remains constant, even as the SMR is rotated. Consequently, the laser tracker can measure the 3D coordinates of a surface-under-test by following the position of an SMR as it is moved over the surface-under-test. Stating this another way, the laser tracker needs to measure only three degrees of freedom (one radial distance and two angles) to fully characterize the 3D coordinates of a surface.
One type of laser tracker contains only an interferometer (IFM) without an absolute distance meter (ADM). If an object blocks the path of the laser beam from one of these trackers, the IFM loses its distance reference. The operator must then track the retroreflector to a known location to reset to a reference distance before continuing the measurement. A way around this limitation is to put an ADM in the tracker. The ADM can measure distance in a point-and-shoot manner. Some laser trackers contain only an ADM without an interferometer.
A gimbal mechanism within the laser tracker may be used to direct a laser beam from the tracker to the SMR. Part of the light retroreflected by the SMR enters the laser tracker and passes onto a position detector. A control system within the laser tracker uses position of the light on the position detector to adjust the rotation angles of the mechanical axes of the laser tracker to keep the beam of light centered on the SMR. In this way, the tracker is able to follow (track) a moving SMR.
Angle measuring devices such as angular encoders are attached to the mechanical axes of the tracker. The one distance measurement and two angle measurements of the laser tracker are sufficient to completely specify a three-dimensional location of the SMR.
Today laser trackers measure to relatively long distances. For laser trackers used with SMRs, a typical maximum measurement range is 80 meters. For TOF scanners or total stations that directly measure surfaces with a beam of light, ranges may extend to several hundred meters or further.
It is often necessary to determine the accuracy of laser trackers to within a few micrometers over its entire measurement range. It is often the case that laboratory space is not available to evaluate the performance of a distance meter within a laser tracker over the tracker's full measurement range. A way is needed to enable relatively accurate evaluation of distance meters over the full measurement range of the distance meters, even when that much laboratory space is not available. Furthermore, it is desirable that such measurements be made relatively quickly and in a fully automated manner. A further objective is to make the evaluation of the distance meters relatively insensitive to environmental influences such as variations in ambient air temperature over the test region.
Although methods for measuring the performance of distance meters are generally suitable for their intended purpose, some limitations still exist in measurement methods with respect to required laboratory space, speed and automation of measurements, and sensitivity to environmental conditions. What is needed is an improved method for evaluating the performance of distance meters. Such distance meters may be stand-alone distance meters or may be incorporated in other instruments such as laser trackers.
According to an embodiment of the present invention, a system includes: a first distance meter operable to send a first beam light in a first path that intercepts a first retroreflector and a second retroreflector, to receive the first beam of light after reflection from the first retroreflector and the second retroreflector, and to measure a first distance traveled by the first beam of light, the first retroreflector being located at a first position; and a second distance meter operable to send a second beam of light in a second path that intercepts the first retroreflector, to receive the second beam of light after reflection from the first retroreflector, and to measure a second distance traveled by the second beam of light.
According to another embodiment of the present invention, a method includes: sending a first beam of light from a first distance meter in a first path that intercepts a first retroreflector and a second retroreflector, the first retroreflector being located at a first position; receiving with the first distance meter the first beam of light after reflection from the first retroreflector and the second retroreflector; measuring with the first distance meter a first distance traveled by the first beam of light; sending with a second distance meter a second beam of light in a second path that intercepts the first retroreflector; receiving with the second distance meter the second beam of light after reflection from the first retroreflector; measuring with the second distance meter the second distance traveled by the second beam of light; and storing the measured first distance and the measured second distance.
Referring now to the drawings, exemplary embodiments are shown which should not be construed to be limiting regarding the entire scope of the disclosure, and wherein the elements are numbered alike in several FIGURES:
The detailed description explains embodiments of the invention, together with advantages and features, by way of example with reference to the drawings.
In
In an embodiment, the first retroreflector assembly 230 includes a retroreflector 232, a retroreflector housing 238, a mounting plate 240, and an adjustment stage 242. In an embodiment, the retroreflector 232 is a cube-corner retroreflector. In other embodiments, the retroreflector is a different type of retroreflector such as a cat's eye retroreflector. In an embodiment, a cube-corner retroreflector 232 includes three mutually perpendicular reflectors 234A, 234B, 234C that intersect in a vertex 236. In an embodiment, the cube-corner retroreflector 232 is made of glass. In another embodiment, the cube-corner retroreflector is made of three separate reflective surfaces, each surrounded on the reflective side by air. In an embodiment, the second retroreflector assembly 250 includes an SMR 252, a nest 254, and an adjustment stage 256.
In an embodiment, the motorized rail assembly 270 includes a central rail 272, a carriage 274, a collection of stands 278, and a motor 279. The carriage 274 rides on the central rail 272 and supports the first retroreflector assembly 230. In an embodiment, the motor 279 drives a belt that moves the carriage 274 along the central rail 272. In an embodiment, the central rail is extended to cover tens of meters, as illustrated in
In an embodiment, the laser source 212 emits a beam of light 280 and receives a returning beam of light 284. In an embodiment, the light is produced by a frequency stabilized helium-neon (HeNe) laser that emits red light. Many types of reference interferometer assemblies may be used, and many different principles of operation may be used by these reference interferometer assemblies. In an embodiment, the light 280 emitted by the laser source 212 reflects off the mirror 214 and passes through the linear-optics assembly 216. The beam of light 281 emerges from the linear optics assembly 216 and travels to the cube-corner retroreflector 232 where it intersects the retroreflector as shown in
In an embodiment, the laser source 212 includes optical and electrical components that together determine the distance between the linear-optics assembly 216 and the cube-corner retroreflector 232. In an embodiment, a processor 290 is coupled to the laser source 212. The processor may be internal to the laser source or coupled to the laser source 212 by wired or wireless connections. In an embodiment, the processor 290 includes memory and is part of a computer. In an embodiment, the distance between the linear-optics assembly 216 and the retroreflector 232 depends on the wavelength of the laser light emitted by the laser source 212, which in turn depends on the temperature, pressure, and relative humidity of the air through which the laser beam travels. In an embodiment, the processor 290 is further coupled to a weather station 292 that includes a temperature sensor 294, a pressure sensor 295, and a humidity sensor 296.
In an embodiment, signals from the weather station 292 are sent to the processor 290 through wired or wireless connections. In an embodiment, the effect of temperature, pressure, and humidity on the index of refraction of the air is determined using a modified Edlin equation. In other embodiments, another equations such as the Ciddor equation is used. The length traveled in a given interval is determined by dividing the speed of light in vacuum (299,792,458 meters per second) by the index of refraction of the air based on readings provided by the weather station 292.
In an embodiment, the distance moved by the retroreflector 232 is measured by the reference interferometer assembly 210 and compared to an equivalent distance moved by the retroreflector 232 as determined by a distance meter 12 under test. In an embodiment, the distance meter 12 is included in a laser tracker 10. The reference interferometer assembly 210 and weather station 292 components are selected for accuracy and are calibrated by accredited calibration laboratories to obtain a relatively low expanded uncertainty in the determined distance traveled by the retroreflector 232. In an embodiment, the tracker 10 is connected to a processor 60, which receives information from a temperature sensor 62, pressure sensor 64, and humidity sensor 66. The processor 60 may be internal to the tracker, external to the tracker, or a combination of internal or external processors. In some embodiments, the processor 60 represents one or more processors that may include any sort of electrical processing device such as field programmable gate arrays, digital signal processing devices, microprocessors, memory, and any other sort of computing or signal processing device.
In an embodiment, the tracker 10 emits a beam of light 290, which arrives at the retroreflector and is reflected as the beam 291 at a position on the opposite side of the axis of symmetry 237 of the cube-corner retroreflector 232. As clearly shown in
One advantage of the method described above in reference to
Another advantage of the system shown in
A system 800 that enables a reduction in factory space by a factor of four is shown in
Terms such as processor, controller, computer, DSP, FPGA are understood in this document to mean a computing device that may be located within an instrument, distributed in multiple elements throughout an instrument, or placed external to an instrument.
While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the invention. Additionally, while various embodiments of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments. Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
This application claims the benefit of U.S. Provisional Application Ser. No. 62/799,996, filed Feb. 1, 2019, the entire disclosure of which is incorporated herein by reference.
Number | Date | Country | |
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62799996 | Feb 2019 | US |