JP3417399B2 - Wavefront sensor - Google Patents

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a wavefront sensor for measuring the wavefront of a light wave, and more particularly to a wavefront sensor for highly accurate measurement even when the operating environment or the conditions of incident light change.

[0002]

2. Description of the Related Art Conventionally, as a device of this type, CS Gardne
r et al. "Design and Performance Analysis of Adapti
ve Optical Telescopes Using Laser Guide Stars "Pro
c. IEEE vol.78 NO.11 p1721-1743 (1990), and T. Noguc
hi et al. "Active Optics Experiments 1" Publ. Natl.
Astr. Obs. Japan vol.1 There is one shown in P49-55 (1989). FIG. 11 is a combination of those shown in the above literature. In the figure, 1 is a primary mirror of a telescope, 2 is a secondary mirror, 3 is a primary mirror controller, 4 is a reference light source lamp, 5
Is a lamp light condensing lens, 6 is a pinhole, 29 is a reference light source, 7 is a beam splitter, 8 is a collimator lens, 9
Is a lens array, 10 is a CCD, 11 is an optical system of a Shack-Hartmann wavefront sensor, 25 is a field stop of the optical system 11 of a wavefront sensor, 12 is an optical collimator lens to be measured, 13 is a deformable mirror, and 14 is a beam splitter. , 15 is a reference wavefront generator, 16 is an objective lens, 17
Is an eyepiece lens, 28 is an afocal optical system including 16, 17, and 26, 18 is a lens array, 19 is a CCD, and 2
0 is the optical system of the Shack-Hartmann wavefront sensor, 2
6 is a field diaphragm of the optical system 20 of the wavefront sensor, 21 is a wavefront calculator, 22 is a deformable mirror controller, and 23 is a deformable mirror controller.
Is a condenser lens for the observation device, 24 is the image plane of the observation device, 5
Reference numerals 0 and 51 are wavefront sensors.

First, the outline of the above apparatus will be described.
The light from the star is collected by the primary mirror 1 and the secondary mirror 2, passes through the field stop 25 and the beam splitter 7, and then is collimated by the collimator lens 12. After that, the condenser lens 23 is passed through the deformable mirror 13 and the beam splitter 14.
Is focused on the image plane 24 of the observation device and observed. The main mirror 1 is a large telescope of several meters long, and the main mirror 1 is likely to be deformed by its own weight. As a countermeasure against this, an active support mechanism is provided on the primary mirror 1 to correct it to an optimum shape. Since the light of a star is considered to be a plane wave when averaged over time, the light reflected by the beam splitter 7 is reflected by the optical system 1 of the wavefront sensor.
1 and the wavefront calculator 21 calculates the wavefront shape based on the output, so that the shape of the primary mirror 1 can be known. The primary mirror controller 3 drives the active support mechanism based on the output of the wavefront calculator 21 to correct the shape of the primary mirror 1.

Further, when considering a short time interval, there is a spatial and temporal variation of the refractive index in the atmosphere. as a result,
Light from a star has turbulence from a plane wave, and even a telescope with which an ideal image formation state can be obtained moves or blurs the image of the star. The deformable mirror 13 corrects the movement and blurring of the star image that cannot be corrected by the primary mirror 1 and that occurs in the short time period as described above. The wavefront fluctuation of the light from the star is obtained by the optical system 20 of the wavefront sensor, and the deformable mirror controller 22 controls the deformable mirror 13 to correct the wavefront based on the measurement result.

Next, the structure of the wavefront sensors 50 and 51 will be described. Optical systems 11 and 2 of wavefront sensors 50 and 51
The basic part of 0 is the lens array 9 and 18 and CCD 1.
It consists of 0,19. The wavefront sensor of this method measures the wavefront of the measured light at the positions of the lens arrays 9 and 18. Since the wavefront changes due to propagation, in the optical system 11 of the wavefront sensor, the collimator lens 8 projects the wavefront of the primary mirror 1 onto the lens array 9. The afocal optical system 28 of the wavefront sensor 51 has a matching measurement range determined by the dimensions of the microlens array 18 and the diameter of the measured wavefront.

Next, the measurement principle of the wavefront sensors 50 and 51 will be described. The wavefront calculator 21 measures the inclination of the wavefront incident on each lens (lenslet) of the lens array 9, 18 from the movement of the focused spot on the CCD 10, 19, and the inclination ΔW _{i of} the wavefront measured by each lenslet. Is added to obtain the wavefront. The movement amount Δr of the focused spot is determined by the inclination angle θ of the wavefront incident on the lenslet and the focal length f of the lens array.
_{It is calculated} from _m by the following formula. _{Δr = f m · tanθ (1} ) Now, the wavefront slope to be measured by the i-th lenslets Δ
W _i is calculated by the following equation, where D _m is the diameter of the lenslet. ΔW _i = D _m · tan θ _i = D _m · Δr _i / f _m (2) The measured wavefront W is expressed by the following equation. W = ΣΔW _i (3)

Since the wavefront measurement is performed based on the displacement of the spot from the reference position, the reference spot position is required. The focused spot by the reference light source is used as the standard spot position. By measuring the wavefront emitted from the reference light source in advance, the standard wavefront indicated by the standard spot position can be known. From the displacement of the spot position when the light to be measured is incident, the change amount of the wavefront is obtained, and the change amount is added to the reference wavefront to obtain the wavefront of the measurement light.

The reference light sources 15 and 29 must be emission light wavefronts that match the wavefront sensor. Since the wavefront sensor 50 measures a mirror-shaped light wave, the incident light needs to be a spherical wave. The reference light source 29 is for obtaining the reference spot position of the wavefront sensor 11. The light emitted from the lamp 4 is focused on the pinhole 6 by the lens 5, and the spherical wave without distortion is obtained by the diffraction at the pinhole 6. Further, the wavefront sensor 51 having the afocal optical system 28 is provided with the reference wavefront generator 15 for emitting the collimated reference light.

[0009]

The conventional wavefront sensor has the following problems.
With the above configuration, when the environmental temperature of the wavefront sensor changes, aberrations occur due to changes in the refractive index of the optical system, changes in the shape, changes in the lens spacing due to thermal expansion of the lens barrel, etc. there were.

Further, there is a problem that aberration of the optical system of the wavefront sensor occurs due to the change of the refractive index of air due to the change of atmospheric pressure, resulting in a wavefront measurement error.

The present invention has been made to solve the above problems, and an object of the present invention is to obtain an apparatus for measuring a wavefront with high accuracy even if the operating environment conditions change.

[0012]

In order to achieve the above-mentioned object, a wavefront sensor according to a first aspect of the present invention comprises a lens array, a lens for projecting light to be measured on the lens array, and this lens. In the wavefront sensor for measuring the wavefront of the light to be measured, which comprises an optical system having a photoelectric converter for detecting the focused spot position of the lens array by the light to be measured, the temperature provided in the optical system. An error wavefront calculator that obtains an error wavefront from the amount of movement of the focused spot position caused by the difference in linear expansion coefficient between the lens array and the substrate of the photoelectric converter due to temperature change based on the output of the sensor, and the photoelectric converter. And a wavefront calculator that subtracts the error wavefront from the wavefront of the measured light obtained based on the output of the converter.

According to a second aspect of the wavefront sensor of the present invention, there is provided a lens array, a temperature compensation optical system for projecting light to be measured on the lens array, and a collection of the lens array by the projected light to be measured. A photoelectric converter for detecting a light spot position, and a wavefront sensor having a wavefront for measuring the wavefront of the light to be measured, wherein the temperature compensation optical system includes the lens array and the substrate of the photoelectric converter due to the temperature change. To generate a wavefront that cancels the error wavefront based on the amount of movement of the focused spot position caused by the difference in linear expansion coefficient.

According to a third aspect of the wavefront sensor of the present invention, a lens array, a lens for projecting light to be measured on the lens array, and a focused spot position of the lens array by the projected light to be measured. In the wavefront sensor for measuring the wavefront of the light to be measured, the lens is composed of a plurality of lenses in which different materials are combined. It is equipped with satisfying. Here, i is the number of lenses forming a plurality of lenses, m is the number of lenses forming a plurality of lenses, φ _i is the power of the i-th lens γ _i is the atmospheric pressure dispersion of the _i -th lens material γ _i = 1 / (n _i −n _a ) n _i is the refractive index of the i-th lens material n _a is the refractive index of air.

[0015]

In the wavefront sensor of the invention according to claim 1 configured as described above, the error wavefront calculator has a lens array and a substrate of the photoelectric converter which are generated by a temperature change based on the output of the temperature sensor. The error wavefront is calculated from the amount of movement of the focused spot position caused by the difference in the linear expansion coefficient of the wavefront calculator, and the wavefront calculator subtracts the error wavefront from the measured wavefront obtained based on the output of the photoelectric converter. Highly accurate wavefront measurement that is not affected by changes can be performed.

Further, in the wavefront sensor of the invention according to claim 2 configured as described above, the temperature compensation optical system causes a difference in linear expansion coefficient between the lens array and the substrate of the photoelectric converter due to the temperature change. By generating a wavefront that cancels the error wavefront based on the amount of movement of the focused spot position caused by the above, highly accurate wavefront measurement that is not affected by temperature changes can be performed.

Further, in the wavefront sensor of the invention according to claim 3 configured as described above, the lens is composed of a plurality of lenses in which different materials are combined, Here, i is the number of lenses forming a plurality of lenses, m is the number of lenses forming a plurality of lenses, φ _i is the power of the i-th lens γ _i is the atmospheric pressure dispersion of the _i -th lens material γ _i = 1 / (n _i −n _a ) n _i is the refractive index of the i-th lens material n _a is the refractive index of air. By having a lens that satisfies the atmospheric pressure compensation condition for the atmospheric pressure change, it is possible to perform highly accurate wavefront measurement that is not affected by the atmospheric pressure change.

[0018]

BEST MODE FOR CARRYING OUT THE INVENTION Embodiment 1. FIG. 1 is a configuration diagram showing a first embodiment of the present invention. 1, the same reference numerals as those in FIG. 11 indicate the same or corresponding parts.
In FIG. 1, 1 is the main mirror of the telescope, 2 is the secondary mirror of the telescope,
8 is a collimator lens, 9 is a lens array, 10 is CC
D and 11 are wavefront sensor optical systems, 100 is a wavefront sensor,
101 is a temperature sensor, 102 is an error wavefront calculator, 103
Is a wavefront calculator.

As described in the conventional example, the wavefront measurement error occurs due to the aberration caused by the change in the refractive index of the optical material, the change in the shape of the optical material due to the temperature change, the change in the lens interval due to the thermal expansion of the lens barrel, and the like. In the present embodiment, the temperature sensor 101 and the error wavefront calculator 102 are provided, the aberration generated at the operating temperature is obtained as an error wavefront, and the error wavefront is subtracted from the measurement wavefront obtained from the output of the CCD 10 by the wavefront calculator 103. The temperature compensation is performed at.

The details of the error wavefront calculator 102 will be described below. The error wavefront calculator 102 is used for the temperature sensor 10
Based on the output of 1, the change in focus position caused by the temperature change in the collimator lens 8 is calculated from a predetermined formula, and this is converted into a wavefront. Further, the error wavefront calculator 102 calculates the wavefront generated by the displacement of the spot position due to the difference in linear expansion coefficient between the lens array 9 and the CCD 10. The error wavefront calculator 102 outputs a sum of the above two wavefronts to the wavefront calculator 103 as an error wavefront.

The contents of calculation performed by the error wavefront calculator 102 are
A method of calculating a change in the focus position of the collimator lens 8 due to a temperature change, a method of obtaining an error wavefront from the change in the focus position, and a lens array 9 and CCD 1.
The methods for obtaining the error wavefront due to the difference in the linear expansion coefficient of 0 will be separately described below in order.

The change in the focus position of the collimator lens 8 is caused by the change in the power caused by the change in the refractive index of the collimator lens due to the change in temperature and the expansion and contraction of the lens barrel. When the back focus of the collimator lens 8 is f _b and the linear expansion coefficient of the lens barrel is α, the change of the focus position with respect to the change of the temperature T can be expressed by the equation (101). dx / dT = (df _b / dT) + αf _b = (− 1 / φ) · (β−α) (101) where β = (1 / φ) · dφ / dT: thermal dispersion rate

Therefore, the focus position change when the temperature change is found can be obtained by the following equation. Δx = (− 1 / φ) · (β−α) · ΔT (102)

The focus position change Δx and the error wavefront ΔW _T are related as follows. ΔW _T = Δx / 8λF ² (103) where λ is the wavelength and F is the F value of the lens.

Therefore, the error wavefront can be calculated by the following expression from the expression (103) and the expression (102) of the change in the focus position of the collimator lens due to the temperature change. ΔW _T = (1 / 8λF ² ) · (−1 / φ) · (β−α) · ΔT (104)

Next, the error wavefront caused by the difference in linear expansion coefficient between the lens array and CCD will be described. The linear expansion coefficient of the lens array substrate material is α _m , and the linear expansion coefficient of the CCD is α _c
Let r be the distance from the optical axis. The spot movement amount Δr caused by the shape change due to the temperature change is expressed by the following equation. Δr = (α _m −α _c ) ΔT · r (105)

The relationship between the spot movement amount Δr and the error wavefront is related as follows. Here, n is the number of lens arrays, f _m is the focal length of the lens arrays, and D _m is the aperture diameter of the lenslets.

From the above, the relationship of the change of the error wavefront with respect to the temperature change is expressed by the following equation. dW _M / dT = Σ (D _m / f _m ) · (α _m −α _c ) · r _i (107)

Therefore, the error wavefront when the temperature change ΔT occurs can be calculated by the equation (108). ΔW _M = (dW _M / dT) · ΔT (108)

The equation (104) and the equation (1
08), the error wavefront calculator 102 outputs the error wavefront ΔW.
By obtaining _T and ΔW _M and subtracting the error wavefront from the measured wavefront W affected by the temperature change by the wavefront calculator 103 as in the equation (109), the correct wavefront W _I can be obtained. W _I = W- (ΔW _T + ΔW _M ) (109)

Reference Example 1 FIG. 2 is a configuration diagram showing a reference example 1 of the present invention. 2, the same reference numerals as those in FIG. 11 denote the same or corresponding parts. In FIG. 2, 1 is the main mirror of the telescope, 2 is the secondary mirror of the telescope, and 8
Is a collimator lens, 9 is a lens array, 10 is CC
D and 11 are wavefront sensor optical systems, 200 is a wavefront sensor,
201 is a barometric pressure sensor, 202 is an error wavefront calculator, 203
Is a wavefront calculator.

As shown in the conventional example, a change in atmospheric pressure causes a change in the refractive index of the atmosphere, which causes a wavefront measurement error. In this reference example , the pressure sensor 201 is used as a compensating means.
And an error wavefront calculator 202 are provided to obtain the error wavefront at the atmospheric pressure used, and the atmospheric pressure is compensated by subtracting the error wavefront from the measurement wavefront affected by the atmospheric pressure change obtained from the output of the CCD 10 by the wavefront calculator 203. It is a thing.

The details of the error wavefront calculator 202 will be described below. The error wavefront calculator 202 includes the atmospheric pressure sensor 20.
Based on the output of 1, the change in the lens power generated in the collimator lens 8 due to the change in atmospheric pressure is calculated, converted into a wavefront, and output to the wavefront calculator 203 as an error wavefront.

Hereinafter, a method of calculating the power change of the collimator lens 8 due to the atmospheric pressure change performed by the error wavefront calculator 202,
Two points of the conversion method from the power change to the error wavefront will be described.

First, the collimator lens 8 due to the change in atmospheric pressure
A method of calculating the power change of is described. The change of the power φ due to the change of the atmospheric pressure P is expressed by the following equation. (Dφ / dP) = (dφ / dn _a ) (dn _a / dP) (201)

The change dx in the focus position due to the change in atmospheric pressure is expressed by the following equation. dx / dP = (dx / dφ) (dφ / dn _a ) (dn _a / dP) = (− 1 / φ ² ) (dφ / dn _a ) (dn _a / dP) = (1 / φ) (1 / n−n _a ) (dn _a / dP) = (1 / φ) · γ · (dn _a / dP) (202) where γ = 1 / n−n _a : atmospheric pressure dispersion (203)

Therefore, the ratio of the defocus wavefront aberration due to the change in atmospheric pressure is expressed by the following equation through the change in the refractive index of the inter-lens medium. dW _P / dP = (1 / 8λF ² ) (dx / dP) = (D / 8λF) · γ · (dn _a / dP) (204)

Therefore, the error wavefront ΔW _P when the pressure change ΔP occurs can be calculated from the equation (205). ΔW = (dW _P / dP) · ΔP (205)

As described above, the error wavefront ΔW _P is calculated by the error wavefront calculator 202 according to the equation (205), and the wavefront calculator 2 is calculated.
In 03, the correct wavefront W _I can be obtained by subtracting the error wavefront from the measured wavefront W affected by the atmospheric pressure change as in the equation (206). W _I = W-ΔW _P (206)

Embodiment 2 . FIG. 3 is a configuration diagram showing a second embodiment of the present invention. 3, the same reference numerals as those in FIG. 11 denote the same or corresponding parts.
In FIG. 3, reference numeral 301 denotes a temperature-compensated afocal optical system,
Reference numeral 302 is a lens array, 303 is an objective lens, 304 is an eyepiece lens, and 19 is a CCD. In addition, here CCD
A wavefront calculator for obtaining the wavefront based on the output of 19 is not shown.

In this embodiment, the lens arrays 302 and C
The error wavefront generated due to the difference in the linear expansion coefficient from that of the CD 19 is compensated by the residual aberration of the temperature compensation afocal optical system 301. The linear expansion coefficient of the substrate material of the lens array 302 is α _m , and the linear expansion coefficient of the CCD 19 is α _c . The relationship between the amount of movement of the spot and the error wavefront is expressed by the above-mentioned equation (107). Here, n is the number of lens arrays, f _m is the focal length of the lens arrays, and D _m is the aperture diameter of the lenslets.

Next, the lens power of the afocal optical system 301 satisfying the temperature compensation condition will be described. First, a method of calculating the power change of the afocal optical system 301 due to the temperature change will be described. The power of the afocal optical system 301 is expressed by equation (302). φ = φ _o + φ _e −e φ _o φ _e = (m + 1) φ _o −meφ _o ² (302) where φ _o : Power of objective lens 303 φ _e : Power of eyepiece 304 m = φ _e / φ _o : Magnification of afocal optical system 301 e = (1 / φ _o ) + (1 / φ _e ) = {(m + 1) / m} · (1 / φ _o ) (303): Distance between objective lens 303 and eyepiece 304

The temperature change rate of the power of the afocal optical system 301 is expressed by the equation (304). _{(Dφ / dT) = φ o} {d (m + 1) / dT} + (m + 1) (dφ O / dT) -mφ o 2 (de / dT) -2meφ o (dφ O / dT) -eφ o 2 (dm / DT) (304) By making the thermal dispersions β _o and β _e of the objective lens 303 and the eyepiece lens 304 equal, the afocal optical system 3
If the magnification m of 01 does not change with temperature,
It is expressed by the following equation. dm / dT = 0 (305) Using the above formulas (303), (304), (305), the temperature change rate of the power of the afocal optical system 301 is expressed by formula (306). dφ / dT =-(m + 1) φ _o (α _B + β _o ) (306) where α _B = (1 / e) · (de / dT): linear expansion coefficient β _o = (1 / φ _{o of the} lens barrel ) ・ (Dφ _o / dT)

Therefore, since a wavefront that cancels the error wavefront θ caused by the spot movement is generated as the temperature compensation condition,
It is necessary to satisfy the following formula. (DW _T / dT) = (1 / 8λF ² ) ・ (dΔx / dφ) ・ (dφ / dT) = (1 / 8λF ² ) ・ (-1 / φ ² ) ・ (dφ / dT) = -θ ( 307)

On the other hand, in a synthetic lens in which thin lenses made of plural kinds of materials are brought close to each other, when the dispersion of the i-th material is μ _i and the lens power is φ _i , the synthetic power and the achromatic condition Must be satisfied. The power of each lens is determined from three conditions including this condition and the formula (307) relating to the power satisfying the above temperature compensation condition.

As described above, by constructing the objective lens 303 and the eyepiece lens 304 by using at least three kinds of materials, the wavefront which satisfies the two conditions of the temperature compensation and the achromatization while satisfying the combined power condition. The sensor can be configured.

Third embodiment. FIG. 4 is a configuration diagram showing a third embodiment of the present invention. 4, the same reference numerals as those in FIG. 11 denote the same or corresponding parts.
In FIG. 4, 1 is the main mirror of the telescope, 2 is the secondary mirror of the telescope,
Reference numeral 400 is a wavefront sensor, and 401 is an atmospheric pressure compensation collimator lens. A wavefront calculator for obtaining the wavefront based on the output of the CCD 10 is not shown here.

The atmospheric pressure dispersion γ represented by the equation (401) can be treated in the same manner as the dispersion μ in the so-called achromatic lens. γ = 1 / (n−n _a ) (401)

When the collimator lens 401 is composed of a plurality of lenses in which different kinds of materials are combined, it is possible to equivalently synthesize and create material characteristics such as atmospheric pressure dispersion γ. In a synthetic lens in which thin lenses made of plural kinds of materials are arranged close to each other, when the dispersion of the i-th material is μ _i , the atmospheric pressure dispersion is γ _i , and the lens power is φ _i , the collimator lens 401 has the following conditions. Need to be satisfied.

As described above, if a collimator lens is constructed by using at least three kinds of materials, an afocal optical system that achromatically achromatically satisfies the synthetic power condition and surely satisfies the two conditions of pressure compensation. You can

Reference Example 2 FIG. 5 is a configuration diagram showing a reference example 2 of the present invention. 5, the same reference numerals as those in FIG. 11 denote the same or corresponding parts. In FIG. 5, 501 is a calibration value calculator, 502 is a wavefront sensor angle controller, and 29 is a reference light source.

In this reference example , the distance between the CCD 10 and the lens array 9 required for accurately calculating the inclination of the wavefront is not directly measured, but is measured and calibrated in the mounted state.

As shown in the conventional example, the relationship between the deviation amount Δr of the spot position on the CCD 10 and tan θ is expressed by the following equation. tan θ = Δr / l _m (501) where l _m is the distance between the microlens array 9 and the CCD 10. Now, light with an incident angle θ is incident on the wavefront sensor, the deviation Δr from the reference spot position is measured, and the distance l _m is obtained from the above θ and Δr by the equation (501).

The method of calibrating the wavefront sensor will be described below. (1) The wavefront calculator 21 measures the reference spot position by the reference light source 29, (2) the wavefront sensor angle controller 502 tilts the optical system 11 of the wavefront sensor by θ, and the tilt angle θ is the calibration value calculator 501. Send to. (3) The wavefront calculator 21 measures the spot position for calibration data, and (4) The displacement Δr of the spot position where the wavefront calculator 21 subtracts the reference spot position from the spot position for calibration data.
Is sent to the calibration value calculator 501. (5) The calibration value calculator 501 calculates the distance l _m between the lens array 9 and the CCD 10 in pixel units from Δr and θ, and the wavefront calculator 21 stores the data in the internal memory. This completes the calibration.

When the wavefront measurement is performed, the actual lens array 9 and CCD 10 are calibrated by performing the above-described calibration in advance.
The distance between them can be accurately obtained, and the accuracy of wavefront measurement can be improved.

Reference Example 3 FIG. 6 is a configuration diagram showing Reference Example 3 of the present invention. 6, the same reference numerals as those in FIG. 11 denote the same or corresponding parts. In FIG. 6, 600 is a wavefront sensor, 601 is a half mirror, 602 is a calibration light introducing half mirror, 603 is an array light source NA adjustment mask, 604 is an array light source, 60
Reference numeral 5 is a shutter. A wavefront calculator that obtains a wavefront based on the output of the CCD 19 is not shown here.

In this reference example , instead of the reference wavefront generator 15 for emitting the collimated reference light necessary for the wavefront sensor having the afocal system 28 described in the section of the prior art, the reference light is obtained with a simple structure. I am trying.

First, the structure of the wavefront sensor will be described. The optical system 2 of the wavefront sensor outputs the light emitted from the array light source 604.
Calibration mirror introduction half mirror 602
Are arranged in front of the CCD 19. An array light source 604 is installed at a mirror image position of the CCD 19 generated by the half mirrors 601 and 602. Array light source 6
The NA adjusting mask 603 provided on the front surface of 04 has a number of openings corresponding to the array light sources 604 provided in the flat plate, and limits the emission angle of each light source forming the array light source 604. The light emitted from the light source and the lenses forming the lens array 18 are made to correspond one to one. F of lens array 18
When the value is F and the distance from the array light source 604 to the mask 603 is x, the aperture diameter D of the mask 603 is obtained by the following equation. D = x / F (601)

The light emitted from the array light source 604 is introduced into the wavefront sensor through the calibration light introducing half mirror 602,
After being reflected by the half mirror 601, the lens array 18 focuses the light on the CCD 19. When the reference light source is used, the light to be measured is blocked by the shutter 605.

Next, a method of correcting the measured wavefront using the reference light source will be described. The light emitted from the array light source 604 is
Since it passes through the optical system of the wavefront sensor twice, the effect of twice the aberration of the optical system is measured. Array light source 60
An accurate array can be obtained by using, for example, a laser diode array for 4, so that the disorder of the array of spots is caused by the influence of the optical system aberration. Obtain the wavefront based on the disordered arrangement of the measured spots,
As an error wavefront caused by the aberration of the optical system, the wavefront calculator 2
1 subtracts the previously obtained error wavefront from the measured wavefront when measuring the wavefront, so that the correct wavefront can be measured.

In the conventional method, when the position of the reference light source 29 is moved in the optical axis direction due to a change in ambient temperature or the like, a distorted spherical wave is incident on the wavefront sensor and the position of the spot is changed. However, in this embodiment, when the installation position of the array-shaped light source 604 moves in the optical axis direction, the blur of the spot occurs due to the loss of the conjugate relationship with the CCD. However, in the wavefront calculator 21, if the center of gravity of a commonly used spot is defined as the spot position measurement, the center of gravity position does not change even when blurring occurs.

As described above, it is possible to realize a reference light source that is strong against changes in operating environment conditions, and this also eases manufacturing tolerances when the array light source is arranged at a conjugate position with the CCD. Can be taken.

Reference Example 4 FIG. 7 is a configuration diagram showing Reference Example 4 of the present invention. 7, the same reference numerals as those in FIGS. 11 and 6 denote the same or corresponding parts. In FIG. 7, 700 is a wavefront sensor, 701 is a polarizing plate, and 704 is an array-shaped polarized light source. A wavefront calculator that obtains a wavefront based on the output of the CCD 19 is not shown here.

In this reference example , the light to be measured is polarized,
A polarizing plate 701 is used instead of the half mirror 601 of Reference Example 3 , and an array-shaped polarized light source 704 is used as the array-shaped light source 604.
Is used.

The array-shaped polarized light source 704 is installed at a mirror image position of the CCD 19 generated by the half mirror 602 and the polarizing plate 701, and is orthogonal to the polarization direction of the measured light. When the polarization direction of the polarizing plate 701 and the polarization direction of the measured light are set to coincide with each other, the measured light passes through the polarizing plate 704,
A focused spot is formed on the CCD 19. The reference light is reflected by the polarizing plate 701 to form a spot on the CCD 19. When the array-shaped polarized light source 704 is used, the light to be measured is blocked by the shutter 605. Other operations are similar to those of the reference example 3 .

As described above, the polarizing plate 701 reflects almost 100% of the calibration light and at least 100% of the measured light.
Since the light is transmitted, it is possible to realize an optical system in which the loss of the reference light and the measured light by the polarizing plate 701 inserted for calibration is extremely small.

Reference Example 5 FIG. 8 is a configuration diagram showing Reference Example 5 of the present invention. 8, the same reference numerals as those in FIGS. 11 and 6 indicate the same or corresponding portions. In FIG. 8, 800 is a wavefront sensor, 801 is a dichroic mirror, and 804 is an array light source having a wavelength different from that of the light to be measured. A wavefront calculator that obtains a wavefront based on the output of the CCD 19 is not shown here.

In this reference example , the wavelengths of the measured light and the reference light are different. The dichroic mirror 801 is configured to transmit light in the wavelength range of the measured light and reflect it in the wavelength range of the reference light.

The array light source 804 is a half mirror 60.
CCD 19 generated by 2 and the dichroic mirror 801
It is installed in the mirror image position of. The measured light passes through the dichroic mirror 801 and forms a spot on the CCD 19. On the other hand, the light emitted from the array light source 804 is introduced by the half mirror 602, reflected by the dichroic mirror 801, and forms a spot on the CCD 19. When the reference light source is used, the light to be measured is blocked by the shutter 605. Other operations are similar to those of the reference example 3 .

As described above, the dichroic mirror 80
In No. 1, since the reference light is reflected by almost 100% and the measured light is transmitted by almost 100%, it is possible to realize an optical system in which the light amount loss of the reference light and the measured light by the dichroic mirror 801 is extremely small.

Reference Example 6 FIG. 9 is a configuration diagram showing Reference Example 6 of the present invention. 9, the same reference numerals as those in FIG. 11 denote the same or corresponding parts. In FIG. 9, 900 is a wavefront sensor, 901 is a diaphragm with a variable diameter, 902 is a diaphragm diameter controller, 903 is a diaphragm diameter calculator which is a diaphragm diameter calculating means, and 904 is an FFT calculator which is an FFT calculating means.

In this reference example , in order to suppress stray light, the aperture diameter is changed in accordance with the state of light condensed by the objective lens 16 of the afocal optical system.

In order to suppress stray light, it is necessary to make the diameter of the diaphragm as small as possible so that the light to be measured does not fall. When the front focal plane of the objective lens 16 is the wavefront measurement position, the point image intensity distribution by the objective lens 16 follows the Fourier transform result of the measured wavefront. The FFT calculator 904 performs Fourier transform of the measured wavefront obtained by the wavefront calculator 21 to obtain a point image intensity distribution. A diaphragm diameter calculator 903 gives a threshold value to the point image intensity distribution, and sets a range exceeding the threshold value as a diaphragm diameter. The aperture diameter controller 902 adjusts the aperture diameter based on this information.

As described above, stray light, which has been a problem in the case of the fixed diaphragm, can be reduced, and malfunctions can be suppressed.

Reference Example 7 : FIG. 10 is a configuration diagram showing Reference Example 7 of the present invention. Figure 10
11, the same reference numerals as those in FIG. 11 indicate the same or corresponding portions. In FIG. 10, 8 is a first collimator lens, and 1
Reference numerals 11 and 113 denote first and second dichroic mirrors, 114 and 115 denote bandpass filters, 116 and
118 is a mirror, 117 is a second collimator lens, 1
Reference numeral 10 is a wavefront sensor. A wavefront calculator that obtains a wavefront based on the output of the CCD 19 is not shown here.

The telescope has a structure in which the sub-mirror 2 is replaced, and the F-number changes as shown by the broken line in FIG. As shown in the conventional example, it was necessary to replace the collimator lens 8 depending on the change of the F value or prepare another wavefront sensor corresponding to each F value.

In order to make the diameters of the wavefronts incident on the lens array 18 different in F value, the first collimator lens 8
The focal length of 1 may be changed according to the F value. In this reference example , the optical path is separated by the first dichroic mirror 111, and a second collimator lens 117 adapted to the F value is installed in the separated optical path to cope with the change in the F value.

Since the second collimator lens 117 and the optical path length can be freely set by changing the optical path, the second collimator lens 117 suitable for the F value can be used and the lens array 18 and thereafter can be shared. it can. Since two wavelengths of light are incident on the lens array, the bandpass filters 114 and 115 are exchanged to perform wavelength selection.

As described above, there is no need to replace the entire optical system depending on the F value, and since there are no moving parts other than the bandpass filters 114 and 115, the tolerance of the optical system can be suppressed to a high level and high precision can be achieved. Wavefront measurement can be realized.

[0080]

According to the present invention configured as described above, it is possible to obtain a wavefront sensor capable of measuring the wavefront of the light to be measured with high accuracy even if the use environment conditions change.

[Brief description of drawings]

FIG. 1 is a configuration diagram of a wavefront sensor according to a first embodiment.

2 is a configuration diagram of a wavefront sensor of Reference Example 1. FIG.

FIG. 3 is a configuration diagram of a wavefront sensor according to a second embodiment.

FIG. 4 is a configuration diagram of a wavefront sensor according to a third embodiment.

5 is a configuration diagram of a wavefront sensor of Reference Example 2. FIG.

FIG. 6 is a configuration diagram of a wavefront sensor of Reference Example 3 ;

7 is a configuration diagram of a wavefront sensor of Reference Example 4. FIG.

8 is a configuration diagram of a wavefront sensor of Reference Example 5. FIG.

FIG. 9 is a configuration diagram of a wavefront sensor of Reference Example 6 ;

10 is a configuration diagram of a wavefront sensor of Reference Example 7. FIG.

FIG. 11 is a configuration diagram of a device (telescope) including a conventional wavefront sensor.

[Explanation of symbols]

1: Telescope primary mirror 2: Telescope secondary mirror 4: Lamp for reference light source 5: Lamp light condensing lens 6: Pinhole 7: Beam splitter 8: Collimator lens (first collimator lens) 9: Lens array 10: CCD 11: Optical system of wavefront sensor 13: Deformable mirror 14: Beam splitter 16: Objective lens 17: Eyepiece 18: Lens array 19: CCD 20: Optical system of wavefront sensor 21: Wavefront calculator 22: Deformable mirror 28: Afocal optical system 29: Reference light source 50: Wavefront sensor 51: Wavefront sensor 100: Wavefront sensor 101: Temperature sensor 102: Error wavefront calculator 103: Wavefront calculator 110: Wavefront sensor 111, 113: Dichroic mirror 114 and 115: bandpass filters 117: Second collimator lens 116, 118: mirror 200: Wavefront sensor 201: Barometric pressure sensor 202: Error wavefront calculator 203: Wavefront calculator 301: Temperature-compensated afocal optical system 302: Lens array 303: Objective lens 304: Eyepiece 400: Wavefront sensor 401: Collimator lens for pressure compensation 501: Calibration value calculator 502: Wavefront sensor angle controller 600: Wavefront sensor 601: Half mirror 602: Half mirror for introducing calibration light 603: Array-shaped light source NA adjustment mask 604: Array light source 605: Shutter 700: Wavefront sensor 701: Polarizing plate 704: Arrayed polarized light source 800: Wavefront sensor 801: Dichroic mirror 804: Array light source whose wavelength is different from that of the light to be measured 900: Wavefront sensor 901: Aperture with variable diameter 902: Aperture controller 903: Aperture diameter calculator 904: FFT calculator

─────────────────────────────────────────────────── ─── Continuation of the front page (56) Reference JP-A-5-18719 (JP, A) (58) Fields investigated (Int.Cl. ⁷ , DB name) G01J 9/00 G01M 11/00 G02B 13 / 00

Claims (3)

(57) [Claims] 1. An optical system comprising: a lens array; a lens for projecting light to be measured on the lens array; and a photoelectric converter for detecting a focused spot position of the lens array by the projected light to be measured. In a wavefront sensor having a system for measuring the wavefront of the measured light, a linear expansion between the lens array and the substrate of the photoelectric converter due to a temperature change based on an output of a temperature sensor provided in the optical system. An error wavefront calculator that obtains an error wavefront from the amount of movement of the focused spot position caused by a difference in the ratio, and a wavefront calculator that subtracts the error wavefront from the wavefront of the measured light obtained based on the output of the photoelectric converter. And a wavefront sensor. 2. A lens array, a temperature compensation optical system for projecting light to be measured on the lens array, and a photoelectric converter for detecting a focused spot position of the lens array by the projected light to be measured, In the wavefront sensor for measuring the wavefront of the light to be measured, the temperature-compensating optical system includes the light condensing caused by a difference in linear expansion coefficient between the lens array and the substrate of the photoelectric converter due to this temperature change. A wavefront sensor, which produces a wavefront that cancels an error wavefront based on the amount of movement of a spot position. 3. An optical system comprising: a lens array; a lens for projecting light to be measured on the lens array; and a photoelectric converter for detecting a focused spot position of the lens array by the projected light to be measured. A wavefront sensor having a system for measuring the wavefront of the light to be measured, wherein the lens is composed of a plurality of lenses in which different materials are combined, and the plurality of lenses satisfy the following expression: Wavefront sensor, Here, i is the number of lenses forming a plurality of lenses, m is the number of lenses forming a plurality of lenses, φ _i is the power of the i-th lens γ _i is the atmospheric pressure dispersion of the _i -th lens material γ _i = 1 / (n _i −n _a ) n _i is the refractive index of the i-th lens material n _a is the refractive index of air.