HIGH SENSITIVITY POSITION-SENSING METHOD

Abstract: High sensitive position sensing apparatus and method for sensing the position of a movable member (14) comprises an optical directional coupler (10) providing four external ports (a,b,c,d). Light from a short coherence length diode laser (13) is injected into the first port (a). The coupler (10) serves as a beam splitter to direct one portion of the injected light to the member (14) via the second port (b) and a single mode optical fiber (11b). Part of this one portion is reflected concurrently from the member (14) and from the adjacent polished coating at the end face of said fiber (11b) back into said fiber (11b) and optically coupled via the third port (c) to a photodetector (15) to provide a signal whose amplitude is indicative of the position of the member (14), based upon the relative phase of said concurrent reflections. The other portion of the injected light is optically coupled to and via the fourth port (d) to another photodetector (18) for roviding, as a reference, a signal proportional to the intensity of the injected light. These two signals are supplied to a subtractive circuit (21) for providing an output in which power fluctuations of the laser are minimized.

Description: This invention relates to a high sensitivity position sensing method, and more particularly to a fiber-optic interferometric sensing method for detecting slight movements of a movable member, such as a cantilever in an atomic force microscope. Fiber optic position or displacement sensors are useful for remote sensing of motion, such as in atomic force microscopes or for the detection of acoustic waves or the measurement of vibration. Several fiber-optic sensors utilizing optical interference effects have heretofore been proposed. U.S. Patent 4,652,744 to Bowers et al. describes a displacement sensor used for acoustic wave detection. It uses the interference of two components of light reflected from the same point on a sample, one component of which is delayed in time by a fiber optic delay line. This method has the disadvantage that it cannot detect slowly changing displacements. The lowest frequency that can be detected is determined by the time delay in the fiber optic delay line. Appl. Phys. Lett. 53, 12 (1988) discloses an atomic force microscope disposed in a vacuum and comprising a cantilever having a tip disposed adjacent a sample and a mirror attached to its backside to facilitate reflection of a laser beam from the cantilever on to a position-sensitive detector. While this arrangement works acceptably in many cases, it requires a highly reflective surface on the cantilever and is not suitable, for example, when the cantilever is made from a fine wire or the like. Rev. Sci. Instr. 55, 162 (1984) and a variation thereof published in Rev. Sci. Instr. 59, 2337 (1988) disclose a fiber optic interferometer which can detect slowly changing displacements and is used for vibration measurements. These devices comprise a long coherence length gas laser and polarization-sensitive optics. Horizontally polarized light from the gas laser is transmitted through a polarizing beamsplitter and launched into the optical fiber. The light passes through a fiber loop that acts analogously to an optical quarter-wave plate. The fiber loop converts the horizontally polarized light into circularly polarized light, which then travels to the end of the fiber. Light that reflects from the end of the fiber interferes either destructively or constructively with light reflected by the object. The relative phase of the two reflecting components determines the total amount of circularly polarized light that propagates back through the fiber. The fiber loop acts on the circularly polarized light to convert it to vertically polarized light. This vertically polarized light leaves the fiber and is reflected by the polarizing beam splitter to a photodiode detector. The apparatus described in these references has the following disadvantages: 1) Bulky components such as the gas laser, objective lens, and beam splitter are used. Between components, the light propagates through air, to air currents and acoustic noise. 2) Manual alignment of the various components is necessary. Routine realignment is necessary to accurately focus the light into the core of the single mode fiber, which is very small. 3) The detection method is based on polarization of the light and relies on the polarizing beam splitter to separate the light that is reflected by the object from the light which is incident from the laser. To make this work properly, the fiber loop size and orientation must be adjusted to ensure that the light returning from the fiber has the proper vertical polarization. Unfortunately, other incidental bends in the fiber will disturb the polarization. Also, the polarization will be temperature sensitive since the birefringence of the fiber is temperature sensitive. 4) Since a long coherence length helium-neon gas laser is used, stray reflections from other parts of the apparatus can interfere either constructively or destructively with the light coming from the end of the fiber. The phase of the stray reflections determines whether the interference is constructive or destructive. Since the phase of the stray reflections varies with temperature, etc., this leads to an unstable signal (low frequency noise). SPIE Proceedings, Vol. 838, pp. 288-291 describes an optical fiber displacement sensor which uses a frequency modulated diode laser and a wave guide coupler. Frequency modulated light is coupled into a multi-mode optical fiber through a fiber coupler and the light is directed onto the object by a lens. The frequency difference between light reflected from the object and light reflected from the end of the fiber causes the optical power to oscillate at a beat frequency determined by the distance between the object and the end of the fiber. This beat frequency is measured with a frequency counter. This method has the following disadvantages: 1) Frequency modulation of the diode laser depends critically on the proper choice of bias current and is a function of temperature and individual diode characteristics. 2) Measuring the beat frequency accurately is a slow process, therefore the bandwidth of the measurement is limited. 3) The optical beam size emerging from the lens is on the order of 1 mm. Thus the method is not suited for measuring small objects, such as force microscope cantilevers which can have dimensions on the order of several micrometers. SPIE Proceedings Vol. 514, pp. 71-74 describes an optical fiber absorption spectrometer. It uses light transmitted to a sensing cell through single mode fiber and a fiber coupler. The sensing cell consists of a region where the fiber core is exposed to the liquid whose absorption spectrum is to be sensed. A mirror at the end of the fiber in the sensing cell reflects the light back through the coupler to the photodetector. The amount of light detected by the photodetector depends on the absorption spectrum of the liquid. The device is not a position or displacement sensor and, although it has some commonality in configuration, it does not use interference effects for sensing. The German patent application DE-A-3 311 809 discloses an interferometric Fabry-Perot sensor system which can be used, for example, to measure temperature, electrical current, magnet or sound phenomena. There is a need for a highly sensitive position sensing apparatus of the fiber-optic interferometric type which incorporates the following highly desirable features: minimal polarization sensitivity, minimal sensitivity to the thermal response of the fiber optic components; compactness of configuration; use of a short coherence length laser; and absence of optical adjustments. These objects of the invention are accomplished by the features of claim 1. Further advantages of the invention are characterized in the dependent claims. Toward this end a highly sensitive apparatus for sensing the position or displacement of a movable member is provided which comprises an optical directional coupler providing a plurality of external ports. Light from a short coherence length diode laser is injected into one of the ports. The coupler serves as a beam splitter to direct one portion of the injected light to the member via a second port and a single mode optical fiber. Part of said one portion of the light is reflected concurrently from the member and from the adjacent cleaved end of said fiber back into said fiber and optically coupled via a third port to a photodetector to provide a signal whose amplitude is indicative of the position of the member, based upon the relative phase of said concurrent reflections. The other portion of the injected light is preferably transmitted by optical coupling through a fourth port to another photodetector for providing, as a reference, a signal proportional to the intensity of the injected light. These two signals are preferably supplied to a subtractive or dividing circuit or the like for providing an output in which power fluctuations of the laser are minimized. For a better understanding of the present invention, reference is made to the following description taken in connection with the accompanying drawings. Fig. 1 is a schematic diagram of a position sensing apparatus shown applied, for sake of illustration, to an atomic force microscope (AFM); Fig. 2 is a fragmentary view, to greatly enlarged scale, of a portion of the apparatus shown in Fig. 1 to illustrate the optical paths of the light reflected from the fiber end and the member, such as the cantilever of an AFM, whose position is to be sensed; and Fig. 3 is a plot showing variations in detected light versus fiber end-to-member spacing. As illustrated in Fig. 1, the position sensing apparatus comprises a conventional fiber directional coupler 10 having four ports a,b,c,d. Coupler 10 optically couples two single mode optical fibers 11,12 having four external leads 11a,11b,12a,12b extending from ports a,b,c,d, respectively. A diode laser 13, injects light into port a via one end of fiber 11. Coupler 10 acts as a nonpolarization-sensitive beam splitter which directs substantially half of the light via port b and fiber 11 to a member 14 whose position is to be sensed. Light is reflected from the end of fiber 11 near member 14 and also from the member itself. The interference condition for these two reflections x and y (see Fig. 2) depends on the relative phase of the two reflections and determines the total amount of light reflected back through fiber 11. The reflected light traveling back through fiber 11 is optically coupled by coupler 10 and transmitted via port c to fiber 12 and directed to a photodetector 15. Photodetector 15 may comprise a photodiode connected to a voltage source +V and connected to ground via a resistor 16. Photodetector 15 provides an output signal in line 17 which responds to the motion of member 14 and thus senses its position. The amplitude of this signal can be used as the signal for sensing the position of member 14. However, means, such as now to be described, are preferably provided for substantially cancelling power amplitude fluctuations in the laser 13. As illustrated, the other half of the light injected into fiber 11 is preferably optically coupled by coupler 10 and transmitted via fiber 12 to a photodetector 18, such as a photodiode connected to a voltage source +V and to ground via an adjustable resistor 19. The photodetector 18 provides, as a reference, an output signal in line 20 that is proportional to the light injected by laser 13 into fiber 11. The position output signal in line 17 is suitably matched against the reference output signal in line 20 to minimize the effect of power fluctuations in laser 13. As illustrated, a circuit or differential amplifier 21 subtracts the reference signal from the position signal. However, if preferred, a divider or other circuit could be substituted for circuit 21. In either event, the output in line 22 of the circuit 21 or its equivalent is used to sense, or if desired through suitable servo feedback electronic circuitry 23, control the position of member 14 relative to some other element or vice versa. As shown in Fig. 3, the amplitude of the optical power detected at photodetector 15 varies as a function of the spacing between the end of fiber 11 and member 14. The amplitude changes from minimum to maximum for a displacement of λ/4, where λ is the optical wavelength. The preferred operating point for detecting small displacements or position changes is at z, the steepest part of the curve, which is approximately half the distance between minimum and maximum. As illustrated, member 14 is a cantilever arm of a force microscope, such as an atomic force microscope (AFM), of the type disclosed in U.S. Patent 4,724,318 assigned to the assignee of the present invention. The AFM comprises a piezoelectric element 24 connected to the member 14 and an x,y,z drive 25, for controlling movement of a sample 26 relative to the tip of cantilever member 14. The specific means by which the x,y,z drive 24 controls movement of sample 26 and the manner in which the piezoelectric element 24 (or a bimorph equivalent) operates on the cantilever member 14 form no part of this invention. However, as illustrated, the servo feedback circuitry 23 would control the z-drive portion of drive 25. To enhance reflectance at the end of lead 11b of fiber 11, the end face of the fiber facing member 14 preferably has a partially reflecting coating (some 10⁻¹⁰ m) thick of a metal, such as silver or aluminum. Alternatively, if preferred, the coating may comprise a quarter-wavelength thickness of a dielectric having a high index of refraction, such as ZrO₂. Stray reflections from the ends of leads 12a,b of fiber 12 at the photodetectors 15 and 18, respectively, can be minimized by immersing the fiber ends in an index matching liquid, such as Series A marketed by Cargille of Cedar Grove, New Jersey, or by polishing said ends so that the plane of the ends of said fiber are not perpendicular to the axis of the fiber. To optimize performance, the laser light source 13 should have short coherence length to minimize interference effects from stray reflections. Laser 13 should therefore be of the multi-mode variety. Diode laser 13 preferably is of the type having a fiber optic output, such as the Model GO-DIP 1000 marketed by General Optronics of Edison, New Jersey. If preferred, however, source 13 may be a super-radiant diode or a light emitting diode which has short coherence length. Alternatively, short coherence length can be achieved by modulating a single mode diode laser at high frequency. While the illustration depicts the member 14 and photodiode 18 adjacent the ends of fibers 11 and 12, respectively, it will be understood that, if preferred, member 14 and photodiode 18 may be disposed adjacent the ends of fibers 12 and 11, respectively. Also, if desired, the directional coupler 10 can be an integrated optical device in which the diode laser 13 and photodetectors 15,18 are connected directly to the ports a,c,d, respectively, of the directional coupler rather than by leads 11a,12a,12b connected to said ports. In such case, the lengths of the "leads" to the diode laser and photodetectors would be substantially zero. It will now be seen that the method embodying the invention possesses the following advantages: 1) Use of compact components with direct fiber interconnection. Because there is no air path between components, sensitivity to air currents and acoustic noise is minimal. Because the components have direct fiber interconnections, they never need realignment. 2) Use of a fiber directional coupler which is not sensitive to polarization, and therefore is polarization independent and immune to polarization changes that inevitably arise due to ambient temperature variation and/or to bending of the fiber. Also, the need for a fiber loop and associated adjustments is desirably eliminated. 3) Use of a short coherence length light source, such as a multi-mode laser diode, a single mode laser diode modulated at high frequencies, or a light emitting diode (LED). The short coherence length assures that stray reflections from other parts of the apparatus will not have a definite phase relationship with the signal light. Thus the signal will be much more stable against variations in temperature and other disturbances. 4) The light from the laser can be monitored. Amplitude fluctuations can be cancelled by an appropriate circuit, such as a divider circuit or a differencing circuit. 5) A frequency modulated light source is not required. 6) The light is confined to less than 5 micrometers in diameter by use of single mode optical fibers. Thus, movement of small objects, such as AFM cantilevers, can be measured without requiring lenses to reduce theoptical spot size. It will be understood by those skilled in the art that the fiber optic position sensor herein disclosed may be used for other purposes, such as for detection of acoustic waves or for measurement of vibration or surface roughness, and that changes in form and detail may be made. Accordingly, the apparatus and method herein disclosed are to be considered merely as illustrative, and the invention is to be limited only as specified in the claims.

Claims: Method for sensing the position of a movable member (14) utilizing a first light-conducting optical fiber (11b) fed by a coupler (10) for directing light to said member (14) and for returning light reflected from said member (14) and light reflected into said first fiber (11b) prior to impinging upon said member (14) to said coupler (10), the interfering reflected light components being used to determine the position of said member (14), characterized in that the method utilizes coherent light in conjunction with single mode optical fibers and a directional coupler (10), the light reflected from the end of said first fiber (11b) into said first fiber (11b) being directed to said coupler (10) superimposed on the light reflected from said member (14) into said first fiber (11b), in said coupler (10) said light being directed through a second light-conducting fiber (12a) to a first photodetector (15), the amplitude of which is a measure of the position of said member (14). Method as claimed in claim 1, characterized in that coherent light from said coupler (10) is split up, one portion being applied to said member (14) and a second portion through a third light-conducting fiber (12b) to a second photodetector (18) for the formation of a reference value. Method as claimed in claim 2, characterized in that the output of said first photodetector (15) is matched to that of said second photodetector (18). Method as claimed in claim 1, 2 or 3, characterized by using a diode laser (13) light having short coherence length as the source of injected light to minimize interference effects from stray reflections. Method as claimed in claim 1, characterized by applying a partially reflecting coating at the end face of the fiber (116) to enhance reflectance therfrom. Method as claimed in claims 1 and 2 characterized by polishing the end face of fibers (12a, 12b) so that its respective plane is not perpendicular to the fiber axis for minimizing stray reflections or by immersing the end of the fibers (12a, 12b) in an index-matching liquid.

Inventors: MAMIN, HARRY JONATHON, RUGAR, DANIEL
Applicants: INTERNATIONAL BUSINESS MACHINES CORPORATION
Application year: 1990
Main classification: G01D5
IPC codes: G02B6, G01D5, G01B9, G01Q60