INTERFEROMETER REQUIRING NO CRITICAL COMPONENT ALIGNMENT

Abstract: A Michealson-type self-aligning interferometer utilizes a laser (1) to produce an output beam (20) of light that is split into a signal beam (40) and a reference beam (30). The signal beam (40) is directed through a Bragg-cell (5), for heterodyne detection, and a beam expander (6), for facilitating target acquisition, toward a retroreflector (7) located on a target body (80). The returning signal beam (54) is thereby reflected back through the beam expander (6) and Bragg-cell (5) to the resonance mirror (2) of the laser (1), and is now shifted in frequency by 2 ZETA . The returning signal beam (54) and reference beam (30) are directed into a detector (4) to produce an electrical signal (60). A frequency divider (8) and a phase demodulator (9) extract the phase information (70) of the electrical signal (60) through heterodyne detection, the phase being proportional to the position of the retroreflector (7) and, hence, the target body (80).

Description: TITLE: INTERFEROMETER REQUIRING NO CRIΗCAL COMPONENT ALIGNMENT FIELD OF THE INVENTION This invention relates to self-referencing interferometers. More particularly, this invention relates to a Michealson-type self-referencing interferometer that utilizes a laser resonator mirror to achieve self-alignment. BACKGROUND OF THE INVENTION Michealson interferometers have been used, in various devices, for the measurement of displacement, spatial non-uniformity, angle, and polarization states of various reflecting bodies. Typical Michealson interferometer devices utilize a gas laser to produce a beam of monochromatic light which is then split into signal and reference beams. The signal beam is transmitted to and then reflected from a target body. The signal and reference beams are recombined in the device into a composite, co-linear beam. The difference in phase between tiie two beams creates an interference pattern, or fringe pattern, in the composite beam which is extremely sensitive to change in the position of the target body. Hence, information about the dynamics of a target body can be determined by study of the dynamics of the interference pattern. In such interferometer devices, the signal and reference beams must be precisely re-aligned into a linear composite beam in order to maximize the signal-to-noise ratio, or contrast, of the interference pattern. Current interferometer designs require precision optical components and extremely stable mechanical structures to achieve this precise alignment. Moreover, such designs utilize more components than necessary, thereby increasing the complexity and reducing the reliability of tiie devices. As a result, such interferometer devices are relatively expensive to manufacture, calibrate, and maintain. One difficulty witii the Michealson interferometer is the problem of keeping tiie reference and the signal light beams in exact parallel and colinear alignment. This is required in order to obtain tiie highest contrast or signal-to-noise ratio. Even with good initial alignment, small vibrations or temperature changes can result in distortion or beam shifting resulting in beam misalignment. The present invention uses an adaptive method such that any small shift or movement of the optical components is of little importance. That is, the reference beam and signal beam will remain colinear over small movements or rotations of the optical components. For example, in the original Michealson device, two flat mirrors and a beam splitter are used. The alignment of these optical components is very critical. Any small rotation of a flat mirror can cause the two beams to diverge. Improvement can be made by replacing the two flat-mirrors by two corner-cubes which will reflect light back at exactly the same angle even if the corner-cube is rotated slightly. In this way, the alignment of the two reflectors in tiie Michealson interferometer becomes less critical. However, the alignment of the beam splitter is still very critical. Any small rotation of the beam splitter will cause tiie reference beam and tiie signal beam to become divergent. The present invention solves this problem by using the laser output mirror as part of the interferometer to combine the reference and signal beams. As shown in FIG. 1, by using a corner cube as the means for reflecting the source beam, and , the output mirror of the laser itself for steering the reflected beam to the splitter, the two beams must always be colinear even if the splitter is rotated over a small angle. There is a need for an improved interferometer device that contains a minimal number of components, fewer of which require extreme precision or extremely stable mechanical structures. The present invention fulfills these needs and provides further related advantages. SUMMARY OF THE INVENTION The present invention is a Michealson interferometer that utilizes a resonator mirror of a laser to precisely align a returning signal beam with a reference beam. A gas laser produces an output beam which is split by a standard beam splitting device into a reference beam and a signal beam. The reference beam is directed into a detector. For subsequent heterodyne detection, the signal beam is transmitted to a Bragg-cell that shifts tiie frequency of the signal beam by Ω and the direction of the signal beam by θ. The signal beam is then directed toward a retroreflector attached to the target, whereby the signal beam is reflected back in the opposite direction. This reflected signal beam enters the Bragg-cell, again being shifted in frequency by Ω and in direction by -θ. As a result, the reflected signal beam is parallel with, but opposite in direction to, the output beam, and its frequency is shifted by 2Ω. The reflected signal beam is then partially transmitted through the beam splitter to tiie resonance mirror of the laser, whereby it is again reflected into the beam splitter and directed into the detector, co-linear with the reference beam but frequency shifted by 2Ω plus phase information. The detector produces an output signal witii an output frequency, and a frequency divider divides this output frequency by 2. A phase-demodulator is used to obtain the phase φ of the output, φ being directly proportional to the position of the retroreflector on tiie target body. Information processing means utilize φ to determine dynamic characteristics of the target body in this manner. This device achieves self-alignment of the reference beam and the reflected signal beam since both beams are perpendicular to the resonance mirror of the laser. Hence, no adjustment of the beam splitter, the laser, or the laser resonance mirror is necessary. Moreover, this device does not require a reference mirror, further simplifying its manufacture, calibration, maintenance, and use. Other features and advantages of tiie present invention will become apparent from the following more detailed description, taken in conjunction with tiie accompanying drawings, which illustrate, by way of example, the principles of the invention. DESCRIPTION OF THE DRAWINGS The accompanying drawing illustrates the invention. In such drawing: FIGURE 1 is a schematic diagram of the invention, illustrating the components and the light and signal paths of the invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT FIG. 1 illustrates a Michealson type self-aligning interferometer. A gas laser 1, preferably a helium-neon laser, has a mirror 2 and produces an output beam 20. A splitting means 3 splits the output beam 20 into spatially separated first beam 30 and second beam 40. The second beam 40 is directed into a frequency and direction shifting means 5, preferably a Bragg-cell for heterodyne detection, whereby the second beam 40 is shifted in frequency by Ω and in direction by θ. Preferably, the second beam 40 is then directed into a beam expander 6 for providing beam broadening and improved coUimation of the second beam 40 to improve beam acquisition of a reflecting means 7, preferably a retroreflector, located on a target body 80. The second beam 40, emerging from the beam expander 6, is directed along a path 50 while traveling in a first direction 52 towards the reflecting means 7, whereby the second beam 40 is reflected back along the path 50 but in the opposite direction 54 from that of the first direction 52. The second beam 40 then re-enters the beam expander 6 which, from tiie opposite direction 54, acts as a beam reducer. The second beam 40 is again directed through the frequency and direction shifting means 5, but from the opposite direction 54, whereby the frequency of the beam is again shifted by Ω and the direction of the beam is shifted by -θ. The resulting second beam 40 is parallel with the output beam 20, but opposite in direction, and is directed through the beam splitting means 3 toward the mirror 2 of the gas laser 1. The second beam 40 is then reflected from the mirror 2 and partially reflected from the beam splitting means 3 into a detecting means 4, preferably a photo-detector or, alternatively, an array detector or television camera. The first beam 30 is similarly directed into tiie detecting means 4, and is precisely aligned with tiie returning second beam 40. The detecting means 4 for detecting the first beam 30 and the returning second beam 40 is electrically connected to a frequency divider 8 which, in turn, is electrically connected to a phase demodulator 9. The detecting means 4 produces an electrical signal 60 which has a frequency of 2Ω plus the phase information 70, and tiie frequency divider 8 divides the frequency of the electrical signal 60 by 2, thereby producing a half-frequency electrical signal 65 which the phase demodulator 9 reduces to the phase information 70. This phase information 70 is directly proportional to the position of tiie reflecting means 7, and as a result can be used to determine information about the length of the path 50. While the invention has been described with reference to a preferred embodiment, it is to be clearly understood by those skilled in the art that the invention is not limited thereto. Rather, the scope of tiie invention is to be interpreted only in conjunction witii tiie appended claims.

Claims: CLAIMS What is claimed is: 1. An interferometer requiring no critical component alignment, comprising: a gas laser for producing an output light beam, the laser having an output mirror; means for splitting the output light beam into two spatially separated components, tiie components being a first beam and a second beam; means for detecting the first and the second beams, the first beam being directed by the splitting means directly to the detector for use as a reference; means for frequency and direction shifting, the second beam being directed by the splitting means to the shifting means, and therein being frequency and direction shifted; means for reflecting, the second beam being directed by the shifting means to the reflecting means, such that the second beam is reflected back to the shifting means and therein being frequency shifted a second time and direction shifted such that the second beam is directed along the path of the output light beam, being colinear thereto, so that the reflected second beam impinges the laser source output mirror and is reflected therefrom toward the splitter, a portion of the twice reflected second beam being colinear with tiie first beam and directed to the detector therewith, the reflected second light beam, being frequency shifted from tiie laser frequency therefore not destabilizing the laser upon entry through t e output mirror, whereby the stability of the splitter position is not highly critical to the proper operation of the interferometer. 2. The interferometer of claim 1 further including a phase demodulator for receiving an electrical signal, the signal corresponding to t e detected light beams, for phase demodulating the signal to produce beam path length information. 3. The interferometer of daim 1 further induding a beam expander for broadening and improving coUimation of the second beam such that the acquisition of tiie second beam by tiie reflecting means is improved. 4. The interferometer of daim 1 wherein the reflecting means is a retroreflector, so that the alignment stability of tiie shifting means is not highly critical. 5. The interferometer of daim 1 wherein tiie means for frequency and direction shifting is a Bragg-cell. 6. The interferometer of daim 1 wherein the means for detecting is a photo- detector. 7. The interferometer of daim 1 wherein tiie means for detecting is an array detector. 8. The interferometer of daim 1 wherein the means for detecting is a television camera. 9. A method for interferometric measurement in which the alignment stability of the elements of apparatus is not highly critical, comprising the steps: providing a gas laser having an output mirror, a beam splitter, a means for frequency and direction shifting, a retroreflector target, a means for detecting, and a means for phase demodulation; produdng an output light beam from the laser; splitting the output light beam into a first and a second beams at the beam splitter; detecting the first beam at the detecting means; frequency and direction shifting the second beam at the shifting means; reflecting the second beam at the retroreflector back to the shifting means; frequency and direction shifting the second beam at the shifting means for a second time; reflecting the second beam at the output mirror back to the beam splitter; detecting the second beam at the detecting means for producing a corresponding electrical signal; phase demodulating the electrical signal to acquire path length information.

Inventors: WANG CHARLES C P, WANG, CHARLES, C., P.
Applicants: WANG CHARLES C P, WANG, CHARLES, C., P.
Application year: 1992
Main classification: G01B9
IPC codes: G01B9