Spatial light modulator and a method for driving the same

Information

  • Patent Grant
  • 6388649
  • Patent Number
    6,388,649
  • Date Filed
    Thursday, March 24, 1994
    30 years ago
  • Date Issued
    Tuesday, May 14, 2002
    22 years ago
Abstract
The disclosed spatial light modulator includes a pair of facing transparent electrodes, and a light-modulating layer and a photoconductive layer provided between the transparent electrodes In the spatial light modulator, the light-modulating layer has different optical states depending on an applied charge amount. Specifically, the light-modulating layer has: a first optical state when the applied charge amount is a first threshold charge amount or more; a second optical state when the applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between the first optical state and the second optical state depending on the applied charge amount. Also, a driving method for such a spatial light modulator is disclosed.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a spatial light modulator (hereinafter abbreviated as an SLM) used in a projection-type display, a holography television, or an optical computer.




2. Description of the Related Art




An optically addressed SLM is positively developed as an essential part of a projection-type display apparatus having a large screen size which is an alternative to a thin film transistor (TFT) liquid crystal panel or a cathode ray tube (CRT).




An SLM performs a light amplification of a two-dimensional image pattern. The SLM includes a photoconductive layer and a light-modulating layer as main components thereof. When image information with low luminance enters the SLM from the side of the photoconductive layer, the electric characteristics of the photoconductive layer are modulated depending on the luminance of the image information. As the result of the modulation, the optical characteristics of the light-modulating layer are modulated. Then, reading light with high luminance enters the SLM from the side of the light-modulating layer, whereby amplified image information can be output.




As the material of the photoconductive layer, CdS, crystalline silicon (Si), amorphous Si (a—Si:H), or the like is used. Among them, a—Si:H is widely used, since a—Si:H has various superior characteristics such as high sensitivity to writing light, a low dark conductivity, wide variations of film formations, and the like. The erasure of the written image is performed without using special erasure pulse light, so that the photoconductive layer is often provided with rectification.




As the material of the light-modulating layer, electrooptic crystals or liquid crystals are used. Among such crystals, surface stabilized ferroelectric liquid crystals (SSFLC; hereinafter referred to simply as PLC) are positively used since the FLC has a faster response (about 100 μsec.) as compared with the conventional liquid crystal of the twisted nematic (TN) type.




It is conventionally known that the FLC has bistability (the binary characteristics). Specifically, the direction of spontaneous polarization of FLC is changed depending on the polarity of the applied electric field, so that the FLC has two different optical states, i.e., ON (or UP) and OFF (or DOWN). The bistability is described in detail in, for example, Appl. Phys. Lett., vol. 36 (1980) pp. 899-901.




In the case where the FLC is used practically in a display or the like, the FLC must be able to display a half-tone state between the ON state and the OFF state. In order to realize the half-tone state, the amount of applied charges is controlled, rather than the externally applied electric field. Since the FLC has the spontaneous polarization which is represented by the spontaneous polarization charge P


s


, it is that the aging due to the decomposition of the FLC molecules can be prevented. On the other hand, the driving waveform has the following problems. The voltage of the writing pulse (characterized by a writing period and a writing voltage)


202


is a very high negative voltage, so that the FLC polarization is in verted (electric field switching) even in a condition without writing light. As a result, the contrast is deteriorated. Also, since the duty ratio of the output light is ½ at most, this causes a loss of brightness. The driving method using the voltage waveform in FIG.


2


(


b


) was proposed by the inventors of this invention. In the driving method, the obtained duty ratio can substantially be 1. However, also in this method, it is impossible to prevent the contrast deterioration due to the electric field switching during the application of the writing pulse


205


.





FIG. 3

shows a driving pulse waveform used for solving the above problems. Such waveforms are used, for example, in SID Digest (1991), pp. 254-256 and U.S. Pat. No. 5,178,445. The driving pulse includes a short erasure pulse


301


with a high voltage and a long writing pulse


302


with a low voltage. In the driving pulse, the absolute value of the voltage of the writing pulse


302


is set to be smaller than the absolute value of the voltage of the erasure pulse


301


, so that it is possible to prevent the electric field switching. In addition, since the period of the writing pulse


302


is long, the duty ratio of the reading light can substantially be 1. Thus, the driving method is suitable for the application to a projection-type display or the like. The latter reference specifically mentions the driving voltage conditions for the driving with high contrast. However in both cases, the employed FLC cannot stably have states other than the ON and OFF states. In the former case, the half-tone display is realized by using the above-mentioned multi-domain gray-scale. The latter case uses, as the writing light, pulse light (for example, the emitted light from CRT having phosphors with shorter emission time than the length of one driving period of the SLM).




When the image on a CRT is written on the SLM, the period of the driving pulse voltage signal of the SLM is generally synchronized with one display period of the CRT.

FIG. 4

shows the timing chart for driving the CRT and the SLM. In

FIG. 4

, the timing chart (a) indicates the synchronization pulse voltage of the CRT, and the timing chart (b) indicates the fluorescence intensity from a phosphor on the CRT screen. Also, the timing chart (c) indicates the voltage of a driving pulse of the SLM which is synchronized with one display period of the CRT, and the timing chart (d) indicates the intensity of an output light from the SLM. As is shown in the timing chart (c), a unit driving pulse voltage signal


404


includes an erasure pulse


402


and a reading pulse (characterized by a reading period and a reading voltage)


403


, and the signal


404


is synchronized with a synchronization pulse


401


of the CRT display shown in the timing chart (a). The SLM is driven by the driving pulse voltage signal


404


. As is shown in the timing chart (b), at a certain timing in the reading period of reading pulse


403


of the driving pulse voltage signal


404


, a phosphor of the CRT emits a writing light pulse


405


. The light is received by the photoconductive layer of the SLM, and the light-modulating layer of the SLM is switched into the ON state. As a result, as is shown in the timing chart (d), the intensity


406


of the output light from the SLM rises. When an erasure pulse


402


of the next unit driving pulse voltage signal


404


is applied, the light-modulating layer is switched into the OFF state, so that the intensity


406


of the output light from the SLM becomes 0. By repeatedly performing the above operations, the output light from the SLM can be observed. This method has an advantage in that the duty ratio of the reading light (the ratio of the ON state period of the reading light to one driving period) can be increased even in the CRT screen having phosphors which emit fluorescence with a short decay time. In general, in the case where a negative voltage of a large value is applied to the SLM, the SLM may erroneously be switched into the ON state due to the electric field caused by the negative voltage even if the writing light is not incident. However, if the driving signal having a waveform shown in the timing chart (c) is used, such a negative voltage having a large value is not applied to the SLM, so that the light-modulating layer of the SLM cannot be erroneously switched into the ON state. In addition, the deterioration of the contrast ratio of the image which may be caused by such erroneous switching can be prevented. It is also reported that, by varying the fluorescence intensity from a phosphor on the CRT screen, it is possible to realize the half-tone display of the output light of the SLM.




If an SLM is applied to a projection-type display or a holography television, it is necessary that a stable half-tone display with good contrast and with good controllability can be performed.




The conventional SLM could stably have only two optical states as the light-modulating layer, and hence the multi-domain gray-scale has been used for the half-tone display. Therefore in this method, as the resolution of the input image is increased (i.e., the size of each pixel is reduced), the number of domains included in one pixel is decreased, and hence the number of obtainable gray scales is decreased. This causes a problem in that it is difficult to perform the half-tone display.




Since, in the practical driving of the SLM, the charge control is not performed in the range of the applied charge amount for obtaining the intermediate state of FLC (e.g., see U.S. Pat. No. 5,178,445), it is difficult to perform the half-tone display with high contrast.




In addition, the time-averaged value of voltages applied to the FLC is not 0, so that the switching threshold voltage is changed as a function of time due to a drift of ions in the liquid crystal molecules. This causes another problem in that the input/output response characteristics of the light-modulating layer are changed as a result of a long time driving.




In the case where one frame of CRT as the writing means (i.e., one display period) is completely synchronized with the driving period of the SLM, it is difficult to make the brightness uniform over every portion of the SLM. This is described below with reference to FIG.


5


. In

FIG. 5

, (a) is a plan view showing scanning lines


501


and


503


on the CRT screen


505


. The timing chart (b) shows the waveform of the driving signal (the driving pulse voltage) of the CRT and the SLM. The timing chart (c) indicates the fluorescence intensity from a pixel


502


of the CRT screen


505


, and the timing chart (d) indicates the intensity of output light from a pixel of the SLM corresponding to the pixel


502


. The timing chart (e) indicates the fluorescence intensity of a pixel


504


of the CRT screen


505


, and the timing chart (f) indicates the intensity of output light from a pixel of the SLM corresponding to the pixel


504


of the CRT screen


505


.




In general, the CRT screen


505


is scanned with an electron beam, and light is emitted from the pixels


502


and


504


in the irradiated portion by the electron beam. As a result, the image is displayed on the CRT screen


505


. When the electron beam scans the CRT screen


505


from the top to the bottom, the pixel


502


on the scanning line


501


in the upper portion of the CRT emits light at an earlier timing, but the pixel


504


on the scanning line


503


in the lower portion of the CRT emits light at a later timing. As a result, if the driving pulse shown in (b) of

FIG. 5

which includes an erasure pulse


506


and a reading pulse


507


is used and the reading period of the reading pulse


507


is set to be substantially equal to one frame of CRT, as a result, the light pulses from the pixels


502


and


504


have waveforms indicated by


508


and


510


shown in the timing charts (c) and (e) in FIG.


5


. The intensities of the output light from the pixels of the SLM corresponding to the light pulses


508


and


510


have waveforms indicated by


509


and


511


shown in the timing charts (d) and (f). Even if it is assumed that the writing light pulses


508


and


510


have an equal intensity, the averaged value of the intensity of the output reading light


511


is smaller than the averaged value of the intensity of the output reading light


509


in one-and the same period. Accordingly, a viewer senses that the output light


511


is darker than the output light


509


, that is, the upper left portion of the screen


505


is brighter than the lower right portion thereof. For the above-mentioned reasons, the brightness of every portion of the output from the SLM is not uniform.




SUMMARY OF THE INVENTION




The spatial light modulator of this invention includes a pair of facing transparent electrodes, and a light-modulating layer and a photoconductive layer provided between the transparent electrodes, wherein the light-modulating layer has different optical states depending on an applied charge amount, the light-modulating layer having: a first optical state when the applied charge amount is a first threshold charge amount or more; a second optical state when the applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between the first optical state and the second optical state depending on the applied charge amount.




In one embodiment of the invention, the photoconductive layer has rectification, and generates, when the photoconductive layer is in a reversed bias condition, a photoelectric current having a magnitude depending on an intensity of writing light incident on the photoconductive layer.




In another embodiment of the invention, the light-modulating layer includes a ferroelectric liquid crystal layer which is sandwiched by two alignment films.




In another embodiment of the invention, wherein a specific resistance of the alignment films is in the range of 10


8


Ω·cm to 10


11


Ω·cm.




According to another aspect of the invention, a driving method for a spatial light modulator is provided. In the method, the spatial light modulator includes a pair of facing transparent electrodes, and a light-modulating layer and a photoconductive layer provided between the transparent electrodes, the light-modulating layer having different optical states depending on an applied charge amount, the light-modulating layer having: a first optical state when the applied charge amount is a first threshold charge amount or more; a second optical state when the applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between the first optical state and the second optical state depending on the applied charge amount, wherein the photoconductive layer has rectification, and generates, when the photoconductive layer is in a reversed bias condition, a photoelectric current having a magnitude depending on an intensity of writing light incident on the photoconductive layer, wherein one period of a waveform of a driving voltage includes an erasure period in which the photoconductive layer is in a forward bias condition and a charge amount larger than the first threshold charge amount is applied, and a writing period in which the photoconductive layer is in a reversed bias condition so as to generate a photoelectric current having a magnitude depending on an intensity of writing light, and wherein the method includes a step of applying the driving voltage to the two transparent electrodes, so that in the writing period, the applied charge amount to the light-modulating layer is kept in the range of the first threshold charge amount or more when the intensity of the writing light is a first threshold light intensity or lower, and the applied charge amount to the light-modulating layer is reduced to the second threshold charge amount or less when the intensity of the writing light is a second threshold light intensity of higher.




In one embodiment of the invention, the light-modulating layer includes a ferroelectric liquid crystal layer which is sandwiched by two alignment films, and wherein conditions of:









V




th


≦(


C




f




V




e




+C




a




V




w


)/(


C




f




+C




a


)−


V




d


, and










V




w




−V




d




≦−V




th








are satisfied, where V


e


denotes the maximum value of the driving voltage in the erasure period, V


w


denotes the minimum value of the driving voltage in the writing period, C


f


denotes a capacitance of the ferroelectric liquid crystal layer without polarization inversion of the ferroelectric liquid crystal layer, C


a


denotes a capacitance of the photoconductive layer, V


d


denotes a diffusion potential of the photoconductive layer, and −V


th


denotes a threshold voltage of the ferroelectric liquid crystal layer.




In another embodiment of the invention, the driving voltage V


e


in the erasure period and the driving voltage V


w


in the writing period are respectively in the ranges of:






1 V≦


V




e


≦40 V, and








−20 V≦


V




w


≦4 V.






According to another aspect of the invention, a driving method for a spatial light modulator is provided. In the driving method, the spatial light modulator includes a pair of facing transparent electrodes, and a light-modulating layer and a photoconductive layer provided between the transparent electrodes, the light-modulating layer having different optical states depending on an applied charge amount, the light-modulating layer having: a first optical state when the applied charge amount is a first threshold charge amount or more; a second optical state when the applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between the first optical state and the second optical state depending on the applied charge amount, and wherein the driving method includes the steps of: applying a driving voltage to the two transparent electrodes; irradiating the spatial light modulator with writing light; measuring an output light intensity of the spatial light modulator with respect to at least one writing light intensity; detecting a change of the output light intensity as a function of time; and performing a feedback to at least one of the writing light intensity and the driving voltage, in accordance with the detected change of the output light intensity.




In one embodiment of the invention, the photoconductive layer has rectification, and generates, when the photoconductive layer is in a reversed bias condition, a photoelectric current having a magnitude depending on an intensity of writing light incident on the photoconductive layer, wherein one period of a waveform of a driving voltage includes an erasure period in which the photoconductive layer is in a forward bias condition and a charge amount larger than the first threshold charge amount is applied, and a writing period in which the photoconductive layer is in a reversed bias condition so as to generate a photoelectric current having a magnitude depending on an intensity of writing light, and wherein the driving voltage, in the writing period, keeps the applied charge amount to the light-modulating layer in the range of the first threshold charge amount or more when the intensity of the writing light is a first threshold light intensity or lowers and reduces the applied charge amount to the light-modulating layer to the second threshold charge amount or less when the intensity of the writing light is a second threshold light intensity of higher.




In another embodiment of the invention, the light-modulating layer includes a ferroelectric liquid crystal layer which is sandwiched by two alignment films, wherein conditions of:









V




th


≦(


C




f




V




e




+C




a




V




w


)/(


C




f




+C




a


)−


V




d


, and










V




w




−V




d




≦−V




th








are satisfied, where V


e


denotes the maximum value of the driving voltage in the erasure period, V


w


denotes the minimum value of the driving voltage in the writing period, C


f


denotes a capacitance of the ferroelectric liquid crystal layer without polarization inversion of the ferroelectric liquid crystal layer, C


a


denotes a capacitance of the photoconductive layer, V


d


denotes a diffusion potential of the photoconductive layer, and −V


th


denotes a threshold voltage of the ferroelectric liquid crystal layer, wherein the driving method includes a step of keeping values of L


1


and L


s


constant by changing at least one of V


e


, V


w


, T


w


and τ, the values of L


1


and L


2


being defined by








L




1


=(


hν/ηe


)(


C




f




+C




a


)(


V




f0




+V




th


)/


T




w


τ,










L




s


=(


hν/ηe


)(2


P




s




/T




w


τ), and










V




f0


=(


C




f




V




e




+C




a




V




w


)/(


C




f




+C




a


)−


V




d


,






where T


w


denotes a width of the writing period, τ denotes a ratio (utilization efficiency) of an intensity of light actually incident on the photoconductive layer to the intensity of the writing light, hν denotes a photon energy of the writing light, η denotes a quantum efficiency of the photoconductive layer, and e denotes an electron charge.




In another embodiment of the invention, the driving method further includes the steps of: measuring changes dY


A


and dY


B


in output light intensities of the spatial light modulator as a function of time with respect to two different writing light intensities L=L


A


and L=L


B


; obtaining changes dL


1


and dL


s


of L


1


and L


2


by using equations of








dL




1


=[(∂


Y/∂L




s


)


L=LB




·dY




A


−(∂


Y/∂L




s


)


L=LA




·dY




B


]/Δ,










dL




s


=[−(∂


Y/∂L




1


)


L=LB




·dY




A


+(∂


Y/∂L




1


)


L=LA




·dY




B


]/Δ,






and






Δ=(∂


Y/∂L




1


)


L=LA


·(∂


Y/∂L




s


)


L=LB


−(∂


Y/∂L




s


)


L=LA


−(∂


Y/∂L




1


)


L=LB


; and






changing V


e


, V


w


, T


w


and τ by amounts equal to dV


e


, dV


w


, dT


w


and dτ, respectively, so as to satisfy relationships of









dL




1


=(∂


L




1




/∂V




e


)


dV




e


+(∂


L




1




/∂V




w


)


dV




w


+(∂


L




1




/∂T




w


)


dT




w


+(∂


L




1


/∂τ)


dτ, and













dL




s


=(∂


L




s




/∂T




w


)


dT




w


+(∂


L




s


/∂τ)


dτ.








In another embodiment of the invention, the driving method further includes the steps of: measuring changes dY


A


and dY


B


in output light intensities of the spatial light modulator as a function of time with respect to two different writing light intensities L=L


A


and L−L


B


; obtaining changes dL


1


and dL


s


of L


1


and L


s


by using equations of








dL




1


=[(∂


Y/∂L




s


)


L=LB




·dY




A


−(∂


Y/∂L




s


)


L=LA




·dY




B


]/Δ,










dL




s


=[−(∂


Y/∂L




1


)


L=LB




·dY




A


+(∂Y/∂L


1


)


L=LA




·dY




B


]/Δ,






and






Δ=(∂


Y/∂L




1


)


L=LA


·(∂


Y/∂L




s


)


L=LB


−(∂


Y/∂L




s


)


L=LA


·(∂


Y/∂L




1


)


L=LB


; and






changing V


e


, V


w


, T


w


and τ by amounts equal to dV


e


, dV


w


, dT


w


and dτ, respectively, so as to satisfy relationships of








dv




e


=0,










dV




w


[(∂


L




1




/∂T




w


)


dL




s


−(∂


L




s




/∂T




w


)


dL




1


]/[(∂


L




1




/∂V




w


) (∂


L




s




/∂T




w


)],










dT




w


=−(∂


L




s




/∂T




w


)


−1




dL




s


, and










d


τ=0.






In another embodiment of the invention, the driving method further includes the steps of: measuring changes dY


A


and dY


B


in output light intensities of the spatial light modulator as a function of time with respect to two different writing light intensities L=L


A


and L−L


B


; obtaining changes dL


1


and dL


s


of L


1


and L


s


by using equations of








dL


=[(∂


Y/∂L




s


)


L=LB




·dY




A


−(∂


Y/∂L




s


)


L=LA




·dY




B


]/Δ,










dL




s


=[−(∂


Y/∂L




1


)


L=LB




·dY




A


+(∂


Y/∂L




1


)


L=LA




·dY




B


]/Δ,






and






Δ=(∂


Y/∂L




1


)


L=LA


·(∂


Y/∂L




s


)


L=LB


−(∂


Y/∂L




s


)


L=LA


·(∂


Y/∂L




1


)


L=LB


; and






changing V


e


, V


w


, T


w


and τ by amounts equal to dV


e


, dV


w


, dT


w


and dτ, respectively, so as to satisfy relationships of








dV




e


=0,










dV




w


−[(∂


L




1


/τ)


dL




s


−(∂


L




s


/τ)


dL




1


]/[(∂


L




1




/∂V




w


)(∂L


s


/∂τ)],










dT




w


=0, and










d


τ−(∂


L




s


/∂τ)


−1




dL




s


.






In another embodiment of the invention, the driving method includes a step of measuring output light intensities of the spatial light modulator with respect to three or more different writing light intensities.




In another embodiment of the invention, the driving method further includes the steps of: irradiating the spatial light modulator with the writing light via an image presentation portion and an intensity modulating portion which modulates an intensity of an image presented on the image presentation portion; and performing a feedback to a transmittance of the intensity modulating portion, in accordance with a change of the output light intensity as a function of time.




In another embodiment of the invention, the writing light is generated from a CRT, and the driving method comprises a step of performing a feedback to an electron beam current value of the CRT in accordance with the change of the output light intensity as a function of time.




In another embodiment of the invention, the measurement of the output light intensities of the spatial light modulator is performed directly after the output side of the spatial light modulator.




In another embodiment of the invention, one period of the driving voltage waveform for driving the spatial light modulator is shorter than one display period of an image formed by the writing light.




In another embodiment of the invention, a ratio of one display period of an image formed by the writing light to one period of the driving voltage is in the range of 1.5 to 1000.




In another embodiment of the invention, the output light intensity of the spatial light modulator with respect to the writing light intensities with the first threshold light intensity or lower of the spatial light modulator is substantially 0, the output light intensity with respect to the writing light intensities between the first threshold light intensity and the second threshold light intensity is increased as the writing light intensity is increased, and the output light intensity with respect to the writing light intensities which exceeds the second threshold light intensity has substantially no dependence on the writing light intensity.




In another embodiment of the invention, the writing light intensity to the spatial light modulator is substantially monotonously decreased as a function of time in one display period of an image formed by the writing light, the maximum value of the writing light intensity directly prior to the end of the display period is the second threshold light intensity or higher, and the maximum value decays to be the first threshold light intensity or lower in a period in which an image is rewritten by the writing light.




In another embodiment of the invention, the writing light is generated from a CRT.




In another embodiment of the invention, the driving voltage applied in the erasure period is in the range of +2 V to +30 V by regarding a direction in which the photoconductive layer is forward-biased as a positive, and the driving voltage applied in the writing period is in the range of −30 V to +2 V.




In another embodiment of the invention, one period of the driving voltage is constituted by a sequence of the erasure period, a first low voltage period, the writing period, and a second low voltage period.




In another embodiment of the invention, the second low voltage period is longer than the first low voltage period.




In another embodiment of the invention, the driving voltage applied in the erasure period is in the range of +2 V to +30 V by regarding a direction in which the photoconductive layer is forward-biased as a positive, the driving voltage applied in the writing period is in the range of −30 V to −2 V, and the driving voltage applied in the second low voltage period is in the range of −2 V to +2 V.




In another embodiment of the invention, the ferroelectric liquid crystal layer and the photoconductive layer are electrically in contact with each other via a metal reflection film which is divided and separated into minute portions.




According to another aspect of the invention, a spatial light modulating apparatus is provided. The spatial light modulating apparatus includes: a spatial light modulator including a light-modulating layer and a photoconductive layer provided between two facing transparent electrodes, the light-modulating layer having different optical states depending on an applied charge amount, the light-modulating layer having: a first optical state when the applied charge amount is a first threshold charge amount or more; a second optical state when the applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between the first optical state and the second optical state depending on the applied charge amount; means for applying a driving voltage to the two transparent electrodes; means for irradiating the spatial light modulator with writing light; means for measuring an output light intensity of the spatial light modulator with respect to at least one writing light intensity; means for detecting a change of the output light intensity as a function of time with respect to the at least one writing light intensity; and means for performing a feedback to at least one of the writing light intensity and the driving voltage in accordance with the detected change of the output light intensity.




According to another aspect of the invention, a liquid crystal device is provided. The liquid crystal device includes a ferroelectric liquid crystal layer sandwiched by two opposing alignment films, and means for applying charges to the ferroelectric liquid crystal layer, wherein a specific resistance of the alignment films is in the range of 10


8


Ω·cm to 10


11


Ω·cm.




Thus, the invention described herein makes possible the advantages of (1) providing a spatial light modulator which can realize a half-tone display with high contrast, (2) providing a spatial light modulator which is stable for a long use of time, (3) providing a spatial light modulator which can display an image with uniform brightness, and (4) a driving method for such a spatial light modulator.




These and other advantages of the present invention will become apparent to those skilled in the art upon reading and understanding the following detailed description with reference to the accompanying figures.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

shows waveforms for illustrating a driving method for an SLM according to the invention.





FIG. 2

shows conventional driving pulse waveforms.





FIG. 3

shows a driving pulse waveform according to the invention.





FIG. 4

shows an exemplary conventional driving method during the writing by a CRT.





FIG. 5

shows pulse waveforms for illustrating that a uniform brightness is not obtained on the screen by the conventional driving method.





FIG. 6

is a cross-sectional view showing an exemplary construction of an SLM having a metal reflective film which is divided into minute portions.





FIG. 7

is a cross-sectional view showing another exemplary construction of an SLM having a metal reflective film.





FIG. 8

is a cross-sectional view showing an exemplary construction of an SLM having a dielectric mirror.





FIG. 9

is a circuit diagram illustrating the operation of the SLM.





FIG. 10

shows the current-voltage characteristics of a photoconductive layer with rectification.





FIG. 11

is a circuit diagram corresponding to that of

FIG. 9

except that the photoconductive layer is shown as an equivalent circuit.





FIG. 12

shows the polarization inversion characteristics of an FLC layer.





FIG. 13

is a timing diagram showing the changes as a function of time in potential and transmittance of a metal reflective portion of the SLM.





FIG. 14

is another timing diagram showing the changes as a function of time in potential and transmittance of a metal reflective portion of the SLM.





FIG. 15

shows theoretical curves showing the relationship between input and output light intensities of the SLM.





FIG. 16

shows a system for measuring the input/output light intensity characteristics of the SLM.





FIG. 17

shows the measured input/output light intensity characteristics of the SLM.





FIG. 18

shows the relationship between a transmittance of the FLC layer and a voltage when the switching threshold voltage is not clear.





FIG. 19

shows a system of a projection-type display.





FIG. 20

shows a system of a holography television.





FIG. 21

shows a system of a projection-type display additionally having a feedback system.





FIG. 22

shows waveforms for illustrating a driving method using a CRT according to the invention.





FIG. 23

shows a driving pulse waveform and the output light intensity corresponding thereto.





FIG. 24

shows another driving pulse wave-form and the output light intensity corresponding thereto.





FIG. 25

shows the input/output light intensity characteristics of the SLM.





FIG. 26

shows the change of fluorescence intensity of a CRT as a function of time and shows waveforms for illustrating the relationship between two threshold values of the SLM.





FIG. 27

shows particular waveforms of the driving pulse according to the invention.





FIG. 28

shows that the half-tone state can be realized by controlling the applied charge amount.





FIG. 29

shows equivalent circuits of FLC considering the alignment film.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




First, the principle for performing the grayscale display in an SLM according to the invention is described. If a medium which displays uniform and continuous gray-scale states is used as the light-modulating layer, it is possible to continuously realize the states between the ON and the OFF states, irrespective of the number of domains in one pixel. That is, even in an extreme case where only one domain exists in one pixel, the gray-scale can be displayed. Therefore, in a case where an image with high resolution is to be displayed (i.e., in a case where the size of a pixel is small), the gray-scale display can be performed.




If the medium used as the light-modulating layer can realize only two optical states, i.e., ON and OFF by controlling the applied voltage, there may be a case where a uniform state between the ON and the OFF states can be stably realized by controlling the amount of externally applied charges, instead of the voltage. By driving such a medium using a driving circuit of charge control type (for example, by connecting a current source, instead of a voltage source), the intermediate state can be realized. If the amount of currents output from the current source is varied depending on the intensity of writing light, it is possible to control the intermediate state in accordance with the intensity of writing light. A photoconductive layer with rectification can be used as such a current source.




Next, a driving method for the above-described SLM having a light-modulating layer which can take a uniform and stable intermediate state depending on the charge amount and a photoconductive layer with rectification will be described. Specifically, the case where the modulator is driven by using a driving voltage waveform including an erasure period and a writing period is described. The amount of charges at the transition from the OFF state to the intermediate state and the amount of charges at the transition from the intermediate state to the ON state are represented by Q


1


and Q


2


, respectively. In other words, Q≧Q


1


, where Q


1


is the applied charge amount means the OFF state, Q


1


>Q>Q


2


means the intermediate state, and Q


2


≧Q means the ON state. When the erasure pulse is first applied in the erasure period, the applied charge amount Q to the light-modulating layer is equal to or larger than Q


1


, so that the state is forcibly returned into the OFF state. Next, in the writing period, the photoconductive layer generates a photoelectric current depending on the writing light intensity. If the writing light intensity is sufficiently low, the state of Q≧Q


1


is maintained during the writing period. If the writing light intensity is sufficiently high, a photoelectric current which is sufficient for changing the charge amount Q so as to be equal to or lower than Q


2


is generated. In this way, the intermediate state can be realized in a wide range between the OFF and the ON states. As a result, a gray-scale display with high contrast can be performed.




Next, a principle of stabilization of performance of the SLM in the time dimension is described. Physical parameters such as the switching threshold voltage of FLC may change by the driving for a long time. If the driving conditions are varied depending on the change, the input/output light intensity characteristics (the relationship between the writing light and the output light intensity) can be constantly maintained. Thus, a stable gray-scale display with good controllability is obtained.




Next, the principle of realizing a uniform image display is described. When plural units of driving signals (driving pulses) are applied to the SLM in one frame of the CRT, the writing and the erasure of the information displayed on the CRT screen to and from the SLM are repeatedly performed in one frame. In such a case, the writing information to the SLM or the output light intensity from the SLM in each unit driving signal (driving pulse) substantially corresponds to the fluorescence intensity from the phosphor on the CRT screen sampled at the time. Accordingly, if one period of this unit driving signal (driving pulse) is substantially shorter than the decay time constant of the fluorescence intensity from phosphor on the CRT screen, the envelope which smoothly links the peak values of output light intensities of the SLM in the respective unit driving signals (driving pulses) is substantially identical with the curve indicating the change of the fluorescence intensity from phosphor as the function of time. This means that an image which is obtained by directly viewing the CRT screen can be obtained on the output face of the SLM. As a result, uniform output light intensities can be obtained irrespective of the position on the screen of the SLM.




The emitted light intensity L from the phosphor on the CRT screen in one frame (the time is referred to as T


CRT


) decays substantially as an exponential function, and the emitted light intensity L is expressed as in Equation (9) by using a time t,








L=L




i




exp


(−


t


/τ)  (9)








(


O≦t≦T




CRT


)






where L


i


is an initial value of the emitted light intensity of the CRT, and τ is the decay time constant. A value L


f


at the end of one frame is expressed as in Equation (10) by substituting T


CRT


for t in Equation (9).








L




f




=L




i




exp


(−


T




CRT


/τ)  (10)






The input light (writing light) intensity at which the output light intensity from the SLM starts to saturate is represented by L


2


. If Lf≧L


2


, the SLM repeatedly performs almost the maximum output state over one frame, so that the maximum brightness as the integration over one frame can be obtained. In the case where the emitted light intensity from the CRT lowers below L


2


in the middle of one frame (Lf<L


2


, i.e., L


i


<L


2


exp(T


CRT


/τ), the output light intensities of the SLM thereafter are not the maximum one. This means that if L


i


is varied in the range including 0≦L


i


≦L


2


exp(T


CRT


/τ), it is possible to realize the gray-scale display with full contrast as the integration value over one frame.




An exemplary SLM according to the invention is shown in

FIG. 6. A

transparent conductive electrode


602


(e.g., ITO, ZnO, SnO


2


, etc.), and a photoconductive layer with rectification


606


,(or a photoresponsive layer) are formed on a transparent substrate


601


(e.g., glass). A metal reflective film


607


(e.g., a metal such as Al, Ti, Cr, or Ag, or a lamination of two or more kinds of metals) is formed thereon. The metal reflective film


607


is divided and separated into minute portions. Then, an alignment film


608


(e.g., a thin polymer film of polyimide or the like) for aligning liquid crystals is formed thereon. On another substrate


612


(e.g., glass), a transparent conductive electrode


611


(e.g., ITO, ZnO, SnO


2


, etc.) is formed. An alignment film


610


(e.g., a thin polymer film of polyimide or the like) is coated thereon. As the final step, the two substrates


601


and


612


having the above constructions are attached to each other with a certain gap therebetween, and FLC


609


are injected and sealed in the gap.




The material for the photoconductive layer


606


can be selected, for example, from: compound semiconductors such as CdS, CdTe, CdSe, ZnS, ZnSe, GaAs, GaN, GaP, GaAlAs, and InP; amorphous semiconductors such as Se, SeTe, and AsSe; polycrystalline or amorphous semiconductors such as Si, Ge, Si


l−x


C


x


, Si


l−x


Ge


x


, and Ge


l−x


C


x


(0<x<1); and organic semiconductors such as (1) phthalocyanine pigments (abbreviated as Pc) such as nonmetal Pc, XPc (X=Cu, Ni, Co, TiO, Mg, Si(OH)


2


, etc.), AlClPcCl, TiOClPcCl, InClPcCl, InClPc, and InBrPcBr, (2) azo coloring matters such as mono azo coloring matters and dis azo coloring matters, (3) perylene pigments such as perylenic acid anhydride and perylenic imide, (4) indigoid dyes, (5) C.I. Pigment Violet 1, (6) polycyclic quinones such as anthraquinones, and pyrenequinones, (7) cyanine coloring matters, (8) xanthene dyes, (9) charge-transfer complexes such as PVK/TNF (Polyvinylcarbazole/Trinitrofluorenon), (10) eutectic complex formed of pyrylium salt dye and polycarbonate resin, and (11) azulenium salt compound.




If the amorphous semiconductors such as Si, Ge, Si


l−x


C


x


, Si


l−x


Ge


x


, and Ge


l−x


C


x


(hereinafter abbreviated as a-Si, a-Ge, a-Si


x−l


C


x


, a-Si


l−x


Ge


x


, and a-Ge


l−x


C


x


) are used for the photoconductive layer


606


, hydrogen or halogen elements may be contained, and oxygen or nitrogen for reducing the dielectric constant and for increasing the resistivity may be contained. In order to control the resistivity, elements such as B, Al, Ga which are p-type impurities, or elements such as P, As, Sb which are n-type impurities may be added. In order to control the dielectric constant and the dark resistance or the operating voltage polarity, a junction of p/n, p/i, i/n, or p/i/n is formed by depositing amorphous materials to which such impurities are added so as to form a depletion region in the photoconductive layer


606


. Instead of the amorphous materials, two or more kinds of above-mentioned materials may be deposited for forming a heterojunction, so as to form a depletion region in the photoconductive layer


606


. The thickness of the photoconductive layer


606


is desirably 0.1-10 μm.




Next, an example of a fabrication method for the SLM is specifically described. First, an ITO thin film as a transparent conductive electrode


602


was deposited on a glass substrate


601


(40 mm×40 mm×0.3 mm) by sputtering. The thickness of the ITO film was set to be 1,000 angstroms. Then, amorphous silicon (a-Si:H) having a pin structure as a photoconductive layer


606


was deposited by plasma chemical vapor deposition (CVD). In this deposition, the thicknesses of a p-layer


603


, an i-layer


604


, and an n-layer


605


were 1,000, 17,000, and 2,000 angstroms, respectively, and the total thickness as the photoconductive layer


606


was 2 μm. As impurities, B (boron) of 400 ppm was added to the p-layer


603


, P (phosphorus) of 40 ppm was added to the n-layer


605


. No impurities were added to the i-layer


604


. Next, Cr was formed over the entire top face by vacuum evaporation, so as to form a metal reflective film


607


. The metal reflective film


607


was then divided into minute portions by using a photolithography technique. Each minute portion of the metal reflective film


607


had a size of 20 μm×20 μm, and a width between pixels was set to be 5 μm. The number of pixels was 10


6


(1,000×1,000). Then, a polyamic acid was applied thereon by a spin coat method, and the polyamic acid was thermally cured, so as to form a polyimide alignment film


608


. The thickness of polyimide was set to be 100 angstroms. The aligning process was performed by unidirectionally rubbing the surface of the alignment film


608


with a nylon cloth.




In the same way, an ITO transparent conductive electrode


611


and a polyimide alignment film


610


were formed on the substrate


612


(glass), and the aligning process was performed. Next, beads each having a diameter of 1 μm were distributed over the substrate


612


, and the substrate


601


was attached to the substrate


612


. Thus, a gap of 1 μm was formed between the substrates. As the last step, FLC


609


were injected into the gap, and a thermal treatment was performed, whereby an SLM


613


was completed.




Another construction of the SLM is shown in FIG.


7


. The SLM includes a photoconductive layer


707


with a p-layer


704


, an i-layer


705


, and an n-layer


706


, a ferroelectric liquid crystal layer


711


which is sandwiched between alignment films


712


formed on a substrate


714


, and a metal reflective film


710


. The fundamental structure is the same as that of the SLM shown in

FIG. 6

, but the SLM shown in

FIG. 7

is different in the following points.




(1) An input light blocking film


702


of a metal such as Cr, Al, Ti, or Ag is formed between a substrate


701


and a transparent conductive electrode


703


. The input light blocking film


702


prevents the writing light from reaching a pixel separation


715


, because the writing light reduces the resistance of the pixel separation


715


and causes the crosstalk to occur between pixels


716


, thereby degrading the resolution.




(2) Between the adjacent portions of the metal reflective film


710


, the whole of the n-layer


706


and part of the i-layer


705


of the photoconductive layer


707


are removed by etching, so as to form a groove. Accordingly, the adjacent portions of the metal reflective film


710


are prevented from being connected via the low-resistance n-layer, i.e., they are electrically separated from each other, so that the resolution is improved.




(3) An output light blocking film


708


of a metal such as Al, Cr, Ti, or Ag is formed on a bottom face of the groove which is formed in the above step (2). Accordingly, it is possible to avoid an erroneous switching operation which is caused by the reading output light which travels to the photoconductive layer


707


side. In addition, the intensity of the reading light can be increased.




(4) An organic output light blocking film


709


is inserted into the groove. Accordingly, the reading light can be more intensively blocked.




An SLM can have other constructions such as shown in FIG.


8


. The SLM


810


includes two transparent electrodes


802


and


806


formed on two substrates


801


and


807


, a photoconductive layer


803


, a dielectric mirror


804


, and a ferroelectric liquid crystal layer


805


. Alignment layers


808


and


809


are formed on the dielectric mirror


804


and the transparent electrode


806


, respectively. In

FIG. 8

, a dielectric reflective film


804


is formed over the entire face instead of the metal reflective film


607


in FIG.


6


.




Next, the driving method and the operating principle of an SLM will be described. Herein, the SLM


717


shown in

FIG. 7

is exemplarily used for the description. As the driving voltage applied between the two transparent conductive electrodes


703


and


713


, a driving voltage having a waveform as shown in

FIG. 3

is exemplarily used. In the waveform shown in

FIG. 3

, an erasure pulse


301


(the erasure voltage V


e


and the erasure period T


e


) and a writing pulse


302


(the writing voltage V


w


and the writing period T


w


) alternately continue.





FIG. 9

shows one pixel portion of the SLM


717


in FIG.


7


. As is shown in

FIG. 9

, the pixel portion can be regarded as a series circuit of an FLC layer


903


and a photoconductive layer


902


. Herein, the driving voltage supplied from a driving power source


901


is indicated by V


in


, a voltage across the FLC layer


903


is indicated by V


f


, and a voltage across the photoconductive layer


902


is indicated by V


a


(−V


in


−V


f


). Thus, the potential of the metal reflective film


710


is V


f


. The reference numeral


904


denotes a writing light.




The photoconductive layer


902


has the diode characteristics, so that the photoconductive layer


902


is in a low-resistance state during the application of forward bias voltage, and is in a high-resistance state during the application of reverse bias voltage, so as to generate a photoelectric current. For simplicity, the diode characteristics are assumed to be ideal (i.e., the forward resistance is 0, and the reverse resistance is infinity), and the dark current is assumed to be so small as compared with the photoelectric current that it can be neglected during the application of the reverse bias voltage. The current-voltage characteristics of the photoconductive layer under the above conditions are shown in FIG.


10


.

FIG. 10

shows current-voltage characteristics


1002


and


1001


with and without light irradiation. Herein, V


d


indicates the diffusion potential of the diode, and V


d


can be defined as a value of V


a


at the crossing of the curve of current-voltage characteristics


1002


during the light irradiation and the horizontal axis. The value of V


d


is usually in the range of about 0.1 V to 5 V. The photoelectric current indicated by I


ph


has the following relationship with the writing light intensity L.








I




ph


=(η


e/h


ν)


L


  (11)






where e denotes the charge of an electron, h ν denotes the energy of the photon, η denotes the quantum efficiency of carrier generation by the photon. In the case where the photoconductive layer


902


is in the reverse bias state, and a transient phenomenon is to be treated, it is necessary, as is shown in

FIG. 11

, to perform the analysis by regarding a photoconductive layer


1102


as a parallel circuit of the current source I


ph


and the capacitance of the photoconductive layer C


a


(=∈


a





0


/d


a


, where ε


a


denotes a specific dielectric constant, ∈


0


denotes a dielectric constant of vacuum, and d


a


denotes the thickness of the photoconductive layer). The reference numeral


1101


indicates a driving power source and the reference numeral


1104


indicates writing light.




The resistance of the FLC layer


1103


is very high, so that only the capacitance component is considered. If there is no polarization inversion of liquid crystals, it is assumed that there only exists the capacitance C


f


(=∈


f





0


/d


f


, where (f denotes a dielectric constant without the polarization inversion, and d


f


denotes the thickness of the liquid crystal layer) which is determined by the geometric shape of the FLC layer


1103


. However, if there occurs a polarization inversion, the hysteresis of the polarization should be considered. In general, there exists the hysteresis characteristics between the applied voltage V


f


and the polarization charge P of the FLC as is shown in FIG.


12


(


a


). In FIG.


12


(


a


), as the applied voltage changes from the positive voltage to the negative voltage, the polarization has a path A→G→B→C→D. As the applied voltage changes from the negative voltage to the positive voltage, the polarization has a path D→C→E→G→A. Herein, P


s


denotes the magnitude of the spontaneous polarization, and V


th


or −V


th


denotes the threshold voltage of switching.




The charge Q stored in the metal reflective film


710


is expressed as follows by considering the polarization charge P.








Q=C




f




V




f




+P


  (12)






The transmittance T of the liquid crystal layer is expressed as follows.







T


=(1


−P/P




s


)/2  (13)




The path A→B→C→D is considered in accordance with Equations (12) and (13). First, as to the path A→B, P=P


s


, T=0, and Q=C


f


V


f


+P


s


(where V


f


≧−V


th


, and Q≧−C


f


V


th


+P


s


). As to the path B→C, P=Q+C


f


V


th


, T=[1−(Q+C


f


V


th


)/P


s


]/2 (where V


f


=−V


th


, −C


f


V


th


−P


s


<Q<−C


f


V


th


+P


s


). As to the path C→D, P==P


s


, T=


1


, and C=C


f


V


f


−P


s


(where V


f


≦−V


th


, Q≦−C


f


V


th


−P


s


). Considering the above, the charge amount Q and the transmittance T have the relationship as shown in FIG.


28


. Herein, Q


1


and Q


2


are threshold charge amounts defined by the following expressions.








Q




1




=−C




f




V




th




+P




s


  (101)










Q




2




=−C




f




V




th




−P




s








In

FIG. 28

, the symbols A to D correspond to those shown in FIG.


12


(


a


). As is seen from the figure, an intermediate state (between B and C; Q


2


<Q<Q


1


) is surely generated other than the OFF state (between A and B; Q


1


<Q) and the ON state (between C and D; Q<Q


2


) The intermediate state is regarded as a state in which the charges of the polarization of +P


s


and the polarization of −P


s


are two-dimensionally distributed or a state in which the FLC molecules are uniformly in the middle of the polarization inversion.




The characteristics in FIG.


12


(


a


) are very ideal, so that in actuality the threshold voltage has no specific value and the voltage value in the switching intermediate state (between B and C) may have a width as is shown in FIGS.


12


(


b


) and


12


(


c


). In such a case, if the slope dP/dV


f


is sufficiently larger than C


f


in the intermediate state, the following analysis is approximately applied. In this case, in the curve of A→G→B→C→D, the value of V


f


at the position where the polarization inversion progresses 10% (T=0.1, i.e., P=(4/5)P


s


) is defined as −V


th


(there may be a case where V


th


<0). In some cases, the curve itself may not be symmetric with respect to the origin. In such cases, the curve D→C→E→G→A is neglected, and only the curve A→G→B→C→D is used, so as to obtain −V


th


. In the cases of FIGS.


12


(


b


) and (


c


), the same Q-T curve as that in

FIG. 28

can be obtained. In both cases, Q


1


and Q


2


are obtained by the following equations.








Q




1




=C




f




V




B




+P




s




−C




f




V




th




+P




s


  (102)










Q




2




=C




f




V




c




−P




s








where V


B


and V


C


denote voltage values at the points B and C, respectively.




By considering the above, the operation of the SLM is described by using the driving pulse wave-form shown in FIG.


1


.

FIG. 1

shows the driving pulse and the output light intensities corresponding to the driving voltage. The driving pulse


103


includes an erasure pulse


101


and a writing pulse


102


. The reference numeral


104


indicates a voltage applied to a ferroelectric liquid crystal layer during an erasure period. The reference numerals


105




a


,


105




b


and


105




c


indicate voltages applied to the ferroelectric liquid crystal layer in case of V


f0


>−V


th


, V


f0


>−V


th


, and V


f0


<−V


th


, respectively. The reference numerals


107




a


,


107




b


, and


107




c


indicate the output light intensities corresponding to the applied voltages


105




a


,


105




b


, and


105




c


, respectively.




First, the case where the erasure pulse


101


is applied (V


in


=V


e


) is considered. The width of this pulse T


e


(erasure period) and the voltage value V


e


(erasure voltage) are sufficient, the photoconductive layer


902


becomes into the forward-biased state, and the FLC layer


903


becomes into the OFF state (corresponding to the A point in

FIG. 12

, P=P


s


). In this case, the applied voltage V


f


to the FLC layer


903


is obtained by the following equation, as indicated by the broken line. V


f


=V


e


−V


d


. The applied charge Q is obtained by Q=C


f


(V


e


−V


d


)+P


s


(>Q


1


).




Next, the instance (time t=0) at which the driving voltage is varied from V


in


=V


e


to V


in


=V


w


is considered. At this instance, a current flows, so that the stored charges to the FLC layer


903


and the photoconductive layer


902


as a capacitor are changed. The capacitance of the photoconductive layer


902


is C


a


, and the polarization inversion is not induced in the FLC layer


903


due to its inertia at this instance. Accordingly, the value of P is not changed in Equation (12), and P remains P=P


s


. Assuming that the value of V


f


at this instance is represented by V


f0


, the following relationship is established by considering the charge preservation in the metal reflective film portion.




 (


C




f




V




f0




+P




s


)−{


C




f


(


V




e




−V




d


)+


P




s




}=C




a


{(


V




w




−V




f0


)−


V




d


}  (14)




In this relationship, the charge in the FLC layer


903


is obtained by Equation (12), and the photoelectric current at this instance is neglected. By Equation (14), V


f0


is represented as follows:








V




f0


=(


C




f




V




e




+C




a




V




w


)/(


C




f




+C




a


)−


V




d


  (15)






If the applied charge amount at this instance is represented by Q


0


, Q


0


is represented as follows:








Q




0




=C




f




V




f0




+P




s




=Q




1




+C




f


(


V




f0




+V




th


)  (103)






Next, the variation of the potential V


f


in the case where the writing period T


w


is infinitely long is considered.




(1) If V


f0


≧−V


th


, i.e., if Q


0


≧Q


1


, the polarization change at t=0 exists between A and B in

FIG. 12

(the OFF state). In t>0, until reaching the B point, V


f


is changed by the photoelectric current I


ph


. The variation of the potential V


f


in this state is represented as follows by the circuit shown in FIG.


11


.








C




a


(


d/dt


)(


V




w




−V




f


)−


I




ph




=dQ/dt=C




f




dV




f




/dt


  (16)






that is,







dV




f




/dt=−I




ph


/(


C




f




+C




a


)  (17)




When this equation is evaluated by using the initial condition of V


f


=V


f0


at t=0, V


f


, P, Q and the transmittance T are obtained as follows:








V




f




=V




f0




−I




ph




t


/(


C




f




+C




a


)










P=P




s


  (18)










Q=Q




0




−{C




f


/(


C




f




+C




a


)}


I




ph




t












T=


0






The time t=t


1


at which the polarization charges reach the point B is the time at which V


f


=−V


th


(i.e., Q=Q


1


).








t




1


=(


C




f




+C




a


)(


V




f0




+V




th


)/


I




ph


  (19)






After reaching the point B, the polarization inversion is performed while maintaining the relationship of V


f


=−V


th


(between B and C in FIG.


12


). The change of the polarization charge P is represented as follows by Equation (12).









I




ph




=dQ/dt=dP/dt


  (20)






When t=t


1


, P=P


s


, so that V


f


, P, Q and the transmittance T are represented as follows:







V




f




=−V




th










P=P




s




−I




ph


(


t−t




1


)  (21)










Q=Q




1




−I




ph


(


t−t




1


)










T


=(


I




ph


/2


P




s


)(


t−t




1


)






The above equations indicate that the polarization inversion state is defined by the charges generated by the photoelectric current in this period. The time at which the polarization inversion is terminated, i.e., the time t


2


at which the polarization charges reach the point C in

FIG. 12

(Q=Q


2


) is the time at which P=−P


s


in Equation (21) and represented as follows:








t




2




=t




1


+2


P




s




/I




ph


  (22)






When t>t


2


, the polarization charges P are fixed (P=−P


s


), so that the change of V


f


is represented in the same way as in Equation (16) or (17). The equation is evaluated by using the condition of V


f


=−V


th


at t=t


2


, the following are obtained.








V




f




=−V




th




=I




ph


(


t−t




2


)/(


C




f




+C




a


)










P=−P




s


  (23)










Q=Q




2




−{C




f


/(


C




f




+C




a


)}


I




ph


(


t−t




2


)










T=


1







FIG. 13

shows the changes of V


f


, T, and Q in the writing period of writing pulse


302


which are described above.




(2) Next, the case of V


f0


<−V


th


, i.e., Q


0<Q




1


is considered. At the instance of t=0, the liquid crystal layer does not follow the polarization inversion due to its inertia. However, the polarization inversion occurs in a very short time period (several tens of μsec.), and it is fixed to a certain polarization state between B and C in FIG.


12


. The potential V


f


is also fixed to V


f0


. If the polarization charge P is represented by P


0


, the following relationship is established based on the charge preservation.






(−


C




f




V




th




+P




0


)=(


C




f




V




f0




+P




s


)=


C




a


(


V




w




+V




th


)−


C




a


(


V




w




=V




f0


)  (24)






Equation (24) can also be represented in the following way.








P




0




P




s


+(


C




a




+C




f


)(


V




th




+V




f0


)  (25)






This transient phenomenon occurs instantaneously, so that it is analyzed supposing the equilibrium state P=P


0


is realized at t=0. The change of the polarization charge P in t>0 is indicated by the path from B to C in FIG.


12


. The polarization charge is changed in accordance with Equation (20). If P=P


0


at t=0, V


f


, P, Q and T are represented by the following equations:







V




f




=−V




th










P=P




0




−I




ph




t


  (26)










Q=Q




1




+P




0




−P




s




−I




ph




t












T


={1−(


P




0




−I




ph




t


)/


P




s


}/2






In

FIG. 12

, when P=−P


s


, the point C is reached at a time t


3


which is represented as follows:








t




3


=(


P




0




+P




s


)/


I




ph


  (27)






Since V


f


in t>t


3


can be represented in the same way as Equation (17), P, Q, and T are represented as follows:








V




f




=−V




th




−I




ph


(


t−t




3


)/(


C




f




+C




a


)










P=−P




s


  (28)










Q=Q




2




−{C




f


/(


C




f




+C




a


)}


I




ph


(


t−t




3


)










T=


1







FIG. 14

shows the changes of V


f


and T in the writing period of the writing pulse


302


which are described above.




Next, the change of the output light intensity Y with respect to the input light intensity L is analyzed in each of the above cases (1) and (2). In the above description, it is assumed that T


w


is infinitely large, and the progress after the erasure pulse


301


is analyzed. However, in the actual driving pulse waveform, the reset is performed again at t=t


w


, and the same operation is repeated in each of succeeding periods. Therefore, the output light intensity Y is observed as the time averaged value of the transmittance T=T(t) in the writing period of the writing pulse


302


(0≦t≦T


w


) as follows:









Y
=


1

T
w






0

T
w





T


(
t
)





t








(
30
)













As the input light intensity L is varied, the photoelectric current I


ph


is changed in accordance with Equation (11). Also, the values of the time t


1


, t


2


, or t


3


in Equation (19), (22), or (27) is changed. When T


w


is fixed, the magnitude relationship among T


w


and t


1


, t


2


or t


3


is changed in accordance with L. As a result, the region in the integration interval of Equation (30) is changed, so that the expression is also changed. By considering the above, when the value of Y in Equation (30) is actually calculated, the results are as follows:




(1) In the case of V


f0


≧−V


th


:








Y


=0 (


L<L




1


)










Y


=(


L


/2


L




s


)(1


−L




1




/L


)


2


(


L




1




≦L≦L




1




+L




s


)










Y=


1−(2


L




1




+L




s


)/2


L


(


L




1




+L




s




<L


)  (31)






(2) In the case of V


f0


<−V


th


:








Y


=(


L


<2


L




1


)/2


L




s


(


L<L




1




+L




s


)










Y


=1−(


L




1




+L




s


)


2


/2


L




s




L


(


L




1




+L




s




≦L


)  (32)






where,








L




1


=(


h ν/ηe


)(


c




f




+C




a


)(


V




f0




+V




th


)/


T




w


  (33)










L




s


=(


hν/ηe


)(2


P




s




/T




w


)







FIG. 15

is a graph showing the relationship between the input light intensity L and the output light intensity Y. In

FIG. 15

, (a) is a case of V


f0


>−V


th


, (b) is a case of V


f0


=−V


th


, and (c) is a case of V


f0


<−V


th


. As is seen from the graph, in the case of (a), the reading light intensity does not rise until the writing light intensity reaches a predetermined value L


1


. In L>L


1


, both of the writing light intensity and the reading light intensity increase. In L>L


1


+L


s


, it is possible to obtain the light output which has almost no dependence on the writing light intensity. In the case of (b), in the region where the input light intensity is low, the writing light intensity is almost in proportion to the reading light intensity. In this case, the input image with the original gray-scale is amplified and output. In the case of (c), even when the input light intensity is 0, the output light intensity has a finite value which is not equal to 0, so that the contrast of the output image is degraded. In view of the above results, in the case of (1), the gray-scale display can be performed without degrading the contrast.




Whereas the analyses in each of the above cases (1) and (2) show that V


f


can be infinitely small in accordance with Equation (23) or (28), these analyses are correct only in the range where the photoconductive layer is in the state capable of generating photoelectric currents, i.e., in the reverse bias state. In the actual operation, once V


f


=V


w


=V


d


is reached, the photoconductive layer no longer generates a photoelectric current, even if the writing light intensity is set as high as possible. That is, Q has the lower limit which is expressed as follows:








Q




lo




=C




f


(


V




w




−V




d


)+


P




s


, (in the case of


V




w




−V




d




=V




th


)  (104)










Q




lo




=C




f


(


V




w




=V




d


)−


P




s


, (in the case of


V




w




=V




d




=−V




th


)






In order to reach the ON state, the condition of Q


lo


≦Q


2


, i.e., the following condition should be satisfied.








V




w




=V




d




≦−V




th


  (29)






As described above, the conditions for the optimal contrast are derived as follows:









V




th


≦(


C




f




V




e




+C




a




V




w


)/(


C




f




+C




a


)−


V




d


, and










V




w




−V




d




≦−V




th


  (105)






The above-described operation principle can be applied to the SLM represented by the circuit of FIG.


9


. In other words, the operation principle can be applied to the SLM in which the photoconductive layer and the FLC layer are in contact with each other via the metal reflective film, such as shown in

FIGS. 6 and 7

. However, even in the SLM in which the dielectric reflective film (including a light absorbing layer or an overcoating layer) is provided as is shown in

FIG. 8

, if the dielectric reflective film and the liquid crystal layer are regarded as a single light-modulating layer, and the curve in

FIG. 12

can be obtained by measuring the relationship between the applied voltage V


f


and the polarization charge P (or the transmittance T), −V


th


can be obtained.




The above discussion holds true in either the uniform state or the multi-domain switching state. However, in order to obtain both a sufficient resolution and the number of gray scales, the former state is desirable. The conditions for obtaining the state are mentioned below. FIG.


29


(


a


) shows an equivalent circuit of one pixel portion of the FLC considering the resistance of the alignment film in the thickness direction. In FIG.


29


(


a


), a plurality of series connections of the capacitance CF for one domain of FLC and the resistance R


A


of a portion of the alignment film which is in contact with the domain in the thickness direction are arranged in parallel.




It is assumed that the initial state is the OFF state, i.e., the state where the polarizations of FLC are uniformly oriented upwardly (↑). Also, it is assumed that the charges sufficient for inverting the polarization in one domain are externally injected. The state at this instance may be the multi-domain switching state as shown in FIG.


29


(


b


) or the uniform state as shown in FIG.


29


(


c


) (specifically referred to herein as a “spatially uniform intermediate state”). In the state of FIG.


29


(


b


), the orientation states between adjacent domains are different from each other. Accordingly, the stress acts between the domains, so as to transit to the uniform orientation state as shown in FIG.


29


(


c


). However, such transition is rate-controlled by the mobility of applied charges. Therefore; in order to obtain the rapid transition, it is necessary that the charges move rapidly (in-plane averaging). For this purpose, it is sufficient to set the resistance R


A


(or the resistivity) of the alignment film to be small.




EXAMPLE 1




First, the intermediate state of liquid crystal was studied. Two glass substrates with transparent electrodes on which alignment films were formed were attached to each other with a gap of 1 μm interposed therebetween. Ferroelectric liquid crystals were injected into the gap, so as to form a liquid crystal panel. The construction of the liquid crystal panel is the same as that of an SLM excluding the photoconductive layer


606


and the metal reflective film


607


from the SLM shown in FIG.


6


. Thus, the liquid crystal panel is referred to as a simple panel. Simple panels were produced by using various types of alignment films.




A charged capacitor (the capacitance of the capacitor was set to be sufficiently smaller than that of the simple panel) was connected in parallel to each of the simple panels, so as to inject charges into the simple panel. The orientation state of the FLC molecules at this time was observed with a polarization microscope. The amount of injected charges was set to be smaller than the amount of charges required for completely inverting the polarization of FLC molecules. In all the cases, the FLC molecules were in the intermediate state. However, there were two states as the intermediate state, i.e., the multi-domain switching state and the uniform orientation state. The latter state was confirmed by observing them under the cross Nicol conditions by the polarization microscope. When the stage of the polarization microscope on which the simple panel was located was rotated, the entire plane of the panel was observed to be uniformly dark. The liquid crystal panels in the uniform orientation state were proved to be liquid crystal panels with the alignment film of polyimide having a specific resistance of 10


11


Ω·cm or less. Accordingly, it is preferable that the specific resistance of the alignment film in order to achieve the uniform orientation state is in the range of 10


8


Ω·cm to 10


11


Ω·cm. If the specific resistance of the alignment film is more than 10


11


Ω·cm, the in-plane moving speed of charges in the alignment film is slow, so that the uniform orientation cannot be attained. On the other hand, if the specific resistance is less than 10


8


Ω·cm, the reliability is deteriorated. As the material of the alignment film used in this invention, a series of conductive polyimide described, for example, in J. Photopolym. Sci. Technol., Vol. 3, No. 1 (1990) pp. 73-81.




The above uniform orientation state was stably realized for about several seconds. The reason why the time is finite is that the applied charges decay due to the leak resistance of the FLC molecules. In any case, the time is significantly longer than the switching time (about 100 μsec.) of the FLC molecules, so that it can be regarded as the stable state. The FLC molecules exhibited various orientation directions depending on the amount of injected charges. As a result, it was found that the orientation direction, i.e., the optical state could be controlled by the amount of injected charges.




As the alignment film, instead of the above-mentioned one, a high-resistive alignment film which is mixed with a conductive material, or an alignment film of which the resistance is decreased by doping an appropriate material can be used. In this example, the alignment film is applied on the entire face of the transparent electrode. Alternatively, the alignment film may be applied on the transparent electrode while some portions of the transparent electrode are not covered by the alignment film. In the portions, the FLC molecules are directly in contact with the transparent electrode, so that the resistivity of the alignment film is equivalently reduced. As a result, the charges rapidly move among domains. The liquid crystal panel is usually used by the irradiation of reading light, so that an alignment film may have photoconductivity.




The following examples mainly describe an SLM using the above-mentioned conductive polyimide.




EXAMPLE 2




The SLM shown in

FIG. 7

was actually driven by the driving pulse shown in

FIG. 3

, and the relationship between the writing light intensity L and the reading light intensity Y was measured. For the measuring, an optical system shown in

FIG. 16

was used. On the reading side of an SLM


1601


, a polarizer


1605


and an analyzer


1609


are provided so as to be perpendicular to each other. Writing light


1603


from a writing light source


1602


is incident on the SLM


1601


. Reading light


1607


from a reading light source


1604


is incident on the SLM


1601


via the polarizer


1605


and a beam splitter


1606


. In the SLM


1601


, the direction of the liquid crystal molecules in the OFF state was set parallel to the polarizing direction of the polarizer


1605


. As the intensity of the output light


1608


, the time averaged value of light intensities measured by the photodetector


1610


was used. In order to drive the SLM


1601


, the driving pulse shown in

FIG. 3

was used. For the erasure pulse


301


, the voltage V


e


was fixed to be +15 V, the time T


e


was fixed to be 100 μsec. For the writing pulse


302


, the time T


w


was fixed to be 1100 μsec. and the voltage V


w


was variously changed. The measured values are plotted in FIG.


17


. In this figure, six cases of the writing voltage V


w


, (A) −5.40 V, (B) −4.05 V, (C) −2.70 V, (D) −1.35 V, (E) −0 V, and (F) 1.35 V are shown. As is apparent from

FIG. 17

, as the voltage V


w


increases, the whole plots are shifted to the right at substantially equal intervals. If the value of V


w


is in the range of −5.40 V (A) to 1.35 V (F), the Y-L relationship at any value of V


w


can be analogized by interpolation of the curves.




Table 1 shows the measured result of V


f0


and the calculated V


f0


−(−V


th


) for the respective cases.




















V


W






Measured value




V


f0


− (−V


th


)







(V)




of V


f0


(V)




(V)





























(A)




−5.40




−1.34




−1.34







(B)




−4.05




−0.31




−0.31







(C)




−2.70




0.71




0.71







(D)




−1.35




1.74




1.74







(E)




0




2.77




2.77







(F)




1.35




3.80




3.80















Here, how V


f0


is measured is described. Each pixel portion of the SLM in

FIG. 7

has a very small area (400 μm


2


), so that the impedance is large. For this reason, it is difficult to directly insert a probe for the measurement therefore, instead of the SLM shown in

FIG. 7

, an SLM in which an electrode corresponding to the metal reflective film was formed on the entire face (10 cm


2


) was used for the measurement. In such an SLM, the entire surface of the SLM could be regarded as one large pixel. A probe was inserted into the electrode, and the potential at the transition from the erasure pulse


301


to the writing pulse


302


was observed by an oscilloscope.




Alternatively, when C


a


, C


f


, and V


d


are independently measured, and V


f0


is calculated from Equation (15), the calculated value of V


f0


is substantially equal to the value shown in Table 1.




A simple panel (in which liquid crystal is injected between two substrates with transparent conductive electrodes) was fabricated and the relationship between the applied voltage and the transmittance was measure. As a result, it was proved that V


th


was substantially equal to 0 V.




If the values of V


f0


−(−V


th


) in Table 1 are compared with the plots of the measured values in

FIG. 17

, the relationship corresponds to FIG.


15


(


c


) when the value of V


f0


−(−V


th


) is negative (in the cases (A) and (B)), and the relationship corresponds to FIG.


15


(


a


) when the value of V


f0


−(−V


th


) is positive (in the cases (C) to (F)). The compared result sufficiently coincides with the above-described analysis.




A broken line shown in

FIG. 17

indicates the characteristics corresponding to the equation V


f0


−(−V


th


)=0 which is analogized by the obtained plots. In the region below the broken line, a response with good contrast can be obtained. In other words, it is concluded that the condition V


f0


≧−V


th


is suitable.




In

FIG. 17

, in the case (F), if the writing light intensity is increased, the output light intensity does not increase. This is because the case does not satisfy the condition of Equation (29). In fact, if V


d


=0.7 V, and V


th


=0 V, the condition of Equation (29) is V


w


≦0.7 V. Thus it is proved that the cases (A) to (E) satisfy this condition, but the case (F) does not satisfy the condition.




In this example, the SLM shown in

FIG. 7

is described. As to the SLM shown in

FIG. 6

, the same results were obtained.




In the case of the SLM shown in

FIG. 8

, the switching threshold voltage is not clear due to the dielectric mirror


804


. The liquid crystal layer is actually attached to the dielectric mirror and they are regarded as a spurious light-modulating layer. A simple panel is constructed by using the spurious light-modulating layer, and the voltage-transmittance characteristics are measured. The measured result is shown in FIG.


18


. As is seen from

FIG. 18

, the threshold voltage has a width. This corresponds to the polarization inversion characteristics shown in FIG.


12


(


c


). However, if the voltage at the position where the transmittance increases by 10% of the maximum value is defined as −V


th


, a good linearity and a contrast ratio are obtained in the range of Equation (105 ).




As to the experiment in

FIG. 17

, the value of the erasure voltage is V


e


=15 V. If V


e


exceeds 40 V, the FLC molecules are decomposed by the electric field, and are likely to disadvantageously deteriorate as a function of time. If V


e


is smaller than 1 V, the sufficient reset can not be performed in the erasure period, which is not preferred.




If the writing voltage V


w


becomes less than −20 V, it is difficult to satisfy the condition of V


f0


≧−


th


for any value of V


e


in the range of 1 V≦V


e


≦40 V. On the other hand, if V


w


exceeds 4 V, it is difficult to satisfy the condition of Equation (29) by any type of FLC.




If, in the driving pulse waveform, the voltage value is not constant in an erasure pulse


2701


and a writing pulse


2702


, for example, as is shown in FIGS.


27


(


a


) and


27


(


b


), there is no problem. However, in such a case, the condition of Equation (105 ) is preferable by regarding the maximum value in the erasure voltage of the erasure pulse


2701


as V


e


and the minimum value in the writing voltage of the writing pulse


2702


as V


w


.




EXAMPLE 3




A projection-type display system was produced by using the SLM shown in FIG.


7


. The system is shown in FIG.


19


. As the writing information of an SLM


1902


, an image presented on a CRT


1901


is used. Writing light


1907


is incident on the SLM


1902


. A driving pulse is supplied by a driving power source


1903


and applied to the SLM


1902


. On the reading side, reading light


1908


from a metal halide lamp is directed to the SLM


1902


via a polarizer


1905


and a beam splitter


1904


. The output light is taken out via an analyzer


1906


and a lens


1910


, so that an image is projected on a screen


1911


. The screen of the SLM


1902


has a square size of 2.5 cm×2.5 cm. On the screen


1911


, the projected image is magnified so as to have a square size of 100 cm×100 cm. For the erasure pulse, the same as in Example 2, V


e


=15 V, T


e


=100 μsec. For the writing period, T


w


1100 μsec. and V


w


was set to be six different values (Table 1).




In all the cases, image was observed on the screen. In the cases (C), (D), and (E), the gray scales in the input image on the CRT


1901


were reproduced with good contrast. This coincides with the result in Example 2, and corresponds to the most ideal case. In these cases, the gray-scale display characteristics of image were asymmetric with respect to the writing light intensity, but it was possible to perform a faithful gray-scale display by appropriately adjusting the δ characteristics of the writing image. The brightness on the screen was 1000 lx. The contrast ratio on the screen was 400:1. On the screen, one pixel was magnified to have a square size of 1 mm×1 mm, but the crosstalk between adjacent pixels was not observed. Thus, a fine image could be obtained. In the cases (A) and (B), the contrast was poor, and the image was entirely whitish. In the case (F), only a dark image could be obtained, and the brightness on the screen was 300 lx.




In an alternative example, a TFT liquid crystal display was used instead of the CRT


1901


. In this alternative example, the same results were obtained.




In another alternative example, a system is constructed by assembling three sets of a CRT and a SLM. The three sets correspond to RGB (red, green, and blue), respectively. By the system, an image was synthesized an the screen. As a result, a vivid color image could be obtained.




EXAMPLE 4




A holography television system was produced by using the SLM shown in FIG.


7


. The system includes a He—Ne laser


2001


, a beam expander


2002


, a polarizer


2003


, a beam splitter


2004


, an SLM


2005


and a screen


2006


in a reading side


2014


. The system also includes a He—Ne laser


2001


, a beam expander


2002


, two beam splitters


2004


and two reflective mirrors


2007


in a writing side


2015


. A driving pulse is supplied by a driving power source


2016


to the SLM


2005


. The reference numerals


2010


and


2011


indicate reading light and output light, respectively. The reference numeral


1009


indicates an observer. Specifically, the SLM had 5,000×5,000 pixels with a pixel pitch of 5 μm. The employed system was shown in FIG.


20


. The fringe pattern formed by reference light


2012


from a He-Ne laser


2001


and object light


2013


was written into an SLM


2005


, then was read out by the He—Ne laser


2001


, and the observation was conducted on a screen


2006


. The driving was performed under the five conditions ((A)−(E)) in Example 2. As a result, a vivid 3D image could be obtained on the screen


2006


. When an object


2008


was moved, the output image was accordingly moved in real time. Under the conditions (C), (D), and (E) in Example 2, the fringe pattern information was reproduced on the output side with high contrast, so that the obtained 3D image was most vivid and included reduced noises.




If the fringe pattern information was captured by a CCD imaging device, and the information was presented on the CRT and written into the SLM, the same results were obtained.




EXAMPLE 5




In this example, the feedback to the driving conditions or optical writing conditions is considered. If a filter having a transmittance τ is inserted on the input side of the SLM as a means for modulating the intensity of the input light (writing light), the relationship between the writing light intensity L and the output light intensity Y is expressed as follows on the basis of Equations (30) to (33):




(1) When L


1


>0 (i.e., V


f0


>−V


th


),






Y=0(


L<L




1


)








Y=(


L


/2


L




S


)(1−


L




1




/L


)


2


, (


L




1




≦L≦L




1




+L




S


)








Y=1−(2


L




1




+L




S


)/2


L


, (


L




1




+L




S




<L


)  (


34)








(2) When


L




1


≦0 (i.e., V


f0


≦−V


th


),






Y=1−(


L


−2


L




1


)/2


L




S


(


L<L




1




+L




S


)








Y=1−(


L




1




+L




S


)


2


/2


L




S




L


(


L




1




+L




S




≦L


)  (35)






where L


1


and L


S


are defined as follows:








L




1


=(


hν/ηe


)(C


f


+C


a


)(


V




f0




+V




th


)/


T




w


τ










L




S


=(


hν/ηe


)(2


P




S




/T




w


τ)  (36)










V




f0


=(


C




f




V




e




+C




a




V




w


)/(


C




f




+C




a


)−


V




d








The characteristics of Equations (34) to (36) are simplified as follows irrespective of the case (1) or (2):








Y=Y


(


L; L




1




, L




S


)










L




1




L




1


(


C




f




, V




th




; V




e




, V




w




, T




w


τ)  (37)










L




S




=L




S


(


P




S




; T




w


, τ)






In other words, the input/output light intensity characteristics are determined by only the two parameters L


1


and L


S


Therefore, if V


e


, V


w


, T


w


, and τ can be adjusted so that L


1


and L


S


are fixed even when the parameters relating to the ferroelectric liquid crystal such as C


f


, V


th


, and P


S


are changed, the input/output light intensity characteristics are not changed (fixed).




It is assumed that the parameters C


f


, V


th


, and P


S


are changed and hence L


1


and L


1


are changed by dL


1


and dL


S


, respectively. The change of the output light intensity L for the fixed writing light intensity L is given as follows:








dY


=(∂


Y/∂L




1


)


dL




1


+(∂


Y/∂L




S


)dL


S


  (38)






By using the above equation, the changes dL


1


and dL


S


of L


1


and L


S


are reversely obtained by the following equations, by measuring the changes dY


A


and dY


B


of the output light intensity for two different writing light intensities L−L


A


and L=L


B


.







dL




1


=[(∂


Y/∂L




S


)


L=LB




·dY




A


−(∂


Y/∂L




S


)


L=LA




·dY




B


]/Δ








dL




S


=[−(∂


Y/∂L




1


)


L=LB




·dY




A


+(∂


Y/∂L




1


)


L=LA




·dY




B


]/Δ








Δ=(∂


Y/∂L




1


)


L=LA


·(∂


Y/∂L




S


)


L=LB −(∂




Y/∂L




S


)


L=LA


·(∂


Y/∂L




1


)


L=LB


  (39)






In the above equations, for example, (∂


Y/∂L




1


)


L=LA


denotes the partial differential coefficient at the writing light intensity of L=L


A


. Once the values of dL


1


and dL


S


are thus obtained, the driving conditions and the optically writing conditions are corrected so as to change L


1


and L


S


by −dL


1


and −dL


S


. That is, the conditions (V


e


, V


w


, T


w


, and τ) are changed by dV


e


, dV


w


, dT


w


, and dτ, so as to satisfy the following conditions:









dL




1


=(∂


L




1




/∂V




e


)


dV




e


+(∂


L




1




/∂V




w


)


dV




w


+(∂


L




1




/∂T




w


)


dT




w


+(∂


L




1




/∂τ) dτ













dL




S


(∂


L




S




/∂T




w


)


dT




w


+(∂


L




S


/∂τ)





  (40)






As to the changing manner, for example, the feedback can be performed only for the driving conditions according to the following equations:







dV




e


−0








dV




w


=[(∂


L




1




/∂T




w


)


dL




S


−(∂


L




S




/∂T




w


)


dL




1


][(∂


L




1




/∂V




w


)(∂


L




S




/∂T




w


)]  (41)










dT




w


=−(∂


L




S




/∂T




w


)


−1




dL




S












dτ=


0






Alternatively, for example, the feedback can be performed for both of the driving conditions and the optically writing conditions according to the following equations:








dV




e


0










dV




w


[(∂


L




1


/∂τ)


dL




S


−(∂L


S


/∂τ)


dL




1


]/[(∂


L




1




∂V




w


)(∂


L




S


/∂τ)  (42)










dT




w


0










d


τ=−(∂


L




S


/∂τ)


−1




dL




S








There may be still another changing way, for example, in which dV


e


is not 0.




In this example, the two values of L


A


and L


B


are set as the writing light intensity and then the values of dL


1


and dL


S


are obtained. Alternatively, three or more values can be used. For example, specifically, for three or more writing light intensities L


(i)


(i=1, 2, 3, . . . ), the corresponding output light intensities y


(i)


(i=1, 2, 3, . . . ) are measured, respectively, and then the values of L


1


and L


S


which make D to be minimum are calculated by using the following equation with Y in Equation (37):









D
=



i








{


Y

(
i
)


-

Y


(



L

(
i
)


;





L
1


,





L
s


)



}

2






(
43
)













Then, the changes of the values of L


1


and L


S


can be obtained.




If there is only one value L


A


which is used as the writing light intensity, only one relationship can be obtained in accordance with Equation (38). Therefore, it is impossible to determine a unique set of dL


1


and dL


S


. That is, it is impossible to find the feedback way so as to keep the input/output light intensity characteristics constant. However, it is possible to approximately stabilize the input/output light intensity characteristics by using the writing light intensity in the vicinity of L


A


.




As described above,

FIG. 17

shows the plots of actually measured values and illustrates the relationship between the input light intensity and the output light intensity for the SLM


717


shown in FIG.


7


. As to the driving conditions, the erasure period of the erasure pulse


301


was T


e


0.1 msec., the voltage value was V


e


=15 V, the writing period of the writing pulse


302


was T


w


1.1 msec. The obtained input/output light intensity characteristics were compared with the theoretical characteristics given be Equations (31) to (33). When the value of L


S


is fixed to be 290 μW/cm


2


and the value of L


1


is set to be 100+30 V


w


(the units of L


1


and V


w


are μW/cm


2


and V respectively), the plots of all the values of V


w


coincide with the theoretical curves (except for the case (F)). The theoretical curves for respective values of V


w


are also shown in FIG.


17


.




In this measurement, if a filter with transmittance τ is inserted on the input side, and the writing period is varied from 1.1 msec., it is analogized by Equation (36) the values should be set as follows:








L




1


=(110 +33


V




w


)/


T




w


τ  (44)










L




S


319


/T




w


τ






The unit of L


1


and Lis μW/cm


2


, the unit of V


w


is V, the unit of T


w


is msec. and τ is a dimensionless number. In this example, the voltage value of erasure pulse is fixed to be V


e


=15 V.




EXAMPLE 6





FIG. 21

shows an exemplary construction of a projection-type display system including means for maintaining the input/output light intensity characteristics of an SLM constant. An SLM


2103


has a construction shown in FIG.


7


and includes 10


6


pixels with a pixel pitch of 25 μm, which was produced in the previous example. As an input image information source, a CRT


2101


located on the writing side of the SLM


2103


was used. The period of image presentation of the CRT


2101


was 16.7 msec. A SELFOC lens array


2102


was used for forming an image of writing light


2115


from the CRT


2101


on an input face of the SLM


2103


. The reading side of the SLM


2103


was irradiated with light of


250


w from a metal halide lamp


2105


. The output image is projected onto a screen


2107


via a polarization beam splitter


2104


and a lens


2106


. A reference light generator


2114


is provided in a portion of an image presentation face of the CRT


2101


. The reference light generator


2114


can generate continuous light having various different intensities. The intensity of the output light


2116


corresponding to the reference light is monitored by a photodetector


2109


on the screen


2107


. In accordance with the monitored value, a control signal is generated by a signal processing system constituted of an A/D converter


2110


, an operation unit


2111


, and a D/A converter


2112


. The generated control signal is fed to a driving pulse generator


2108


or a transmittance variable filter


2113


. The driving pulse waveform generated by the driving pulse generator


2108


and the transmittance of the transmittance variable filter


2113


are varied in accordance with the control signal.




In

FIG. 21

, instead of the SELFOC lens array


2102


, an imaging optical system with usual lenses can be used. Instead of the polarization beam splitter


2104


, a combination of a usual beam splitter, a polarizer, and an analyzer can be used In

FIG. 21

, for the convenience, the A/D converter


2110


, the operation unit


2111


, the D/A converter


2112


, and the driving pulse generator


2108


are separately shown in terms of their functions. They can be constructed as a combined single electric circuit having the same functions. In the case where the photodetector


2109


is located on the screen


2107


, the signal can be fed to the A/D converter


2110


by various methods. In this example, the signal is fed to the A/D converter


2110


via electric wiring. Alternatively, the signal can be fed by a radio system using radio waves, infrared rays, or the like. In another construction, the A/D converter


2110


is provided near the photodetector


2109


, and a digitized signal is fed by such a radio system. The reference light generator


2114


may alternatively be implemented by a portion of the image presentation portion of the CRT


2101


.




In this example, the photodetector


2109


is provided on the screen. Alternatively, the photodetector


2109


may be provided, for example, directly in front of the lens


2106


or directly in the rear of the lens


2106


. The number of lenses may be increased. If plural lenses are used, the photodetector may be provided in the lens system. Such a construction in which the photodetector is located in the vicinity of the lens system has an advantage in that the positional alignment of the projection system and the screen is not required.




The transmittance variable filter is constructed in various styles, and the transmittance thereof is controlled in accordance with the construction. For example, in the transmittance variable filter, a liquid crystal panel is sandwiched between a polarizer and an analyzer, and the transmittance is controlled by changing the voltage applied to the liquid crystal panel. Alternatively, in the transmittance variable filter, two polarizing plates are faced each other and the transmittance is controlled by rotating one of the polarizing plates. In this example, the former construction and transmittance control means are used.




In order to actually operate the system, the reference operating conditions are obtained in the following manner. First, as the optically writing conditions and the driving conditions, V


w


was set to be −2.7 V, T


w


be 1.1 msec. and τ be 0.8. In accordance with Equation (44), L


1


was obtained as 23.8 μW/cm


2


, and L


S


as 363 μW/cm


2


. As the intensity of the light from the reference light generator


2114


, two values were set, e.g., L


A


100 μW/cm


2


and L


B


=400 μW/cm


2


. The output light intensities corresponding to these values were obtained as Y


A


=0.08, and Y


B


−0.49, respectively, on the basis of Equations (34) to (36).




Next, the operation of the operation unit


2111


when the system is actually operated in the above conditions is specifically described. The output light intensities corresponding to the two values of writing light intensities L


A


and L


B


are measured (the measured values are represented by Y


A


′ and Y


B


′, respectively), and the deviation from the reference conditions, i.e., dY


A


−Y


A


′−Y


A


and dY


B


=Y


B


′ are calculated. By applying the calculated values into Equation (39), the changed amount of L


1


and L


S


, i.e., dL


1


and dL


S


are obtained. In Equation (39), the partial differential coefficients such as (∂


Y/∂L




S


)


L=LA


are obtained by applying L


1


=23.8 μW/cm


2


and L


S


=363 μW/cm


2


, and L


A


100 μW/cm


2


and L


B


=400 μW/cm


2


, etc. into partial differential equations of Equation (34) or (35). If dL


1


and dL


S


are actually calculated by Equation (39), the result is given as follows:








dL




1


=−596


dY




A


+97.9


dY




B


  (45)










dL




S


=1149


dY




A


−931


dY




B








Here, the unit of L


1


and L


S


is μW/cm


2


, and dY


A


and dY


B


are dimensionless numbers. If the values of dL


1


and dL


S


are applied into Equation (42), it is determined how much V


w


and τ should be varied. The partial differential coefficients such as ∂L


1


/∂τ in Equation (42) are obtained by applying V


w


−2.7 V, T


w


=1.1 msec. and τ=0.8 into partial differential equations of Equation (44). The equations for actually obtaining dV


w


and dT are given as follows:








dV




w


=(−26.7


dL




1


+1.747


dL




S


)×10


−3


  (46)










dτ=


2.21


dL




S


×10


−3








When V


w


and τ are actually varied by dV


w


and dτ obtained above, the standard input/output light intensity characteristics (L


1


=23.8 μW/cm


2


, L


S


=363 μW/cm


2


) are maintained. The above series of processes are repeated at a predetermined cycle (e.g., 10 sec. ), the input/output light intensity characteristics are always kept constant.




As to the measurement timing, for example, Y


A


is measured in the first 1 sec. of 10 sec. cycle, and Y


B


is measured in the second 1 sec. In the remaining 8 sec., dV


w


and dτ are calculated and the driving conditions and the optically writing conditions are corrected. Alternatively, two reference light generators


2114


which emit two types of light having fixed intensities L


A


and L


B


may be adjacently provided. In such a case, the output Y


A


and Y


B


corresponding thereto are simultaneously monitored.




The system was actually operated in the above manner. The gray-scale display characteristics of the output image on the screen were not changed from the initial conditions even after 500 hours. This means that the input/output light intensity characteristics of the SLM


2103


are kept constant. Next, as an comparative example, the system was operated in the constant driving and optically writing conditions without feedback. The gray-scale display characteristics were changed only after few minutes, and the entire screen was observed as becoming whitish. As a result, it is proved that the feedback stabilizes the gray-scale display characteristics.




In this example, the measurement of Y


A


and Y


B


is performed at one point. Alternatively, in order to increase the accuracy, a plurality of reference light


25


generators


2114


are provided and a plurality of sets (Y


A


, Y


B


) are measured correspondingly. Then, the averaged value is calculated, and used for the process. If the temperature distribution in the effective area of the SLM


2103


is not uniform, for example, the characteristic quantities of the FLC such as P


S


are also varied in an in-plane distribution manner. Therefore, if the transmittance variable filter


2113


has the inplane distribution of the transmittance variation for compensating such temperature distribution in the SLM


2103


, the gray-scale display can be more stably performed




In this example, a monochrome display is performed on the screen. It is appreciated that the display can be expanded into a three-color display. Specifically, for example, when three sets of a CRT and an SLM are used as the optically writing means so as to perform the writing of RGB image signals, respectively, there should be provided three sets of the reference light generators


2114


and the photodetectors


2109


. In each of the sets, prior to the photodetector


2109


, a corresponding set of monochrome filters of red, blue and green is located, so as to detect the light intensity of each color component. Thus, the feedback can separately performed for each of the three sets of driving systems and optically writing systems.




In this example, the SLM having a construction shown in

FIG. 7

is used. Alternatively, for example, even in the cases where SLMs shown in

FIGS. 6 and 8

are used, a stable gray-scale display can be obtained by performing the feedback in the same way.




It is understood that the way of feedback can be applied to, in addition to the projection-type display, a holography television, an optical computer, and the like.




EXAMPLE 7




Next, the system was operated by performing the feedback only to V


w


and T


w


in the driving conditions on the basis of Equation (41) instead of Equation (42). The operation was performed in the same way as in Example 6, except that the feedback was performed for the length of the writing period T


w


, instead of the transmittance of the transmittance variable filter


2113


. As the result of the operation, the same effects could be attained as in Example 6. In the operation method of Example 7, it is possible to eliminate the transmittance variable filter


2113


itself. Thus, the system can have a more simplified construction.




EXAMPLE 8




Next, the system was operated by changing the electron beam current value in the CRT


2101


, instead of changing the transmittance of the transmittance variable filter


2113


in Example 6. Specifically, in an electron gun of the CRT


2101


, a direct current bias voltage is superimposed on a control grid to which a video signal is applied, and the feedback is performed for the direct current bias voltage value, so as to perform the operation. The construction of the system is the same as that shown in

FIG. 21

except that the transmittance variable filter


2113


is not provided and that the feedback is performed for the direct current bias voltage value of the control grid of the CRT


2101


. According to the method of Example 8, the same effects can be attained as in the case where the transmittance variable filter


2113


is provided in front of the CRT


2101


, and the obtained image is as stable as in Example 6.




EXAMPLE 9




Next, the system shown in

FIG. 21

was operated by using a liquid crystal panel with backlight instead of the CRT


2101


. The obtained image was as stable as in the case where the CRT


2101


was used.




It is possible to vary the transmittance by performing the feedback for the driving system of the liquid crystal panel, or to perform the feedback to the brightness of the backlight, instead of the use of the transmittance variable filter


2113


.




In Examples 2 to 9 described above, the CRT is often used as the optical writing means. If the lifetime of the fluorescence is sufficiently longer than the driving pulse period of the SLM (e.g., the lifetime of the fluorescence is 3 msec, while the driving pulse period is 1.2 msec.), the fluorescence from the phosphor on the CRT can be regarded as the continuous light




EXAMPLE 10




Next, the principle for realizing a uniform image display by the method of the invention is described. The timing chart (a) of

FIG. 22

indicates the intensity of an electron beam


2203


in the CRT. The timing chart (b) indicates the emitted light intensity from a phosphor on the CRT screen. The timing charts (c) and (e) indicate the waveforms of driving signals


2208


and


2215


, respectively. The timing charts (d) and (f) indicate the intensities of output light


2209


and output light


2216


from the SLM, respectively. The electron beam scans the CRT screen. In terms of a certain pixel on the CRT, the pixel is reached by the electron beam every one frame (one display period)


2202


of the image. At this time, the intensity of the electron beam


2203


is approximately in proportion to the brightness of the pixel in the image to be displayed on the CRT in the frame. Therefore, the electron beams


2203


having different intensities


2201




a


,


2201




b


, and


2201




c


continuously reach each pixel at a predetermined interval. The phosphor on the CRT emits light having an intensity which is approximately in proportion to the intensity of the reached electron beam


2203


. The emitted light from the phosphor decays with its characteristic time constant. Accordingly, the characteristic curve of the intensity


2204


of the light emitted from the phosphor shown in the timing chart (b) of

FIG. 22

is obtained.




In one frame


2202


of the CRT, when an SLM is driven by a plurality of unit driving signals (driving pulses)


2207


, the intensity


2209


of the output light for each unit driving signal (driving pulse)


2207


is in proportion to the intensity


2204


of the emitted light from the phosphor at that time. As a result, the brightness of the pixel sensed by the eyes of a person, i.e., the time averaged value of the output light intensity


2209


in the frame


2202


is substantially in proportion to the fluorescence intensity


2204


from the phosphor. Accordingly, a faithful image is reproduced on the SLM. As the number of unit driving signals (driving pulses)


2207


in one frame


2202


is increased, the envelope linking the peaks of output light intensity


2209


in each unit driving signal


2207


becomes closer to the curve of fluorescence intensity


2204


shown in the timing chart (b) in FIG.


22


. As a result, the output light intensity


2209


does not depend on the time difference between the driving signal (driving pulse voltage)


2208


and the electron beam intensity


2203


. In other words, in whichever portion of the driving signal


2208


the electron beam pulses


2201


having different intensities


2201




a


,


2201




b


, and


2201




c


enter, the time averaged value of the output light intensity


2209


in one frame


2202


is not so changed. This means that the output light intensity


2209


can be obtained at the same sensitivity with respect to the intensity of the electron beam


2263


in any portion on the screen of the SLM, so that the brightness of the output image of the SLM is uniform.




The image was displayed by using the SLM shown in FIG.


7


and the optical system shown in

FIG. 19

in which the CRT was used as the optical writing means. The pixel pitch of the CRT


1901


may coincide with the pixel pitch of the SLM


1902


, but alternatively may not coincide therewith. In this example, in the employed CRT


1901


, the pixel pitch was 50 μm, and the number of scanning lines was 525. The decay time constant τ of the fluorescence from the phosphor on the CRT expressed by Equation (9) was 7 msec. In order to form the image of the CRT


1901


on the photoconductive layer of the SLM


1902


, an imaging optical system such as a lens system or a SELFOC lens array (the trade mark of NIHON ITA GLASS K.K.) may be inserted.




One frame of the CRT


1901


was 16.7 msec., and the driving period of the SLM


1902


was set to be shorter than this (e.g., about 1 msec.). As to the mutual driving method, they may be driven independently without synchronization, or they may be driven with synchronization by generating a trigger pulse every several times driving periods of the SLM (e.g., every sixteenth period) and sending the trigger pulse to the CRT


1901


. In this optical system, the former method was adopted.




As is shown in the timing chart (c) of

FIG. 22

, the SLM


1902


was actually driven by using a driving signal


2208


including a number of unit driving signals (driving pulses)


2207


, and a moving image was reproduced on the CRT


1901


. Then, the output light from the SLM


1902


was monitored. In the unit driving signal (driving pulse)


2207


, the width of the erasure pulse


2205


was 0.1 msec. and the voltage (height) was +10 V. The width of the reading pulse


2206


was 1.1 msec., and the voltage (height) was −0.91 V. In this case, one period of the CRT was 1.2 msec. The output light from the SLM


1902


was directly monitored by an observer at the position of the lens


1910


via the beam splitter


1904


. As the result of the observation, it was proved that the image-displayed on the CRT


1901


was faithfully reproduced on the output face of the SLM


1902


. The brightness of the reproduced image was uniform over the entire screen of the SLM. In addition, the gray-scale representation was faithfully reproduced. Moreover, for the brightness of the reading light


1908


as much as 10


6


lx, an image with good contrast was obtained. The contrast ratio in this condition was 200:1. On the output face of the SLM, the residual image phenomenon was not observed with respect to the moving image of the CRT. Since conductive polyimide with high stability was used for the alignment film for the liquid crystal molecules of the SLM


1902


, the temporal change did not occur but was stable even after the continuous driving over several hundreds of hours. Therefore, the quality and the brightness of the output image from the SLM would not be changed.




Moreover, the intensity of the reading output light


1909


was detected by the photodetector, and the temporal change was observed with an oscilloscope. As the result of the observation, the waveform of the output light intensity


2209


shown in the timing chart (d) of

FIG. 22

was obtained for the driving signal


2208


shown in the timing chart (c). The envelope smoothly linking the peaks of the output light intensity


2209


in each unit driving signal (driving pulse)


2207


substantially coincided with the waveform of the fluorescence intensity


2204


from the phosphor shown in the timing chart (b). The response of the output light intensity


2209


was not saturated even for the fluorescence intensity


2204


from the phosphor in the case where the intensity pulse of the electron beam


2203


was maximum.




EXAMPLE 11




Next, a driving signal (driving pulse)


2215


including a unit driving signal (driving pulse)


2214


shown in the timing chart (e) of

FIG. 22

was used for driving the optical system shown in FIG.


19


. The unit driving signal


2214


includes an erasure pulse


2210


, a first low voltage pulse


2211


, a writing pulse


2212


, and a second low voltage pulse


2213


. In the unit driving signal (driving pulse)


2214


, the width of the erasure pulse


2210


was 0.1 msec., and the voltage (height) was +10 V. The width of the first low voltage pulse


2211


was 0.1 msec., and the voltage (height) was 0 V. The width of the writing pulse


2212


was 0.1 msec., and the voltage (height) was −10 V. The width of the second low voltage pulse


2213


was 0.9 msec., and the voltage was 0 V. In this example, the SLM having the construction shown in

FIG. 7

was employed. In this case, the image on the CRT


1901


was faithfully reproduced on the output face of the SLM


1902


with uniform brightness. In addition, on the output face of the SLM, the gray-scale representation was performed, and the residual image phenomenon was not observed. The brightness of the reading light from the SLM


1902


could be increased as high as 10


6


lx. However, the switching phenomenon of FLC occurred due to the electric field caused by the writing pulse


2212


included in the driving signal


2215


. Accordingly, the image contrast on the output face of the SLM was somewhat inferior to that in Example 10, and the contrast was 80:1. The reproduced image was observed sufficiently. The positive and negative portions of the driving signal


2215


were symmetric with respect to the voltage, so that the driving stability of SLM was further enhanced. The SLM was stable after continuous driving for several thousands of hours.




In the same way as in Example 10, the intensity of the output light


1909


was detected by the photodetector, and the change as a function of time was observed by the oscilloscope. As a result, the wave-form of the output light intensity


2216


shown in the timing chart (f) in

FIG. 22

was obtained for the driving signal


2215


shown in the timing chart (e).




EXAMPLE 12




Next, in order to study the response characteristics of an SLM, the following experiments were conducted. A halogen lamp was used as the writing light source, instead of the CRT, and how the brightness of the reading light was changed for the intensity of the writing light was observed. In the experiment, in order to examine how liquid crystal molecules are switched for the driving signal (driving pulse), the waveform of the driving signal and the change of the reading light as a function of time were observed by the oscilloscope. The results were shown in FIG.


23


. In

FIG. 23

, the timing chart (a) shows the variation of intensity of the output light from the SLM


717


when the SLM


717


shown in

FIG. 7

is driven by the driving signal


2208


for writing light having various intensities. The driving signal


2208


is substantially the same as the driving signal in Example 10. In the timing chart (a) in

FIG. 23

, the characteristic curve


2304


a indicates the case where the writing light having an intensity of 3000 μW/cm


2


is used, the characteristic curve


2304




b


indicates the case where the writing light having an intensity of 500 μW/cm


2


is used, and the characteristic curve


2304




c


indicates the case where the writing light is not used. It is apparent from the timing chart (a) of

FIG. 23

that as the intensity of the writing light is increased, the output light intensity


2304


in the reading period of the reading pulse


2302


rises more steeply (i.e., more rapidly), and the time average of the reading light intensity becomes larger. In the timing chart (b) of

FIG. 23

, the driving signal (driving pulse voltage)


2303


includes an erasure pulse


2301


and a reading pulse


2302


. It is apparent from the timing chart (b) that a photoelectric current which is in proportion to the writing light intensity is generated in the photoconductive layer in the reading period of the reading pulse


2302


, and charges are accumulated at the interface between the photoconductive layer and the FLC layer. Then, the polarization of the liquid crystals is gradually inverted so as to meet the charge amount. As a result, the gray-scale display of SLM can be obtained.




In the same way, the measurement was performed by using the driving pulse voltage


2215


. The obtained results are shown in FIG.


24


. In the timing chart (a) of

FIG. 24

, the characteristic curve


2406




a


indicates the case where writing light having an intensity of 3000 μW/cm


2


is used, the characteristic curve


2406




b


indicates the case where writing light having an intensity of 500 μW/cm


2


is used, and the characteristic curve


2406




c


indicates the case where writing light is not used. In the timing chart (b) of

FIG. 24

, the driving signal (driving pulse voltage)


2405


includes an erasure pulse


2401


, a first low voltage pulse


2402


, a writing pulse


2403


, and a second low voltage pulse


2404


.

FIG. 24

shows that the gray-scale display is obtained by changing the writing light intensity. When the writing pulse


2403


is applied to the SLM, the electric field switching occurs in the FLC of the SLM. In addition, it is seen that even in the case where the intensity of the writing light is 0, there occurs a slight peak of the output light intensity in the characteristic curve


2406




c.






The time averages of output light intensities for the respective writing light intensities are calculated with respect to the above-described two driving methods.

FIG. 25

shows the calculated results. In

FIG. 25

, the characteristic curve


2501


indicates the case where a driving signal without including a writing pulse in the unit driving signal, e.g., a driving signal


2207


shown in the timing chart (c) of

FIG. 22

is used for driving the SLM. The other characteristic curve


2502


indicates the case where a driving signal with a writing pulse


2212


in the unit driving signal, e.g., a driving signal


2214


shown in the timing chart (e) of

FIG. 22

is used for driving the SLM. In both of the driving methods, it is found that the gray-scale control can be performed in the writing light intensity range of 100 to 1000 μW/cm


2


. In addition, it is found that below 100 μW/cm


2


, the output light intensity is substantially 0, and over 1000 μW/cm


2


the output light intensity is saturated.




The contrast ratio of time averaged reading output light is calculated to be 530:1 for the driving pulse voltage


2208


, and 320:1 for the driving pulse voltage


2215


. Thus, the obtained contrast ratios are relatively good.




EXAMPLE 13




With regard to two types of driving signals (driving pulses), the reading was performed by the optical system shown in

FIG. 19

without changing the pulse waveform and voltage value while changing the period for one cycle. In this way, the uniformity of the brightness of the output light from SLM was measured. An image with uniform brightness which was displayed on the CRT


1901


was written into the SLM


1902


having the construction shown in FIG.


7


. For the output light


1909


from the SLM


1902


, a ratio R of the brightness in the brightest portion to the brightness in the darkest portion was calculated. The ratio R was used as a criteria for judging the nonuniformity of the image brightness. The calculated results are shown in Table 2 below. In Table 2, T


SLM


denotes a period of a driving signal (driving pulse) for the SLM, and T


CRT


denotes one display period of the CRT. Also, R


1


and R


2


denote the ratios R in the cases where the driving signal (driving pulse)


2208


shown in the timing chart (c) in FIG.


22


and the driving signal (driving pulse)


2215


shown in the timing chart (e) are used for the driving, respectively. The period T


CRT


is fixed to be 16.7 msec.

















TABLE 2











T


SLM


(msec.)




T


CRT


/T


SLM






R


1






R


2































0.00835




2000

















0.0167




1000




1.0




1.0







0.167




100




1.0




1.0







1.67




10




1.1




1.1







8.35




2




1.2




1.3







11.1




1.5




2.1




2.0







16.7




1




11.3




12.7







33.4




0.5

























From Table 2, it is found that the output light has substantially uniform intensity when the value of T


CRT


/T


SLM


is in the range of 1.5 to 1000. If the value of T


CRT


/T


SLM


exceeds 1000, the switching speed of the FLC in the SLM cannot follow the change of the driving pulse. As a result, the contrast of the reproduced image on the output face of the SLM is deteriorated. If the value of T


CRT


/T


SLM


becomes smaller than 1, the flicker of the output light becomes noticeable. As a result, the quality of the image is deteriorated.




EXAMPLE 14




In the driving signal (driving pulse)


2208


shown in the timing chart (c) of

FIG. 22

, the length of the period of the erasure pulse


2205


was fixed to be 0.1 msec., and the length of the period of the reading pulse


2206


was fixed to be 1.1 msec. The voltages (heights) of these pulses were varied, so as to drive the SLM


717


having the construction shown in FIG.


7


. In one specific example, the voltage of the erasure pulse


2205


was fixed to be 10 V, and the voltage of the reading period


2206


was varied in the range of −30 V to +2 V. There occurred no change in the quality of the image read out from the SLM. When the voltage of the reading pulse


2206


exceeds +2 V, the photoconductive layer did not generate photoelectric current in the reading period, so that the brightness of the output light was reduced. In another specific example, the voltage of the reading pulse


2206


was fixed to be −0.91 V, and the voltage of the erasure pulse


2205


was varied in the range of +2 V to +30 V. The quality of the image read out from the SLM did not vary so much. When the voltage of the erasure pulse


2205


was lowered to less than +2 V, the photoconductive layer of the SLM did not come into the forward condition, so that the contents recorded in the SLM (in more detail, in the respective pixels of the SLM) could not be properly erased. As a result, the contrast of the image was deteriorated.




EXAMPLE 15




In the driving signal (driving pulse voltage) shown in the timing chart (e) of

FIG. 22

, those used in Example 11 were used as the basic signal, and one of the voltage (heights) of the erasure pulse


2210


, the writing pulse


2212


and the second low voltage pulse


2213


was varied, so as to drive the SLM


717


shown in FIG.


7


. If the voltage of the erasure pulse


2210


was varied, for the same reasons described for the case of the driving signal (driving pulse voltage) in Example 14, an image with good quality was obtained on the output face of the SLM when the voltage of the erasure pulse


2210


was in the range of +2 V to +30 V. If the voltage of the writing pulse


2212


was varied, an image with good quality was obtained on the output face of the SLM when the voltage of the writing pulse


2212


was in the range of −30 V to −2 V. Even when the voltage exceeds −2 V, the image quality is good, but such a range is equivalent to that of the driving signal (driving pulse voltage)


2208


shown in the timing chart (c) of FIG.


22


. Next, the voltage of the second low voltage pulse


2213


was changed. In this case, an image with good quality was obtained on the output face of the SLM in the range of −30 V to −2 V. This period corresponds to the reading period of the reading pulse


2206


in the driving signal


2208


, so that it is thought that the proper operation can be attained only in the voltage range in which the photoconductive layer of the SLM generate a photoelectric current.




EXAMPLE 16




In each of Examples 10 to 15, in one frame


2202


of the timing chart (a) of

FIG. 22

, the waveform of the output light intensity


2209


or


2216


of the SLM shown in the timing chart (d) or (f) reproduces the fluorescence intensity


2204


from a phosphor on the CRT screen shown in the timing chart (b). Accordingly, even if the fluorescence intensity from a phosphor is the maximum, the response of the output light intensity


2209


or


2216


is decreased in the latter half of the frame


2202


. This means that there arises a loss in brightness if the brightness is considered as the integration with respect to time. This example describes a driving method for solving such a problem and for enabling a gray-scale display, in detail.




Herein, it is assumed that the CRT rewrites the images at a frequency f (a period T


CRT


=1/f). The ratio of the driving period T


CRT


of the CRT to the driving period T


SLM


of the SLM is represented by n. In other words, they have the following relationship:








T




CRT




=n×T




SLM


  (47)






For simplicity, n is assumed to be an integer. The following time-averaged value of the output light intensity


2209


shown in the timing chart (d) of

FIG. 22

is actually observed by the eyes of a person, as the output light intensity of the SLM.








Y={ΣY




i


})/


n


  (48)






In Equation (48), Y


i


denotes the output light intensity in each writing period, and Y


i


is given by the relationship shown in

FIG. 25

by using the output light L of the CRT in the unit driving signal (driving pulse)


2207


or


2214


as the writing light intensity.




The output light L of the CRT monotonously decreased as a function of time in one period. Accordingly, the output Y of the SLM in the period T


CRT


is changed in accordance with the relationship between the light output L(t) at the time t and the threshold values L


1


and L


2


(e.g., in the case where the driving is performed by the driving signal


2208


, L


1


=100 μW/cm


2


and L


2


=1000 μW/cm


2


in FIG.


25


). The variation of the output Y


i


when n=16 in Equation (47) is shown in FIG.


26


. In

FIG. 26

, the timing chart (a) indicates the light output from the CRT when the light output L at the time t=T


CRT


is larger than the threshold value L


2


, and the timing chart (b) indicates the intensity of the output light from the SLM in such a case. The timing chart (c) indicates the light output from the CRT in the case where L=L


2


at time t=T


1


, and the light output L at time t=T


CRT


is larger than L


1


. The timing chart (d) indicates the intensity of the output light from the SLM in such a case. The timing chart (e) indicates the light output from the CRT when L<L


1


at t=T


2


, and the timing chart (f) indicates the intensity of the output light from the SLM in such a case. The change of L in each unit driving signal (driving pulse)


2207


is negligible.




As is expressed by Equation (48), the light output of the SLM is represented as the linear sum of the light pulse intensities Y


i


output for each driving period of the SLM. In this case, each pulse intensity Y


i


when L≧L


2


can be approximated as being substantially constant. If each pulse intensity Y


i


when L


1


≦L<L


2


can be divided into at least m scales in accordance with L, it is possible to easily realize at least n×m gray-scales by the above-described driving method of the invention. In the SLM having the construction shown in

FIG. 6

or


7


which is actually produced in the experiment, the number of levels m into which Y


i


can be divided in accordance with L is as much as 90. Therefore, in order to realize 256 gray-scales, it is preferred to be at least n≧3.




By using the driving pulse


2208


, T


CRT


was set to be 16.7 msec., and T


SLM


was equal to T


CRT


/16, i.e., 1.04 msec., so as to actually display an image. In the driving signal (driving pulse)


2208


, the width of the erasure pulse was set to be 0.104 msec. and the voltage to be 15 V. The width of the writing pulse was set to be 0.936 msec. and the voltage to be −3.63 V. In these driving conditions, the response was the same as that shown in FIG.


25


. Two threshold values L


1


and L


2


were actually calculated to be L


1


=100 μW/cm


2


, and L


2


=800 μW/cm


2


.




According to the driving method of the invention, it is necessary to carefully treat the residual image phenomenon which depends on the decay characteristics of the fluorescence (output L) of the CRT. For example, as is shown in the timing charts (a) and (b) in

FIG. 26

, when the brightest light output Y is to be obtained, L≧L


2


at time t=T


CRT


. Accordingly, if black is to be displayed in the next period (T


CRT




≧t


≧2T


CRT


), Y>0 since L>L


1


. That is, if the first image display means (e.g., CRT) rewrites the image at 60 Hz, the actually observed image is not rewritten at 60 Hz, so that there occurs the residual image phenomenon. In order that the residual image cannot be observed by the eyes of a person, it is necessary to attenuate the light output L to be lower than L


i


after at least the time t=2T


CRT


. In other words, it is necessary to use a phosphor with residual light characteristics by which the light amount of L


2


decays below L


1


within T


CRT


.




The phosphor on the CRT used as the first image display means in this example has the characteristic shown by Equation (49):








L=L




i




exp


(−


t


/τ)(0


≧t≧T




CRT


)  (49)






In Equation (49), L


i


denotes the initial value of the fluorescence intensity of the CRT, and τ denotes the decay time constant. In the phosphor used in this example, τ=8 msec. Accordingly, at time t=T


CRT


, L is 0.124 L


i


, and at time t=


2


T


CRT


, L is 0.015 L


i


. In the case where the brightest output Y is to be obtained, L


i


was set so as to satisfy the condition of 0.124 L


i


=L


2


=800 μW/cm


2


. Thus, L


i


was set to be 6450 μW/cm


2


. At this time, 0.015 L


i


=97 μW/cm


2


<L


i


, so that the residual image could be suppressed to be minimum.




In order to reduce the initial light amount L


i


, it is sufficient to increase τ and L


1


/L


2


. For example, it is assumed that τ=440 msec. (i.e., it is assumed that L=0.103 L


i


at time t=1 s), the residual light at time t=T


CRT


was 0.963 L


i


and the residual light at time t=2 T


CRT


was 0.927 L


i


. Accordingly, the initial light amount for obtaining the brightest output Y could be reduced to be L


i


=11.4 μW/cm


2


. In addition, by increasing the ratio of L


1


to L


2


of the SLM (in this case, L


1


/L


2


=0.963), the residual light can be suppressed to a minimum.




In this example, the case where the driving signal (driving pulse voltage)


2208


is used is mainly described. Alternatively, in the case of the driving signal (driving pulse voltage)


2215


, the signal includes two threshold values as is shown in

FIG. 25

, so that the operation can be performed by the same method.




The invention provides a driving method for an SLM which can perform a gray-scale display with high contrast, uniformity and controllability, and which is stable for a long time use. A projection-type display adopting the driving method can obtain a faithful gray-scale display with good contrast. A holography television apparatus adopting the driving method can obtain a vivid three-dimensional image with reduced noise.




Various other modifications will be apparent to and can be readily made by those skilled in the art without departing from the scope and spirit of this invention. Accordingly, it is not intended that the scope of the claims appended hereto be limited to the description as set forth herein, but rather that the claims be broadly construed.



Claims
  • 1. A spatial light modulator according to claim 1, wherein said photoconductive layer has rectification, and generates, when said photoconductive layer is in a reversed bias condition, a photoelectric current having a magnitude depending on an intensity of writing light incident on said photoconductive layer.
  • 2. A spatial light modulator according to claim 1, wherein said light-modulating layer includes a ferroelectric liquid crystal layer which is sandwiched by two alignment films.
  • 3. A spatial light modulator according to claim 2, wherein a specific resistance of said alignment films is in the range of 108 Ω·cm to 1011 Ω·cm.
  • 4. A driving method for a spatial light modulator,wherein said spatial light modulator includes a pair of facing transparent electrodes, and a light-modulating layer and a photoconductive layer provided between said transparent electrodes, said light-modulating layer having different optical states depending on an applied charge amount, said light-modulating layer having: a first optical state when said applied charge amount is a first threshold charge amount or more; a second optical state then said applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between said first optical state and said second optical state depending on said applied charge amount, wherein said photoconductive layer has rectification, and generates, when said photoconductive layer is in a reversed bias condition, a photoelectric current having a magnitude depending on an intensity of writing light incident on said photoconductive layer, wherein one period of a waveform of a driving voltage includes an erasure period in which the photoconductive layer is in a forward bias condition and a charge amount larger than said first threshold charge amount is applied, and a writing period in which the photoconductive layer is in a reversed bias condition so as to generate a photoelectric current having a magnitude depending on an intensity of writing light, and wherein said method includes a step of applying said driving voltage to said two transparent electrodes, so that in said writing period, said applied charge amount to said light-modulating layer is kept in the range of said first threshold charge amount or more when the intensity of said writing light is a first threshold light intensity or lower, and said applied charge amount to said light-modulating layer is reduced to said second threshold charge amount or less when the intensity of said writing light is a second threshold light intensity of higher.
  • 5. A driving method according to claim 4, wherein said light-modulating layer includes a ferroelectric liquid crystal layer which is sandwiched by two alignment films, andwherein conditions of: −Vth≦(CfVe+CaVw)/(Cf+Ca)−Vd, and Vw−Vd≦−Vth are satisfied, where Ve denotes the maximum value of the driving voltage in said erasure period, Vw denotes the minimum value of the driving voltage in said writing period, Cf denotes a capacitance of said ferroelectric liquid crystal layer without polarization inversion of said ferroelectric liquid crystal layer, Ca denotes a capacitance of said photoconductive layer, Vd denotes a diffusion potential of said photoconductive layer, and −Vth denotes a threshold voltage of said ferroelectric liquid crystal layer.
  • 6. A driving method according to claim 5, wherein the driving voltage Ve in said erasure period and the driving voltage Vw in said writing period are respectively in the ranges of:1 V≦Ve≦40 V, and −20 V≦Vw≦4 V.
  • 7. A driving method according to claim 5, wherein said ferroelectric liquid crystal layer and said photoconductive layer are electrically in contact with each other via a metal reflection film which is divided and separated into minute portions.
  • 8. A driving method according to claim 4, wherein one period of said driving voltage waveform for driving said spatial light modulator is shorter than one display period of an image formed by said writing light.
  • 9. A driving method according to claim 8, wherein a ratio of one display period of an image formed by said writing light to one period of said driving voltage is in the range of 1.5 to 1000.
  • 10. A driving method according to claim 8, wherein the output light intensity of said spatial light modulator with respect to the writing light intensities with said first threshold light intensity or lower of said spatial light modulator is substantially 0, the output light intensity with respect to the writing light intensities between said first threshold light intensity and said second threshold light intensity is increased as the writing light intensity is increased, and the output light intensity with respect to the writing light intensities which exceeds said second threshold light intensity has substantially no dependence on said writing light intensity.
  • 11. A driving method according to claim 8, wherein the writing light intensity to said spatial light modulator is substantially monotonously decreased as a function of time in one display period of an image formed by said writing light, the maximum value of said writing light intensity directly prior to the end of said display period is said second threshold light intensity or higher, and said maximum value decays to be said first threshold light intensity or lower in a period in which an image is rewritten by said writing light.
  • 12. A driving method according to claim 8, wherein said writing light is generated from a CRT.
  • 13. A driving method according to claim 8, wherein the driving voltage applied in said erasure period is in the range of +2 V to +30 V by regarding a direction in which the photoconductive layer is forward-biased as a positive, and the driving voltage applied in said writing period is in the range of −30 V to +2 V.
  • 14. A driving method according to claim 8, wherein one period of the driving voltage is constituted by a sequence of said erasure period, a first low voltage period, said writing period, and a second low voltage period.
  • 15. A driving method according to claim 14, wherein said second low voltage period is longer than said first low voltage period.
  • 16. A driving method according to claim 14, wherein the driving voltage applied in said erasure period is in the range of +2 V to +30 V by regarding a direction in which the photoconductive layer is forward-biased as a positive, the driving voltage applied in said writing period is in the range of −30 V to −2 V, and the driving voltage applied in the second low voltage period is in the range of −2 V to +2 V.
  • 17. A driving method for a spatial light modulator,wherein said spatial light modulator includes a pair of facing transparent electrodes, and a light-modulating layer and a photoconductive layer provided between said transparent electrodes, said light-modulating layer having different optical states depending on an applied charge amount, said light-modulating layer having: a first optical state when said applied charge amount is a first threshold charge amount or more; a second optical state when said applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between said first optical state and said second optical state depending on said applied charge amount, and wherein said driving method includes the steps of: applying a driving voltage to said two transparent electrodes; irradiating said spatial light modulator with writing light; measuring an output light intensity of said spatial light modulator with respect to at least one writing light intensity; detecting a change of the output light intensity as a function of time; and performing a feedback to at least one of the writing light intensity and the driving voltage, in accordance with the detected change of the output light intensity, in order to keep a ratio of writing light intensity to output light intensity approximately constant.
  • 18. A driving method according to claim 17, wherein said photoconductive layer has rectification, and generates, when said photoconductive layer is in a reversed bias condition, a photoelectric current having a magnitude depending on an intensity of writing light incident on said photoconductive layer,wherein one period of a waveform of a driving voltage includes an erasure period in which the photoconductive layer is in a forward bias condition and a charge amount larger than said first threshold charge amount is applied, and a writing period in which the photoconductive layer is in a reversed bias condition so as to generate a photoelectric current having a magnitude depending on an intensity of writing light, and wherein the driving voltage, in said writing period, keeps said applied charge amount to said light-modulating layer in the range of said first threshold charge amount or more when the intensity of said writing light is a first threshold light intensity or lower, and reduces said applied charge amount to said light-modulating layer to said second threshold charge amount or less when the intensity of said writing light is a second threshold light intensity of higher.
  • 19. A driving method according to claim 18, wherein said light-modulating layer includes a ferroelectric liquid crystal layer which is sandwiched by two alignment films,wherein conditions of: −Vth<(CfVe+CaVw)/(Cf+Ca)−Vd, and Vw−Vd≦−Vth are satisfied, where Ve denotes the maximum value of the driving voltage in said erasure period, Vw denotes the minimum value of the driving voltage in said writing period, Cf denotes a capacitance of said ferroelectric liquid crystal layer without polarization inversion of said ferroelectric liquid crystal layer, Ca denotes a capacitance of said photoconductive layer, Vd denotes a diffusion potential of said photoconductive layer, and −Vth denotes a threshold voltage of said ferroelectric liquid crystal layer,wherein said driving method includes a step of keeping values of L1 and Ls constant by changing at least one of Ve, Vw, Tw and τ, said values of L1 and Ls being defined by L1=(hν/ηe)(Cf+Ca)(Vf0+Vth)/Twτ, Ls=(hν/ηe)(2Ps/Twτ), and Vf0=(CfVe+CaVw)/(Cf+Ca)−Vd, where Tw denotes a width of said writing period, τ denotes a ratio (utilization efficiency) of an intensity of light actually incident on said photoconductive layer to the intensity of said writing light, hν denotes a photon energy of said writing light, η denotes a quantum efficiency of said photoconductive layer, e denotes an electron charge, and Ps denotes a magnitude of spontaneous polarization.
  • 20. A driving method according to claim 19, wherein said ferroelectric liquid crystal layer and said photoconductive layer are electrically in contact with each other via a metal reflection film which is divided and separated into minute portions.
  • 21. A driving method according to claim 18, further comprising the steps of:measuring changes dYA and dYB in output light intensities of said spatial light modulator as a function of time with respect to two different writing light intensities L=LA and L=LB; obtaining changes dL1 and dLs of L1 and Ls by using equations of dL1=[(∂Y/∂Ls)L=LB·dYA−(∂Y/∂Ls)L=LA·dYB]/Δ, dLs=[−(∂Y/∂L1)L=LB·dYA+(∂Y/∂L1)L=LA·dYB]/Δ, and Δ=(∂Y/∂L1)L=LA·(∂Y/∂Ls)L=LB−(∂Y/∂Ls)L=LA·(∂Y/∂L1)L=LB; and changing Ve, Vw, Tw and τ by amounts equal to dVe, dVw, dTw and dτ, respectively, so as to satisfy relationships of −dL1=(∂L1/∂Ve)dVe+(∂L1/∂Vw)dVw+(∂L1/∂Tw)dTw+(∂L1/∂τ)dτ, and −dLs=(∂Ls/∂Tw)dTw+(∂Ls/∂τ)dτwhere Ve denotes the maximum value of the driving voltage in said erasure period, Vw denotes the minimum value of the driving voltage in said writing period, Tw denotes a width of said writing period, and τ denotes a ratio (utilization efficiency) of an intensity of light actually incident on said photoconductive layer to the intensity of said writing light.
  • 22. A driving method according to claim 18, further comprising the steps of:measuring changes dYA and dYB in output light intensities of said spatial light modulator as a function of time with respect to two different writing light intensities L=LA and L=LB; obtaining changes dL1 and dLs of L1 and Ls by using equations of dL1=[(∂Y/∂Ls)L=LB·dYA−(∂Y/∂Ls)L=LA·dYB]/Δ, dLs=[−(∂Y/∂L1)L=LB·dYA+(∂Y/∂L1)L=LA·dYB]/Δ, and Δ=(∂Y/∂L1)L=LA·(∂Y/∂Ls)L=LB−(∂Y/∂Ls)L=LA·(∂Y/∂L1)L=LB; and changing Ve, Vw, Tw and τ by amounts equal to dVe, dVw, dTw and dτ, respectively, so as to satisfy relationships of: dVe=0, dVw=[(∂L1/∂Tw)dLs−(∂Ls/∂Tw)dL1]/[(∂L1/∂Vw)(∂Ls/∂Tw)], dTw=−(∂Ls/∂Tw)−1dLs, and dτ=0 where Ve denotes the maximum value of the driving voltage in said erasure period, Vw denotes the minimum value of the driving voltage in said writing period, Tw denotes a width of said writing period, and τ denotes a ratio (utilization efficiency) of an intensity of light actually incident on said photoconductive layer to the intensity of said writing light.
  • 23. A driving method according to claim 18, further comprising the steps of:measuring changes dYA and dYB in output light intensities of said spatial light modulator as a function of time with respect to two different writing light intensities L=LA and L=LB; obtaining changes dL1 and dLs of L1 and Ls by using equations of dL1=[(∂Y/∂Ls)L=LB·dYA−(∂Y/∂Ls)L=LA·dYB]/Δ, dLs=[−(∂Y/∂Ls)L=LB·dYA+(∂Y/∂Ls)L=LA·dYB]/Δ, and Δ=(∂Y/∂L1)L=LA·(∂Y/∂Ls)L=LB−(∂Y/∂Ls)L=LA·(∂Y/∂L1)L=LB; and changing Ve, Vw, Tw and τ by amounts equal to dVe, dVw, dTw and dτ, respectively, so as to satisfy relationships of dVe=0, dVw=[(∂L1/∂τ)dLs−(∂Ls/∂τ)dL1]/[(∂L1/∂Vw)(∂Ls/∂τ)], dTw=0, and dτ=−(∂Ls/∂τ)−1dLs where Ve denotes the maximum value of the driving voltage in said erasure period, Vw denotes the minimum value of the driving voltage in said writing period, Tw denotes a width of said writing period, and τ denotes a ratio (utilization efficiency) of an intensity of light actually incident on said photoconductive layer to the intensity of said writing light.
  • 24. A driving method according to claim 18, comprising a step of measuring output light intensities of said spatial light modulator with respect to three or more different writing light intensities.
  • 25. A driving method according to claim 18, further comprising the steps of:irradiating said spatial light modulator with said writing light via an image presentation portion and an intensity modulating portion which modulates an intensity of an image presented on said image presentation portion; and performing a feedback to a transmittance of said intensity modulating portion, in accordance with a change of the output light intensity as a function of time.
  • 26. A driving method according to claim 18, wherein said writing light is generated from a CRT, and said driving method comprises a step of performing a feedback to an electron beam current value of said CRT in accordance with the change of the output light intensity as a function of time.
  • 27. A driving method according to claim 18, wherein the measurement of the output light intensities of said spatial light modulator is performed directly after the output side of said spatial light modulator.
  • 28. A spatial light modulating apparatus comprising:a spatial light modulator including a light-modulating layer and a photoconductive layer provided between two facing transparent electrodes, said light-modulating layer having different optical states depending on an applied charge amount, said light-modulating layer having: a first optical state when said applied charge amount is a first threshold charge amount or more; a second optical state when said applied charge amount is a second threshold charge amount or less; and a spatially uniform intermediate state between said first optical state and said second optical state depending on said applied charge amount; means for applying a driving voltage to said two transparent electrodes; means for irradiating said spatial light modulator with writing light; means for measuring an output light intensity of said spatial light modulator with respect to at least one writing light intensity; means for detecting a change of the output light intensity as a function of time with respect to said at least one writing light intensity; and means for performing a feedback to at least one of the writing light intensity and the driving voltage in accordance with the detected change of the output light intensity in order to keep a ratio of writing light intensity to output light intensity approximately constant.
  • 29. A liquid crystal device including a ferroelectric liquid crystal layer sandwiched by two opposing alignment films, and means for applying charges to said ferroelectric liquid crystal layer whereby said ferroelectric liquid crystal layer exhibits a spatially uniform intermediate state between bistable states, wherein a specific resistance of said alignment films is in the range of 108 Ω·cm to 1011 Ω·cm.
Priority Claims (3)
Number Date Country Kind
5-068525 Mar 1993 JP
5-104051 Apr 1993 JP
5-138066 Jun 1993 JP
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4984198 Kobayashi et al. Jan 1991 A
5089812 Fuse et al. Feb 1992 A
5130830 Fukushima et al. Jul 1992 A
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5364668 Takimoto et al. Nov 1994 A
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Number Date Country
0385346 Sep 1990 EP
0494452 Jul 1992 EP
0508227 Oct 1992 EP
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