Multilens imaging apparatus with correction of misregistration

Abstract: This invention relates to a multi-lens imaging apparatus and, more particularly, to a multi-lens imaging apparatus for obtaining a single high-fine image by synthesizing a plurality of images obtained by picking up an image of a common object using a plurality of imaging systems and to an apparatus which can provide an image having an aspect ratio different from that of an image obtained by a single imaging apparatus, especially, a panoramic image, by synthesizing a plurality of images using a plurality of imaging systems. This invention has as its object to obtain a high-fine image by synthesizing images from a plurality of imaging systems and, more specifically, to correct mis-registration such as keystone distortions generated in the images.

Description: The present invention relates to a multi-lens imaging apparatus and, more particularly, to a multi-lens imaging apparatus which obtains a single high-fine image by synthesizing a plurality of images obtained by picking up a common object image using a plurality of imaging systems and to an apparatus which can provide a image having a different aspect ratio from that of a image obtained by a single imaging apparatus, for example, a panoramic image, by synthesizing a plurality of images obtained using a plurality of imaging optical systems. Document GB-A-2 226 923 discloses an automatic convergent stereoscopic machine vision, wherein an automatic focusing and an automatic convergence can be obtained. The system operating on the basis of a closed-loop servo system comprises a plurality of imaging optical systems, the image fields of which at least partially overlap each other due to optical axis intersecting space. Furthermore, the system includes detection means for extracting and evaluating image signals of the plurality of imaging optical systems, wherein specifically the overlapping portions of the images are considered by using correlation matching within the overlapping portions. Each of the plural imaging optical systems is simultaneously focused with the other imaging optical systems and, thereupon, the views of the imaging optical systems are converged onto the same spot, thereby performing a correction of the detected displacement amounts of the registration in accordance with the detection signals of the detection means for obtaining an accurate view composed of the particular views of the plural imaging optical systems. Furthermore, document EP-A-0 335 004 discloses a corresponding device in the form of a three-dimensional shooting video camera apparatus, wherein a plurality of video camera main bodies is coupled in such a way that the video cameras synchronously operate on the basis of the same photographing conditions. These photographing conditions are detected and evaluated, and a correction thereof is provided for the purpose that both cameras have an identical setting with respect to the photographing conditions which is then automatically carried out. In general, when an ultra high-fine image consisting of 4,000 x 4,000 pixels is picked up by an imaging system, and the picked-up image is displayed on an ultra high-fine monitor, problems associated with techniques for achieving a high density and a high sensitivity in the imaging system are posed. As a method of solving such problems in the imaging system, the principle of a multi-lens imaging apparatus for picking up an image of a common object using two imaging systems each having a small number of pixels, and obtaining a single high-fine image by synthesizing the two images obtained by the two imaging systems has been proposed. In the multi-lens imaging apparatus based on this principle, as shown in Fig. 1, right and left side imaging systems 110 R and 110 L are prepared, and pick up an image of an object 101 by shifting their sampling points by a 1/2 spatial phase pitch. A right side image I R obtained by the right side imaging system 110 R and a left side image I L obtained by the left side imaging system 110 L are synthesized by a microprocessor (to be referred to as a "CPU" hereinafter) 120, thereby obtaining a single high-fine output image I OUT as compared to an image obtained when the image of the object 101 is picked up by a single imaging system. Fig. 2 is an explanatory view for explaining a basic arrangement of the right and left side imaging systems 110 R and 110 L shown in Fig. 1. The left side imaging system 110 L is constituted by a left side imaging optical system 111 L and a left side image sensor 112 L , and the right side imaging system 110 R is constituted by a right side imaging optical system 111 R and a right side image sensor 112 R . The right and left side imaging optical systems 111 R and 111 L have equivalent specifications, and each comprises a zoom lens. The right and left side image sensors 112 R and 112 L have equivalent specifications, and each comprises a camera tube such as a saticon or a solid-state imaging element such as a CCD. Optical axes L R and L L of the right and left imaging systems 110 R and 110 L cross almost at a point O on an object surface 102, and these systems are arranged at positions axially symmetrical about a normal 0-0' to the object surface 102. When the angle formed between each of the optical axes L R and L L and the normal 0-0' to the object surface 102 (to be referred to as an "inclination angle" hereinafter) is represented by , 2 is defined as the convergence angle. In the multi-lens imaging apparatus, when the object distance is changed, the convergence angle 2 is changed by rotating each of the right and left side imaging systems 110 R and 110 L about an X mark shown in Fig. 2 in accordance with the change in object distance, thus performing an imaging operation. However, in the above-mentioned multi-lens imaging apparatus, only the principle shown in Fig. 1 and the results of principle experiments for demonstrating the principle are presented, and no detailed arrangement of the multi-lens imaging apparatus is presented. Thus, a problem associated with how to arrange the detailed multi-lens imaging apparatus utilizing the above-mentioned principle remains unsolved. Since the optical axes L R and L L of the right and left side imaging systems 110 R and 110 L are inclined with respect to the object surface 102, the right and left side images I R and I L obtained by the right and left side image sensors 112 R and 112 L suffer from trapezoidal distortions (to be referred to as "keystone distortions" hereinafter), as shown in Fig. 3. As a result, when the right and left side images I R and I L are merely synthesized, a high-fine image cannot be obtained. Since the optical systems are arranged to have a convergence angle therebetween in principle, mis-registration between images obtained from the two imaging operation systems may occur. Fig. 4A shows the outline of mis-registration in a multi-lens imaging system. The system shown in Fig. 4A includes imaging optical systems (lenses) 910 and 920, and image sensors 911 and 921. The imaging optical systems 910 and 920 have optical axes 912 and 922, respectively. When an object image is picked up while the optical axes 912 and 922 are inclined through  in the x-z plane with respect to a central axis 0-0', an arbitrary object point on an object surface is represented by P. At this time, if image points of the image sensors 911 and 921 with respect to P are respectively represented by R' and L', since R' ≠ L', mis-registration occurs, and two images with respect to the object point P are formed on a simply added synthesized image 930, as shown in Fig. 4B. As a result, a high-fine image cannot be provided. Conventionally, as a panoramic imaging apparatus using a plurality of imaging optical systems and designed for dynamic images, for example, Japanese Laid-Open Patent Application No. JP-A-63-8641 is known. In an apparatus of this type, in general, the angle formed between the imaging optical systems is set by mechanical adjustment, so that image fields contact each other. However, it is very difficult to strictly register two adjacent images, and the boundary line between the two images normally becomes conspicuous. For the same reason as described above, since it is difficult to re-focus objects having different object distances or to perform zooming of these objects, the above-mentioned apparatus is limited to a cut photographing use in units of scenes. As a method of changing the aspect ratio of a frame of a television or video signal (e.g., conversion between 4 : 3 of the NTSC and 16 : 9 of the HD or ED2), a method of trimming upper and lower portions or right and left portions of the frame is known. In this method, since a picked-up image is partially used, when an image is picked by an NTSC camera using a 4 : 3 image sensor, and is output onto a 16 : 9 HD monitor, a total of 25% upper and lower images are lost in addition to the fact that the number of pixels is originally short, thus considerably deteriorating image quality. Conversely, when an image is picked up by a 16 : 9 HD camera, and is output onto a 4 : 3 NTSC monitor, no problem associated with image quality is posed, but the horizontal field angle is decreased by 1/3. SUMMARY OF THE INVENTION It is an object of the present invention to obtain a high-fine image by synthesizing images from a plurality of imaging systems and, more specifically, to correct mis-registration such as keystone distortions generated in the images. In order to achieve the above object, there is provided a multi-lens apparatus as claimed in appended claim 1. According to the present invention, an image having a desired aspect ratio and almost free from image deterioration can be obtained, and a panoramic image in which a boundary line is not conspicuous can also be obtained. According to the present invention, when a plurality of images is synthesized, the mis-registration amount of overlapping images may be partially detected. According to the present invention, means for setting a convergence angle of imaging systems to be a predetermined value may be arranged so as to change the aspect ratio of an image. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a view for explaining the principle of a multi-lens imaging apparatus for obtaining a single high-fine image by synthesizing two images obtained by picking up an image of a common object using two imaging systems; Fig. 2 is an explanatory view for explaining a basic arrangement of right and left side imaging systems shown in Fig. 1; Fig. 3 is an explanatory view for explaining keystone distortions generated in images obtained by right and left side image sensors shown in Fig. 1; Figs. 4A and 4B are explanatory views of mis-registration occurring in the prior art; Figs. 5A and 5B show a multi-lens imaging apparatus according to an embodiment of the present invention, in which Fig. 5A is a perspective view showing the arrangement of right and left imaging systems, and Fig. 5B is a block diagram for explaining operations of keystone distortion correction signal generation portions; Fig. 6 is an explanatory view for explaining the principle of correcting keystone distortions in the keystone distortion correction signal generation portions shown in Fig. 5B; Fig. 7 is an explanatory view for explaining the principle of correcting keystone distortions in the keystone distortion correction signal generation portions shown in Fig. 5B; Fig. 8 is an explanatory view for explaining the principle of correcting keystone distortions in the keystone distortion correction signal generation portions shown in Fig. 5B; Fig. 9 is an explanatory view for explaining operations of camera tube electron beam scanning locus control drivers shown in Fig. 5B; Fig. 10 is a perspective view showing the arrangement of right and left side imaging systems in a multi-lens imaging apparatus according to another embodiment of the present invention; Fig. 11 is a block diagram for explaining operations of correction conversion portions in the multi-lens imaging apparatus according to the embodiment shown in Fig. 10; Fig. 12 is a perspective view showing the arrangement of right and left side imaging systems in a multi-lens imaging apparatus according to still another embodiment of the present invention; Fig. 13 is a block diagram showing operations of correction optical systems shown in Fig. 12; Fig. 14 is an explanatory view for explaining the principle of correcting keystone distortions in the correction optical systems shown in Fig. 12; Fig. 15 is an explanatory view for explaining the principle of correcting keystone distortions in the correction optical systems shown in Fig. 12; Fig. 16 is an explanatory view for explaining the principle of correcting keystone distortions in the correction optical systems shown in Fig. 12; Figs. 17A and 17B show a multi-lens imaging apparatus according to still another embodiment of the present invention, in which Fig. 17A is a perspective view showing the arrangement of right and left side imaging systems, and Fig. 17B is a block diagram for explaining a correction method of keystone distortions; Fig. 18 is an explanatory view for explaining operations of a keystone distortion conversion portion and a subtraction process circuit shown in Fig. 17B; Fig. 19 is a graph showing the relationship between the image difference and the inclination angle (conversion variable); Figs. 20A and 20B show a multi-lens imaging apparatus according to still another embodiment of the present invention, in which Fig. 20A is a perspective view showing the arrangement of right and left side imaging systems, and Fig. 20B is a block diagram for explaining a correction method of keystone distortions; Figs. 21A to 21C show a multi-lens imaging apparatus according to still another embodiment of the present invention, in which Fig. 21A is a perspective view showing the arrangement of right and left side imaging systems, Fig. 21B is a block diagram for explaining an operation of a control portion, and Fig. 21C is a block diagram for explaining an image synthesizing operation; Fig. 22 is an explanatory view for explaining a basic arrangement of imaging systems in the multi-lens imaging apparatus according to the embodiment shown in Figs. 21A to 21C; Fig. 23 is a view for explaining response characteristics of each convergence angle motor shown in Fig. 21A; Figs. 24A and 24B show a multi-lens imaging apparatus according to still another embodiment of the present invention, in which Fig. 24A is a perspective view showing the arrangement of right and left side imaging systems, and Fig. 24B is a block diagram for explaining an operation of a calculation control portion; Figs. 25A and 25B show a multi-lens imaging apparatus according to still another embodiment of the present invention, in which Fig. 25A is a perspective view showing the arrangement of right and left side imaging systems, and Fig. 25B is a block diagram for explaining an operation of a calculation control portion; Figs. 26A and 26B show a multi-lens imaging apparatus according to still another embodiment of the present invention, in which Fig. 26A is a perspective view showing the arrangement of right and left side imaging systems, and Fig. 26B is a block diagram for explaining an operation of a calculation control portion; Fig. 27 is a block diagram for explaining an operation of a correlation calculation process portion in a multi-lens imaging apparatus according to still another embodiment of the present invention; Fig. 28 is a block diagram for explaining an operation of a magnification correlation calculation process portion in a multi-lens imaging apparatus according to still another embodiment of the present invention; Fig. 29 is an explanatory view for explaining a method of shortening the correlation calculation time in the magnification correlation calculation process portion shown in Fig. 28; Fig. 30 is an explanatory view for explaining another method of shortening the correlation calculation time in the magnification correlation calculation process portion shown in Fig. 28; Fig. 31 is a view showing a basic arrangement according to still another embodiment of the present invention; Fig. 32 is a perspective view of optical systems of the embodiment shown in Fig. 31; Fig. 33 is a diagram showing the flow of a signal process for calculating a mis-registration amount; Fig. 34 is a view for explaining a problem; Fig. 35 is a diagram showing the flow of a compensation signal process in the embodiment shown in Fig. 31; Fig. 36 is a diagram showing the flow of a image signal process in the embodiment shown in Fig. 31; Fig. 37 is a perspective view showing optical systems according to still another embodiment of the present invention; Fig. 38 is a diagram showing the flow of a compensation signal process in the embodiment shown in Fig. 37; Fig. 39 is a perspective view showing optical systems according to still another embodiment of the present invention; Fig. 40 is a diagram showing the flow of a compensation signal process in the embodiment shown in Fig. 39; Fig. 41 is a perspective view showing optical systems according to still another embodiment of the present invention; Fig. 42 is a diagram showing the flow of a compensation signal process in the embodiment shown in Fig. 41; Fig. 43 is a perspective view showing optical systems according to still another embodiment of the present invention; Fig. 44 is a diagram showing the flow of a signal process for calculating a mis-registration amount; Fig. 45 is a perspective view for explaining an optical effect; Fig. 46 is an explanatory view for explaining a method of obtaining an image having a desired aspect ratio; Fig. 47 is an explanatory view of the aspect ratio; Fig. 48 is a view showing an optical basic arrangement; Fig. 49 is a view showing a basic arrangement according to still another embodiment of the present invention; Fig. 50 is a perspective view showing the detailed arrangement of the embodiment shown in Fig. 49; Fig. 51 is a block diagram showing relationships among functions in the embodiment shown in Fig. 49; Fig. 52 is an explanatory view associated with a method of calculating three-dimensional position information of an object; Fig. 53 is an explanatory view associated with a method of calculating two-dimensional position information of an object; Figs. 54A and 54B are views showing a correlation calculation process; Fig. 55 is a graph showing a correlation value; and Fig. 56 is an explanatory view of an image correction process. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Figs. 5A and 5B show an arrangement of a multi-lens imaging apparatus according to an embodiment of the present invention. The multi-lens imaging apparatus of this embodiment obtains a single high-fine image by synthesizing two images obtained by picking up an image of a common object using two imaging systems (right and left side imaging systems 10 R and 10 L ) The arrangement of the right and left side imaging systems 10 R and 10 L will be described in detail below with reference to Fig. 5A. The left side imaging system 10 L includes a left side imaging optical system 11 L (see Fig. 8), a left side image sensor 12 L comprising a camera tube, and a camera tube electron beam scanning locus control driver 31 L for controlling the locus of scanning of the electron beam emitted from the camera tube constituting the left side image sensor 12 L . The left side imaging optical system 11 L includes lens groups 21 L to 24 L including a zoom lens group 22 L and a focus lens group 24 L , a zoom motor 25 L as a driving system for driving the zoom lens group 22 L , a focus motor 26 L as a driving system for driving the focus lens group 24 L , a mechanism system (not shown) and a driving system (convergence angle motor 27 L ) for integrally rotating the left side imaging optical system 11 L and the left side image sensor 12 L in a plane including an optical axis L L , and a rotational angle detecting means 28 L for detecting the rotational angle of the convergence angle motor 27 L . As the rotational angle detecting means 28 L , for example, an externally attached member such as a rotary encoder may be used, or a means such as a pulse motor for detecting the rotational angle by the driving system itself according to a driving method may be used. The right side imaging system 10 R has the same arrangement as that of the left side imaging system 10 L . Assume that when the focus motor 26 L and the zoom motor 25 L of the left side imaging optical system 11 L are independently controlled by signals from a focus encoder 42 L and a zoom encoder 41 L , and a focus motor 26 R and a zoom motor 25 R of a right side imaging optical system 11 R are independently controlled by signals from a focus encoder 42 R and a zoom encoder 41 R , a focal length f of the left side imaging optical system 11 L always coincides with a focal length f of the right side imaging optical system 11 R , and an image formation magnification β of the left side imaging optical system 11 L always coincides with an image formation magnification β of the right side imaging optical system 11 R . At this time, a keystone distortion correction signal generation portion 32 L shown at the left side in Fig. 5B can calculate the focal length f of the left side imaging optical system 11 L on the basis of a signal from the zoom encoder 41 L , and a keystone distortion correction signal generation portion 32 R shown at the right side in Fig. 5B can calculate the focal length f of the right side imaging optical system 11 R on the basis of a signal from the zoom encoder 41 R . Also, since the keystone distortion correction signal generation portion 32 L can calculate an object distance to the left side imaging optical system 11 L on the basis of a signal from the focus encoder 42 L ,it can calculate the image formation magnification β of the left side imaging optical system 11 L . Similarly, the keystone distortion correction signal generation portion 32 R can calculate the image formation magnification β of the right side imaging optical system 11 R on the basis of a signal from the focus encoder 42 R . Furthermore, the keystone distortion correction signal generation portions 32 R and 32 L can calculate inclination angles  on the basis of signals from the corresponding rotational angle detecting means 28 R and 28 L . As shown in Fig. 5B, the multi-lens imaging apparatus of this embodiment further includes the keystone distortion correction signal generation portion 32 L for generating a keystone distortion correction signal on the basis of the output signals from the rotational angle detecting means 28 L , the zoom encoder 41 L , and the focus encoder 42 L of the left side imaging optical system 11 L , and outputting the keystone distortion correction signal to the camera tube electron beam scanning locus control driver 31 L , the keystone distortion correction signal generation portion 32 R for generating a keystone distortion correction signal on the basis of the output signals from the rotational angle detecting means 28 R , the zoom encoder 41 R , and the focus encoder 42 R of the right side imaging optical system 11 R , and outputting the keystone distortion correction signal to a camera tube electron beam scanning locus control driver 31 R , and a synthesizing process portion 38 for forming a single high-fine image by synthesizing a right side image I R sent from a right side image sensor 12 R and a left side image I L sent from the left side image sensor 12 L . Note that the high-fine image formed by the synthesizing process portion 38 is output to a high fine monitor 40, and is displayed thereon. The principle of correcting keystone distortions in the keystone distortion correction signal generation portions 32 R and 32 L will be described below with reference to Figs. 6 to 8. When keystone distortions are respectively generated in the left side image I L obtained by the left side image sensor 12 L constituting the left side imaging system 10 L and in the right side image I R obtained by the right side image sensor 12 R constituting the right side imaging system 10 R , if a point A on the Y-axis of a required image I indicated by a broken line in Fig. 6 is defined as a reference point, a point A L on the left side image I L corresponding to the point A is deviated leftward in Fig. 6 by a horizontal deviation amount Δy, and a point A R on the left side image I R corresponding to the point A is deviated rightward in Fig. 6 by a horizontal deviation amount Δy. If an arbitrary point P 0 on the required image I indicated by a broken line in Fig. 7 is defined as a reference point, a point P 1 on the left side image I R corresponding to the point P 0 is deviated rightward in Fig. 7 by a horizontal deviation amount Δy 0 , and is deviated upward in Fig. 7 by a vertical deviation amount Δz 0 ' if the coordinates of the point P 0 are represented by (y 0 , , z 0 '), and the coordinates of the point P 1 are represented by (y 0 , +Δy 0 ', z 0 '+Δz 0 '). However, the horizontal and vertical deviation amounts Δy 0 , and Δz 0 ' can be calculated from the focal length f and the image formation magnification β of the right side imaging optical system 11 R and the inclination angle  of the right side imaging system 10 R . This principle will be described in more detail below with reference to Fig. 8. As shown in Fig. 8, when the right and left imaging systems 10 R and 10 L respectively perform imaging operations of an object surface 2, so that their optical axes L R and L L cross at a point O on the object surface 2, a conjugate object surface 3 passing through the point O on the object surface 2 and conjugate with the right side image sensor 12 R is assumed. A point P 0 on the object surface 2 and a point P 1 on the conjugate object surface 3, which satisfy OP 0 = OP 1 , will be examined below. In this case, an object height y 0 of the point P 0 with respect to the right side imaging optical system 11 R and an object height y 1 of the point P 1 with respect to the right side imaging optical system 11 R satisfy: y 1 = y 0 × cos() A length OQ 1 between an intersection Q 1 of a perpendicular drawn from the point P 1 to the optical axis L R , and point 0 is expressed by: OQ 1 = y 0 X sin() Furthermore, if image heights on the right side image sensor 12 R with respect to the object heights y 0 and y 1 are respectively represented by y 0 ' and y 1 ', the horizontal deviation amount Δy 0 ' is given by: Δy 0 ' = y 1 ' - y 0 ' If the distance (object distance) from the front-side principal point of the right side imaging optical system 11 R to the object surface 2 is represented by S 0 , and the distance from the rear-side principal point of the right side imaging optical system 11 R to the image surface of the right side image sensor 12 R is represented by S 0 ' the image height y 1 ' is expressed by: y 1 ' = y 1 × S 0 '/(S 0 - OQ 1 ) Thus, from equations (1), (2), and (4), the image height y 1 ' can be expressed by: y 1 ' = S 0 ' × y 0 × cos()/(S 0 - y 0 × sin()) Also, the image height y 0 ' is expressed by: y 0 ' = y 0 × S 0 '/S 0 For this reason, from equations (3), (5), and (6), the horizontal deviation amount Δy 0 ' can be expressed by: Δy 0 ' = {S 0 ' × cos()/(S 0 ' - y 0 ' × sin()) - 1} × y 0 ' Similarly, the vertical deviation amount Δz 0 ' can be expressed by: Δz 0 ' = z 1 ' - z 0 ' = {S 0 '/(S 0 ' - y 0 ' × sin()) - 1} × z 0 ' In this case, the distance S 0 ' from the rear-side principal point of the right side imaging optical system 11 R to the image surface of the right side image sensor 12 R is expressed as follows using the focal length f and the image formation magnification β of the right side imaging optical system 11 R : S 0 ' = f × (1 - β) Therefore, the horizontal and vertical deviation amounts Δy 0 ' and Δz 0 ' can be respectively calculated from the focal length f and the image formation magnification β of the right side imaging optical system 11 R and the inclination angle  of the right side imaging system 10 R . The same applies to the left side imaging system 10 L . The operation of the multi-lens imaging apparatus of this embodiment will be described below. When the object surface 2 is located at an infinity distance position, no keystone distortions are generated in the right and left side images I R and I L obtained by the right and left side image sensors 12 R and 12 L . For this reason, the synthesizing process portion 38 synthesizes the right and left side images I R and I L without executing the keystone distortion correction of the right and left side images I R and I L , and outputs the synthesized image to the high fine monitor 40. On the other hand, when the object surface 2 is located at a finite distance position, the right and left side imaging systems 10 R and 10 L are inclined in opposite directions by the convergence angle motors 27 R and 27 L , so that the right and left side imaging systems 10 R and 10 L are directed toward the object surface 2. Thereafter, the inclination angles  of the right and left side imaging systems 10 R and 10 L are controlled by the convergence angle motors 27 R and 27 L , so that the sampling points on the optical axis L L of the left side imaging system 10 L are shifted by a 1/2 spatial phase pitch from those on the optical axis L R of the right side imaging system 10 R . At this time, in synchronism with control of the inclination angles  by the convergence angle motors 27 R and 27 L , the magnification setting operations and focusing operations of the right and left side imaging optical systems 11 R and 11 L are performed using the zoom motors 25 R and 25 L and the focus motors 26 R and 26 L . In this case, since the imaging operations are performed in a state wherein the right and left imaging systems 10 R and 10 L are inclined through the inclination angle , keystone distortions are generated in the right and left side images I R and I L obtained by the right and left side image sensors 12 R and 12 L . Therefore, in order to correct these keystone distortions, the keystone distortion correction signal generation portion 32 L of the left side imaging optical system 11 L calculates the horizontal and vertical deviation amounts Δy 0 ' and Δz 0 ' of each point on the left side image I L obtained by the left side image sensor 12 L using the output signals from the rotational angle detecting means 28 L and the focus encoder 42 L and the zoom encoder 41 L from equations (7) to (9) described above, generates a keystone distortion correction signal for correcting the keystone distortion generated in the left side image I L , and outputs the signal to the camera tube electron beam scanning locus control driver 31 L of the left side imaging optical system 11 L . In this case, the distance S 0 ' is calculated from equation (9). Alternatively, the distance S 0 ' may be calculated from the output signal from the focus encoder 42 L . The keystone distortion correction signal generation portion 32 R of the right side imaging optical system 11 R operates in the same manner as described above. The camera tube electron beam scanning locus control driver 31 L of the left side imaging optical system 11 L changes the scanning locus of the electron beam emitted from the camera tube constituting the left side image sensor 12 L on the basis of the keystone distortion correction signal sent from the keystone distortion correction signal generation portion 32 L , thereby correcting the keystone distortion generated in the left side image I L . More specifically, the camera tube electron beam scanning locus control driver 31 L of the left side imaging optical system 11 L changes the scanning locus of the electron beam by controlling a deflection circuit of the camera tube constituting the left side image sensor 12 L on the basis of the keystone distortion correction signal sent from the keystone distortion correction signal generation portion 32 L , thereby scanning the left side image I L along a point A 1 → a point B 1 , a point A 2 → a point B 2 , a point A 3 →a point B 3 , and a point A 4 → a point B 4 , as indicated by the left-hand side figure in Fig. 9. As a result, the left side image I L output from the camera tube constituting the left side image sensor 12 L is converted into the required image I, which is scanned along a point a 1 → a point b 1 , a point a 2 → a point b 2 , a point a 3 → a point b 3 , and a point a 4 → a point b 4 , as indicated by the right-hand side figure in Fig. 9, and the converted image is input to the synthesizing process portion 38. In place of the rotational angle detecting means 28 R and 28 L , means for detecting relative postures of the right and left imaging systems 10 R and 10 L to obtain the inclination angles  may be used. The right and left imaging optical systems 11 R and 11 L may be constituted using zoom lenses or fixed focal point lenses. Fig. 10 is a perspective view showing the arrangement of the right and left side imaging systems 10 R and 10 L in a multi-lens imaging apparatus according to another embodiment of the present invention, and Fig. 11 is a block diagram for explaining operations of correction conversion portions 52 R and 52 L . The multi-lens imaging apparatus of this embodiment has the following differences from the multi-lens imaging apparatus of the embodiment shown in Figs. 5A and 5B. (1) Both the right and left side image sensors 12 R and 12 L comprise solid-state imaging device in place of the camera tubes. (2) The apparatus of this embodiment does not have the camera tube electron scanning locus control drivers 31 R and 31 L of the right and left imaging systems 10 R and 10 L shown in Fig. 5A. (3) The apparatus of this embodiment has a left side image memory 51 L for left side image data output from the left side image sensor 12 L , and a right side image memory 51 R for right side image data output from the right side image sensor 12 R , as shown in Fig. 11. (4) The apparatus of this embodiment has a correction conversion portion 52 L (to be described later) between the left side image memory 51 L and the synthesizing processing portion 38, and also has a correction conversion portion 52 R (to be described later) between the right side image memory 51 R and the synthesizing processing portion 38. The operation of the multi-lens imaging apparatus of this embodiment will be described below. When the object surface 2 is located at an infinity distance position, since no keystone distortions are generated in the right and left side images I R and I L obtained by the right and left side image sensors 12 R and 12 L , right and left side image data respectively stored in the right and left image memories 51 R and 51 L are directly supplied to the synthesizing process portion 38 without executing keystone distortion correction of the right and left side images I R and I L , and the right and left side images I R and I L are synthesized by the synthesizing process portion 38. The synthesized image is then output to the high fine monitor 40. On the other hand, when the object surface 2 is located at a finite distance position, the right and left side imaging systems 10 R and 10 L are inclined by the convergence angle motors 27 R and 27 L in opposite directions, so that the right and left side imaging systems 10 R and 10 L are directed toward the object surface 2. Thereafter, the inclination angles  of the right and left side imaging systems 10 R and 10 L are controlled by the convergence angle motors 27 R and 27 L , so that the sampling points on the optical axis L L of the left side imaging system 10 L are shifted by a 1/2 spatial phase pitch from those on the optical axis L R of the right side imaging system 10 R . At this time, in synchronism with control of the inclination angles  by the convergence angle motors 27 R and 27 L , the magnification setting operations and focusing operations of the right and left side imaging optical systems 11 R and 11 L are performed using the zoom motors 25 R and 25 L and the focus motors 26 R and 26 L . In this case, since the imaging operations are performed in a state wherein the right and left imaging systems 10 R and 10 L are inclined through the inclination angle , keystone distortions are generated in the right and left side images I R and I L obtained by the right and left side image sensors 12 R and 12 L . Therefore, in order to correct these keystone distortions, as shown in Fig. 11, the keystone distortion correction signal generation portion 32 L of the left side imaging optical system 11 L calculates the horizontal and vertical deviation amounts Δy 0 ' and Δz 0 ' of each point on the left side image I L obtained by the left side image sensor 12 L using the output signals from the rotational angle detecting means 28 L and the focus encoder 42 L and the zoom encoder 41 L from equations (7) to (9) described above, generates a keystone distortion correction signal for correcting the keystone distortion generated in the left side image I L , and outputs the signal to the correction conversion portion 52 L . The correction conversion portion 52 L converts the coordinate of the left side image data of the left side image I L read out from the left side image memory 51 L so as to cancel the horizontal and vertical deviation amounts Δy 0 ' and Δz 0 ' on the basis of the keystone distortion correction signal sent from the keystone distortion correction signal generation portion 32 L , thereby correcting the keystone distortion generated in the left side image I L . In this case, the distance S 0 ' is calculated from equation (9). Alternatively, the distance S 0 ' may be calculated from the output signal from the focus encoder 42 L . The keystone distortion correction signal generation portion 32 R and the correction conversion portion 52 R of the right side imaging optical system 11 R perform the same operation as described above. As a result, the synthesizing process portion 38 synthesizes the right and left side image data of the right and left side images I R and I L , which are respectively sent from the correction conversion portions 52 R and 52 L , and in which the keystone distortions are corrected, so that a single high-fine synthesized image can be displayed on the high fine monitor 40. In the multi-lens imaging apparatus of this embodiment, the output signal from the correction conversion portion 52 L is supplied to the synthesizing process portion 38. Alternatively, the output signal from the correction conversion portion 52 L may be stored again in the left side image memory 51 L , and thereafter, the data may be supplied from the left side image memory 51 L to the synthesizing process portion 38. The same applies to the output signal from the other correction conversion portion 52 R . Fig. 12 is a perspective view showing an arrangement of the right and left imaging systems 10 R and 10 L in a multi-lens imaging apparatus according to still another embodiment of the present invention, and Fig. 13 is a block diagram for explaining operations of correction optical systems 61 R and 61 L . In the multi-lens imaging apparatus of this embodiment, lenses constituting correction optical systems 61 R and 61 L (to be described later) are decentered in the vertical direction with respect to the optical axes L R and L L so as to generate distortions, thereby correcting keystone distortions generated in the right and left side images I R and I L obtained by the right and left side image sensors 12 R and 12 L . More specifically, the arrangement of the multi-lens imaging apparatus is substantially the same as that of the multi-lens imaging apparatus of the embodiment shown in Figs. 10 and 11, except that the apparatus of this embodiment has the correction optical system 61 L arranged between the left side imaging optical system 11 L and the left side image sensor 12 L , and the correction optical system 61 R arranged between the right side imaging optical system 11 R and the right side image sensor 12 R , in place of the correction conversion portions 52 L and 52 R . The operation of the multi-lens imaging apparatus of this embodiment will be described below. When the object surface 2 is located at an infinity distance position, since no keystone distortions are generated in the right and left side images I R and I L obtained by the right and left side image sensors 12 R and 12 L , the right and left side images I R and I L are synthesized by the synthesizing process portion 38 without executing keystone distortion correction of the right and left side images I R and I L , and the synthesized image is output to the high fine monitor 40. On the other hand, when the object surface 2 is located at a finite distance position, the right and left side imaging systems 10 R and 10 L are inclined by the convergence angle motors 27 R and 27 L in opposite directions, so that the right and left side imaging systems 10 R and 10 L are directed toward the object surface 2. Thereafter, the inclination angles  of the right and left side imaging systems 10 R and 10 L are controlled by the convergence angle motors 27 R and 27 L , so that the sampling points on the optical axis L L of the left side imaging system 10 L are shifted by a 1/2 spatial phase pitch from those on the optical axis L R of the right side imaging system 10 R . At this time, in synchronism with control of the inclination angles  by the convergence angle motors 27 R and 27 L , the magnification setting operations and focusing operations of the right and left side imaging optical systems 11 R and 11 L are performed using the zoom motors 25 R and 25 L and the focus motors 26 R and 26 L . In this case, since the imaging operations are performed in a state wherein the right and left imaging systems 10 R and 10 L are inclined through the inclination angle , keystone distortions are generated in the right and left side images I R and I L obtained by the right and left side image sensors 12 R and 12 L . Therefore, in order to correct these keystone distortions, as shown in Fig. 13, the keystone distortion correction signal generation portion 32 L of the left side imaging optical system 11 L calculates the horizontal and vertical deviation amounts Δy 0 , and Δz 0 , of each point on the left side image I L obtained by the left side image sensor 12 L using the output signals from the rotational angle detecting means 28 L and the focus encoder 42 l and the zoom encoder 41 L from equations (7) to (9) described above, generates a keystone distortion correction signal for correcting the keystone distortion generated in the left side image I L , and outputs the signal to the correction optical system 61 L of the left side imaging optical system 11 L . The correction optical system 61 L of the left side imaging optical system 11 L decenters at least one of lenses constituting the correction optical system 61 L in the vertical direction with respect to the optical axis L L on the basis of the keystone distortion correction signal sent from the keystone distortion correction signal generation portion 32 L so as to generate a distortion, thereby correcting the keystone distortion generated in the left side image I L . In this case, the distance S 0 ' is calculated from equation (9). Alternatively, the distance S 0 ' may be calculated from the output signal from the focus encoder 42 L . The keystone distortion correction signal generation portion 32 R and the correction optical system 61 R of the right side imaging optical system 11 R perform the same operations as described above. The principle of correcting keystone distortions will be described below with reference to Fig. 14. The object surface 2 is inclined through the inclination angle  with respect to the optical axis L R , and its image is formed on the right side image sensor 12 R . If the distance from the object surface 2 to the right side imaging optical system 11 R is represented by S 1 , the distance from the right side imaging optical system 11 R to the image surface of the right side image sensor 12 R is represented by S 1 ', and a point O on the object surface 2 is defined as an intersection between the optical axis L R and the object surface 2, an image formation magnification β H at a height H of the object surface 2 is expressed as follows by a paraxial calculation: β H = S 1 '/(S 1 + H × sin()) = β × {S 1 /(S 1 + H × sin())} where β = the image formation magnification at the point O on the object surface 2 A decentering distortion d generated when a concave lens 62 R of the correction optical system 61 R (consisting of the concave lens 62 R and a convex lens 63 R ) arranged between the right side imaging optical system 11 R and the right side image sensor 12 R is parallelly decentered by a distance E in the vertical direction in Fig. 15 is given, in consideration of up to a third-order term, by: d = -(E/2) × (tan(ω)) 2 × (3 × V E1 - V E2 ) for tan(ω) = H/f (f = the focal length of the right side imaging optical system 11R) Note that V E1 and V E2 included in equation (11) are parallel decentering distortion coefficients of the correction optical system 61 R , and are respectively given by: V E1 = (h ×  × V q - a × V p ) - (h ×  × B q - a × B p ) V E2 = h ×  × P q - a × P p where  = the refracting power of the correction optical system 61 R V p = the third-order distortion of the convex lens 63 R B p = the astigmatism coefficient of the convex lens 63 R P p = the Petzval's sum of the convex lens 63 R V q = the third-order distortion on the object surface 2 side of the concave lens 62 R B q = the astigmatism coefficient on the object surface 2 side of the concave lens 62 R P q = the Petzval's sum on the object surface 2 side of the concave lens 62 R h = the incident position of the paraxial object ray onto the correction optical system 61 R a = the incident angle of the paraxial object ray onto the correction optical system 61 R Since the distortion generated when the correction optical system 61 R is decentered is calculated in the above-mentioned procedures, keystone distortion correction shown in Fig. 16 can be attained by decentering the correction optical system 61 R so that the signs of β H /β - 1 and the decentering distortion d are opposite to each other: d = -β H /β - 1 In this manner, a keystone distortion can be corrected in a region up to the third order. Note that the parallel decentering amount E of the correction optical system 61 R can be calculated from equations (10) to (14). When the right side image I R in which the keystone distortion is corrected in this manner, and which is obtained from the right side image sensor 12 R , and the left side image I L in which the keystone distortion is similarly corrected, and which is obtained from the left side image sensor 12 L are synthesized by the synthesizing process portion 38, a single high-fine image can be displayed on the high fine monitor 40 (see Fig. 13). Figs. 17A and 17B show a multi-lens imaging apparatus according to still another embodiment of the present invention. The multi-lens imaging apparatus of this embodiment obtains a single high-fine image by synthesizing two images obtained by picking up an image of a common object using two imaging systems (right and left side imaging systems 10 R and 10 L ). The arrangement of the right and left side imaging systems 10 R and 10 L will be described in detail below with reference to Fig. 17A. The left side imaging system 10 L includes lens groups 21 L to 24 L including a zoom lens group 22 L and a focus lens group 24 L , a zoom motor 25 L as a driving system for driving the zoom lens group 22 L , a focus motor 26 L as a driving system for driving the focus lens group 24 L , a mechanism system (not shown) and a driving system (convergence angle motor 27 L ) for integrally rotating the left side imaging optical system 11 L and a left side image sensor 12 L in a plane including an optical axis L L , and a rotational angle detecting means 28 L for detecting the rotational angle of the convergence angle motor 27 L , which constitute a left side imaging optical system 11 L . As the rotational angle detecting means 28 L , for example, an externally attached member such as a rotary encoder may be used, or a means such as a pulse motor for detecting the rotational angle by the driving system itself according to a driving method may be used. The right side imaging system 10 R has the same arrangement as that of the left side imaging system 10 L . Assume that when the focus motor 26 L and the zoom motor 25 L of the left side imaging optical system 11 L are independently controlled by signals from the focus encoder 42 L and the zoom encoder 41 L , and a focus motor 26 R and a zoom motor 25 R of a right side imaging optical system 11 R are independently controlled by signals from a focus encoder 42 R and a zoom encoder 41 R , a focal length f of the left side imaging optical system 11 L always coincides with a focal length f of the right side imaging optical system 11 R , and an image formation magnification β of the left side imaging optical system 11 L always coincides with an image formation magnification β of the right side imaging optical system 11 R . At this time, a calculation control portion 71 shown in Fig. 17B can calculate the focal length f of the left side imaging optical system 11 L on the basis of a signal from the zoom encoder 41 L , and can calculate the focal length f of the right side imaging optical system 11 R on the basis of a signal from the zoom encoder 41 R . Also, since the calculation control portion 71 can calculate an object distance to the left side imaging optical system 11 L on the basis of a signal from the focus encoder 42 L , it can calculate the image formation magnification β of the left side imaging optical system 11 L , and similarly, it can calculate the image formation magnification β of the right side imaging optical system 11 R on the basis of a signal from the focus encoder 42 R . Furthermore, the calculation control portion 71 can calculate inclination angles  from the signals output from the rotational angle detecting means 28 R and 28 L . The output signals from the zoom encoders 41 R and 41 L and the focus encoders 42 R and 42 L are input to the calculation control portion 71, as shown in Fig. 17B. The calculation control portion 71 can calculate the distance S 0 ' from the rear-side principal point of the left side imaging optical system 11 L to the image surface of the left side image sensor 12 L and the distance S 0 ' from the rear-side principal point of the right side imaging optical system 11 R to the image surface of the right side image sensor 12 R from equation (9) described above: S 0 ' = f × (1 - β) Left side image data of a left side image I L output from the left side image sensor 12 L is stored in a left side image memory 72 L , and right side image data of a right side image I R output from the right side image sensor 12 R is stored in a right side image memory 72 R . The principle of correcting keystone distortions generated in the right and left images I R and I L by a keystone distortion conversion portion 73, second right and left side image memories 74 R and 74 L , and a subtraction process circuit 75 shown in Fig. 17B will be described below with reference to Figs. 18 and 19. The keystone distortion conversion portion 73 calculates horizontal and vertical deviation amounts Δy 0 ' and Δz 0 ' of predetermined several image points from equations (7) and (8) described above using the left side image data read out from the left side image memory 72 L , the right side image data read out from the right side image memory 72 R , and the distances S 0 ' sent from the calculation control portion 71. At this time, the inclination angle  is defined as a conversion variable (an angle is not detected), and the horizontal and vertical deviation amounts Δy 0 ' and Δz 0 ' are calculated by substituting, e.g.,  =  1 ( 1 is an arbitrary value). Thereafter, the keystone distortion conversion portion 73 shifts the coordinates of the image points in the right and left side image memories 72 R and 72 L by the calculated horizontal and vertical deviation amounts Δy 0 ' and Δz 0 ', and writes the shifted right and left side image data in the second right and left side image memories 74 R and 74 L , respectively. Thereafter, the subtraction process circuit 75 reads out the coordinate-shifted right and left side image data respectively from the second right and left side image memories 74 R and 74 L , and calculates a sum (to be referred to as an "image difference" hereinafter) δ S1 of the absolute values of differences of these data. Subsequently, the keystone distortion conversion portion 73 changes the inclination angle  (conversion variable) to be  =  2 , and an image difference δ s2 is similarly calculated. When the above-mentioned operations are repeated, since the relationship between the inclination angle  (conversion variable) and the image difference δ s can be obtained, as shown in, e.g., Fig. 19, an inclination angle  0 (conversion variable) at which the image difference δ s assumes a minimum value is obtained. The keystone distortion conversion portion 73 calculates the horizontal and vertical deviation amounts Δy 0 , and Δz 0 , of all image points of the left side image data from equations (7) and (8) using the inclination angle  0 (conversion variable) at which the image difference δ s assumes a minimum value, thereafter, shifts the coordinates of all the image points of the left side image data by the calculated horizontal and vertical deviation amounts Δy 0 , and Δz 0 , , and writes the shifted left side image data in the second left side image memory 74 L . As a result, the left side image data in which the keystone distortion is corrected is written in the second left side image memory 74 L . Therefore, when the left side image data in which the keystone distortion is corrected, and which is written in the second left side image memory 74 L , and the right side image data in which the keystone distortion is corrected, and which is written in the second right side image memory 74 R are synthesized by a synthesizing process portion (not shown), a single high-fine image can be displayed on a high fine monitor (not shown). Figs. 20A and 20B show a multi-lens imaging apparatus according to still another embodiment of the present invention. The arrangement of the multi-lens imaging apparatus of this embodiment is substantially the same as that of the multi-lens imaging apparatus of the embodiment shown in Figs. 17A and 17B, except that the right and left image sensors 12 R and 12 L comprise camera tubes, and the keystone distortion conversion portion 73 controls camera tube electron beam scanning locus drivers 31 R and 31 L according to the calculated horizontal and vertical deviation amounts Δy 0 ' and Δz 0 '. Since the operations of the camera tube electron beam scanning locus drivers 31 R and 31 L and the principle of correcting keystone distortions in the multi-lens imaging apparatus of this embodiment are the same as those in the multi-lens imaging apparatuses in the embodiments shown in Figs. 5A and 5B and Figs. 17A and 17B, a repetitive description will be avoided here. Figs. 21A to 21C show a multi-lens imaging apparatus according to still another embodiment of the present invention, and Fig. 22 shows a basic arrangement of imaging systems in the multi-lens imaging apparatus of the embodiment shown in Figs. 21A to 21C. The multi-lens imaging apparatus of this embodiment obtains a single high-fine image by synthesizing two images obtained by picking up an image of a common object using two sets of imaging systems (right and left side imaging systems 10 R and 10 L ) . As shown in Fig. 22, the left side imaging system 10 L is constituted by a left side imaging optical system 11 L and a left side image sensor 12 L , and the right side imaging system 10 R is constituted by a right side imaging optical system 11 R and a right side image sensor 12 R . The right and left side imaging optical systems 11 R and 11 L have equivalent specifications, and each comprises a zoom lens. The right and left side image sensors 12 R and 12 L have equivalent specifications, and each comprises a camera tube such as a saticon or a solid-state imaging element such as a CCD. Optical axes L R and L L of the right and left imaging systems 10 R and 10 L cross almost at a point O on an object surface 2, and these systems are arranged at positions axially symmetrical about a normal O-O' to the object surface 2. In this multi-lens imaging apparatus, when the object distance is changed, the convergence angle 2 is changed by rotating each of the right and left side imaging systems 10 R and 10 L about an X mark shown in Fig. 22 in accordance with the change in object distance, thus performing an imaging operation. The arrangement of the right and left imaging systems 10 R and 10 L will be described in detail below with reference to Fig. 21A. The left side imaging system 10 L includes lens groups 21 L to 24 L including a zoom lens group 22 L and a focus lens group 24 L , a zoom motor 25 L as a driving system for driving the zoom lens group 22 L , a focus motor 26 L as a driving system for driving the focus lens group 24 L , a mechanism system (not shown) and a driving system (convergence angle motor 27 L ) for integrally rotating the left side imaging optical system 11 L and a left side image sensor 12 L in a plane including an optical axis L L , and a rotational angle detecting means 28 L for detecting the rotational angle of the convergence angle motor 27 L , which constitute a left side imaging optical system 11 L . As the rotational angle detecting means 28 L , for example, an externally attached member such as a rotary encoder may be used, or a means such as a pulse motor for detecting the rotational angle by the driving system itself according to a driving method may be used. The right side imaging system 10 R has the same arrangement as that of the left side imaging system 10 L . A control method for the convergence angle motors 27 R and 27 L will be described below with reference to Fig. 21B. When the right and left imaging systems 10 R and 10 L perform imaging operations respectively at convergence angles 2+Δ R and 2+Δ L to have angular deviations Δ R and Δ L with respect to the predetermined convergence angle 2 (see Fig. 22), the rotational angle detecting means 28 L detects the angular deviation Δ L with respect to an angle  (see Fig. 22) formed between the optical axis L L of the left side imaging system 10 L and the normal O-O' to the object surface 2, and the rotational angle detecting means 28 R detects the angular deviation Δ R with respect to an angle  formed between the optical axis R R of the right side imaging system 10 R and the normal O-O' to the object surface 2. The angular deviations Δ R and Δ L output from the rotational angle detecting means 28 R and 28 L are supplied to a control portion 231. Assume that the convergence angle motors 27 R and 27 L have the following response characteristics. For the sake of simplicity, as shown in Fig. 23, only a mis-registration amount Δa of a image output from the right side imaging system 10 R when the optical axis L R of the right side imaging system 10 R is deviated by the angular deviation Δ R will be examined below. If the distance (object distance) from the front-side principal point of the right side imaging optical system 11 R to the object surface 2 is represented by S 0 , the distance from the rear-side principal point of the right side imaging optical system 11 R to the right side image sensor 12 R is represented by S 1 , and the deviation amount of the optical axis L R of the right side imaging system 10 R in the object surface 2 is represented by Δy, when the angular deviation Δ R is small, we have: S 0 × tan(Δ R ) = Δy × cos() If the image formation magnification of the right side imaging optical system 11 R is represented by β, we have: β = Δa/Δy Furthermore, if the focal length of the right side imaging optical system 11 R is represented by f, we have: S 0 = f × (β - 1)/β From equations (15) to (17), the mis-registration amount Δa of the image is given by: Δa = {f × (β - 1) × tan(Δ R )}/cos() Therefore, assume that the convergence angle motor 27 R shown in Fig. 21A has sufficient response characteristics for an angle (Δ R ) necessary for correcting the mis-registration amount Δa of the image given by equation (18) to be equal to or smaller than an allowable value Δa 0 . The same applies to the convergence angle motor 27 L of the left side imaging optical system 11 L. The control portion 231 supplies a correction signal -Δ L to the convergence angle motor 27 L of the left side imaging system 10 L as a control target value, and supplies a correction signal -Δ R to the convergence angle motor 27 R of the right side imaging system 10 R as a control target value, as shown in Fig. 21B. As a result, the mis-registration amount Δa of the image obtained by each of the right and left imaging systems 10 R and 10 L can be corrected to be equal to or smaller than the allowable value Δa 0 . When the mis-registration amounts of the images are corrected as described above, a image signal output from the left side image sensor 12 L is stored in a left side image memory 232 L , and a image signal output from the right side image sensor 12 R is stored in a right side image memory 232 R , as shown in Fig. 21C. Thereafter, these images are synthesized by a synthesizing process circuit 233, and a synthesized image signal is output. Therefore, since the multi-lens imaging apparatus of this embodiment can synthesize images obtained by the right and left imaging systems 10 R and 10 L while registering the two images, if, for example, the convergence angle is controlled in advance so that the relative spatial phase between the right and left side image sensors 12 R and 12 L is shifted by a 1/2 pitch when the sampling points of the right and left image side sensors 12 R and 12 L are imaginarily projected onto an object, the synthesizing process circuit 233 can obtain a single high fine image. In the multi-lens imaging apparatus of this embodiment, when a solid state imaging element is used as each of the right and left side image sensors 12 R and 12 L , either a single-sensor type element or two- or three-sensor type element via a color separation system may be used. When a camera tube is used as each of the right and left side image sensors 12 R and 12 L , either a single-tube type element or two- or three-tube type element via a color separation system may be used. The control portion 231 may supply a correction signal -(Δ L +Δ R ) to one of the two convergence angle motors 27 R and 27 L as a control target value in place of respectively supplying the correction signals -Δ R and -Δ L to the two convergence angle motors 27 R and 27 L as control target values. Figs. 24A and 24B show a multi-lens imaging apparatus according to still another embodiment of the present invention. In the multi-lens imaging apparatus of the embodiment shown in Figs. 21A to 21C, as can be understood from equation (18), when the focal lengths f of the right and left side imaging optical systems 11 R and 11 L are large, or when the allowable values Δa 0 of the mis-registration amounts of images are small, the correction signals -Δ R and -Δ L output from the control portion 231 also take small values (e.g., on the order of several seconds), and it becomes difficult to obtain angular response performance necessary for correction under the influence of, e.g., non-sensitive bands of the convergence angle motors 27 R and 27 L . In the multi-lens imaging apparatus of the embodiment shown in Figs. 24A and 24B, the image mis-registration amount Δa given by equation (18) is calculated, and is corrected by means other than the convergence angle motors 27 R and 27 L , thereby solving the above-mentioned problem. The apparatus of this embodiment has the following differences from the multi-lens imaging apparatus of the embodiment shown in Figs. 21A to 21C. (1) Zoom encoders 41 R and 41 L for detecting the focal lengths f of the right and left side imaging optical systems 11 R and 11 L are respectively provided to the zoom motors 25 R and 25 L . (2) Focus encoders 42 R and 42 L for detecting the object distances S 0 with respect to the right and left side imaging optical systems 11 R and 11 L are respectively provided to the focus motors 26 R and 26 L . (3) The apparatus of this embodiment includes horizontal direction drive systems 243 R and 243 L for respectively driving the right and left side image sensors 12 R and 12 L in the horizontal direction. (4) The apparatus of this embodiment also includes a calculation control portion 244 (to be described later; see Fig. 24B). The operation of the multi-lens imaging apparatus of this embodiment will be described below. In the left side imaging optical system 11 L , when the zoom motor 25 L is controlled by a signal from the zoom encoder 41 L , and the focus motor 26 L is controlled by an output signal from the focus encoder 42 L , the focal length f and the image formation magnification β are caused to always coincide with each other. In the right side imaging optical system 11 R , the focal length f and the image formation magnification β are similarly caused to always coincide with each other. Therefore, the focal lengths f and the image formation magnifications β of the right and left side imaging optical systems 11 R and 11 L can be obtained from the output signals from the zoom encoders 41 R and 41 L , and the object distances S 0 with respect to the right and left side imaging optical systems 11 R and 11 L can be obtained from the output signals from the focus encoders 42 R and 42 L . For this reason, the output signals from the zoom encoders 41 R and 41 L and the focus encoders 42 R and 42 L are input to the calculation control portion 244, and the calculation control portion 244 calculates equation (18) described above, thus obtaining the mis-registration amounts Δa 0 of images. The calculation control portion 244 controls the horizontal direction drive systems 243 R and 243 L to move the right and left side image sensors 12 R and 12 L in the horizontal direction according to the calculated mis-registration amounts Δa 0 of the images, thereby correcting the mis-registration amounts Δa of the images to be equal to or smaller than the allowable value Δa 0 . As each of the zoom encoders 41 R and 41 L and the focus encoders 42 R and 42 L , for example, an externally attached member such as a potentiometer may be used, or a means such as a pulse motor for detecting the rotational angle by the driving system itself according to a driving method may be used. Also, each of the horizontal direction drive systems 243 R and 243 L may comprise, e.g., a piezo element or piezoelectric bimorph. When a swing motion in the vertical direction occurs due to insufficient precision of a mechanism system (not shown) for driving the convergence angle motor, encoders for respectively detecting inclination angles (elevation angles) Δ 1 , in the vertical direction, of the right and left side imaging systems 10 R and 10 L , and vertical direction drive systems for respectively moving the right and left side image sensors 12 R and 12 L in the vertical direction may be separately arranged. Thus, when the right and left side image sensors 12 R and 12 L are moved in the vertical direction according to the detected inclination angles Δ 1 in the vertical direction, mis-registration amounts Δb, in the vertical direction, of images obtained by the right and left imaging systems 10 R and 10 L can be similarly corrected to be equal to or smaller than an allowable value Δb 0 . At this time, the mis-registration amount Δb, in the vertical direction, of each image can be calculated by the following equation like in equation (18): Δb = f × (β - 1) × tan(Δ 1 ) For the following reasons, the mis-registration amounts Δb, in the vertical direction, of images may be corrected upon combination of coarse adjustment attained by the convergence angle motors 27 R and 27 L in the multi-lens imaging apparatus of the embodiment shown in Figs. 21A to 21C, and fine adjustment attained by the horizontal direction drive systems 243 R and 243 L in the multi-lens imaging apparatus of this embodiment: (1) to prevent regions to be subjected to aberration correction of the right and left side imaging optical systems 11 R and 11 L from being increased very much; and (2) to prevent the loads on the horizontal direction drive systems 243 R and 243 L from being increased. Figs. 25A and 25B show a multi-lens imaging apparatus according to still another embodiment of the present invention. In the multi-lens imaging apparatus of this embodiment, the right and left side image sensors 12 R and 12 L respectively comprise camera tubes, and the arrangement of the apparatus of this embodiment is substantially the same as that of the multi-lens imaging apparatus of the embodiment shown in Figs. 24A and 24B, except that camera tube electron beam scanning locus control drivers 251 R and 251 L are used in place of the horizontal direction drive systems 243 R and 243 L . More specifically, in the multi-lens imaging apparatus of this embodiment, since the camera tubes read video signals by scanning electron beams, the scanning loci of the electron beams by the camera tubes are controlled by the camera tube electron beam scanning locus control drivers 251 R and 251 L in accordance with the mis-registration amounts Δa obtained by equation (18) above, thereby registering the images expressed by the video signals output from the right and left side image sensors 12 R and 12 L . Figs. 26A and 26B show a multi-lens imaging apparatus according to still another embodiment of the present invention. In the multi-lens imaging apparatus of this embodiment, the right and left side image sensors 12 R and 12 L respectively comprise solid-state imaging device, and the mis-registration amounts Δa of images obtained by the right and left imaging systems 10 R and 10 L are corrected to be equal to or smaller than the allowable value Δa 0 without using the horizontal direction drive systems 243 R and 243 L shown in Fig. 24B. The apparatus of this embodiment has the following differences from the multi-lens imaging apparatus of the embodiment shown in Figs. 24A and 24B. (1) The apparatus of this embodiment does not include the horizontal direction drive systems 243 R and 243 L . (2) The apparatus of this embodiment includes a correction conversion portion 261 and a second left side image memory 262 between the left side image memory 232 L and the synthesizing process circuit 233 (see Fig. 26B). The operation of the multi-lens imaging apparatus of this embodiment will be described below. The calculation control portion 244 receives the output signals from the rotational angle detecting means 28 R and 28 L , the zoom encoders 41 R and 41 L , and the focus encoders 42 R and 42 L , and calculates the mis-registration amounts Δa and Δb of images using equations (18) and (19). The correction conversion portion 261 converts the coordinates of image data output from the left side image memory 232 L in accordance with the mis-registration amount Δa calculated by the calculation control portion 244, and writes the converted image data in the second left side image memory 262. As a result, when the synthesizing process circuit 233 synthesizes the image data respectively output from the second left side image memory 262 and the right side image memory 232 R , a high-fine synthesized image signal can be obtained. Note that the correction conversion portion 261 and a second left side image memory may be arranged between the right side image memory 232R and the synthesizing process circuit 233 in place of the correction conversion portion 261 and the second left side image memory 262. The left side image memory 232 L and the second left side image memory 262 may be replaced with a common one. Furthermore, when the coordinates of image data output from the left side image memory 232 L are converted, an interpolation calculation process of image data may be performed as needed. In each of the multi-lens imaging apparatus of the embodiments shown in Figs. 21A to 26B according to the present invention, the mis-registration amounts Δa of images are calculated based on the output signals from the rotational angle detecting means 28 R and 28 L , the zoom encoders 41 R and 41 L , and the focus encoders 42 R and 42 L . Alternatively, the mis-registration amounts Δa of images may be calculated from image signals output from the right and left imaging systems 10 R and 10 L . Such embodiments of multi-lens imaging apparatuses of the present invention will be described hereinafter. Fig. 27 is a block diagram for explaining an operation of a correlation calculation process portion in a multi-lens imaging apparatus according to still another embodiment of the present invention. The multi-lens imaging apparatus of this embodiment has the following differences from the multi-lens imaging apparatus of the embodiment shown in Figs. 26A and 26B. (1) The apparatus of this embodiment includes a correlation calculation process portion 271 for performing a correlation calculation between image data output from the second left side image memory 262 and image data output from the right side image memory 232 R to obtain a correlation value δ s . When the correlation value δ s is equal to or larger than a predetermined value, the portion 271 calculates a new shift amount X so that the correlation value δ s becomes equal to or smaller than the predetermined value, and outputs the calculated shift amount X to the correction conversion portion 261. (2) When the correction conversion portion 261 writes image data output from the left side image memory 232 L in the second left side image memory 262, it shifts the coordinates of the image data in the horizontal and vertical directions by the shift amount X sent from the correlation calculation process portion 271. The operation of the multi-lens imaging apparatus of this embodiment will be described below. The correction conversion portion 261 shifts the coordinates of image data output from the left side image memory 232 L in the horizontal and vertical directions by a predetermined shift amount X (e.g., by one pixel each in the horizontal and vertical directions), and writes the coordinate-shifted image data in the second left side image memory 262. The correlation calculation process portion 271 performs a correlation calculation between image data output from the second left side image memory 262 and image data output from the right side image memory 232 R to obtain a correlation value δ s . When the correlation value δ s is equal to or larger than a predetermined value, the portion 271 calculates a new shift amount X so that the correlation value δ s becomes equal to or smaller than the predetermined value, and outputs the calculated shift amount X to the correction conversion portion 261. The correction conversion portion 261 shifts the coordinates of image data output from the left side image memory 232 L in the horizontal and vertical directions by the new shift amount X, and writes the coordinate-shifted image data in the second left side image memory 262. Thereafter, the above-mentioned operations are repeated until the correlation value δ s becomes equal to or smaller than the predetermined value. After the correlation value δ s becomes equal to or smaller than the predetermined value, a synthesizing process circuit (not shown) synthesizes image data respectively output from the second left side image memory 262 and the right side image memory 232 R , thus obtaining a high-fine synthesized image signal. In order to shorten the correlation calculation time in the correlation calculation process portion 271, for example, the correlation calculation may be performed using only image data at the central portion of a frame. As a correlation calculation method, a known matching method, gradient method, or the like may be used. Since a finally obtained shift amount X 0 indicates the mis-registration amount Δa of a image, the correlation calculation process portion 271 may calculate a correction signal corresponding to the finally obtained shift amount X 0 , and the correction control methods described in the embodiments shown in Figs. 21A to 25B, i.e., the following control methods may be executed: (1) convergence angle control (2) correction drive control using drive systems capable of shifting the image sensors in the horizontal and vertical directions (3) correction control for changing the electron beam scanning loci The above-mentioned multi-lens imaging apparatus of the embodiment shown in Fig. 27 executes correction control of the mis-registration amounts Δa of images caused by convergence angle errors using the image signals output from the right and left side imaging systems 10 R and 10 L . However, the correction control of the mis-registration amounts Δa of images caused by a difference between the image formation magnifications of the right and left imaging optical systems 10 R and 10 L may be executed using the image signals output from the right and left imaging systems 10 R and 10 L . A multi-lens imaging apparatus according to such an embodiment of the present invention will be described below. Fig. 28 is a block diagram for explaining an operation of a magnification correlation calculation process portion in a multi-lens imaging apparatus according to still another embodiment of the present invention. The multi-lens imaging apparatus of this embodiment has substantially the same arrangement as that of the multi-lens imaging apparatus of the embodiment shown in Fig. 27, except that the apparatus of this embodiment includes a magnification correlation calculation process portion 281, a calculation process portion 282, and a third left side image memory 283. The operation of multi-lens imaging apparatus of this embodiment will be described below. Assume that the central positions of images obtained by the right and left side imaging systems 10 R and 10 L are registered with each other like in the multi-lens imaging apparatus of the embodiment shown in Fig. 27. The calculation process portion 282 converts the coordinates of image data output from the left side image memory 232 L by multiplying the coordinates with a constant k proportional to the distance from the center of the frame, and writes the coordinate-converted image data in the third left side image memory 283. The magnification correlation calculation process portion 281 executes a correlation calculation between image data output from the third left side image memory 283 and image data output from the right side image memory 232 R to obtain a correlation value δ s . When the correlation value δ s is equal to or larger than a predetermined value, the portion 281 calculates a new constant k, so that the correlation value δ s becomes equal to or smaller than the predetermined value, and outputs the constant to the calculation process portion 282. The calculation process portion 282 converts the coordinates of image data output from the left side image memory 232 L by multiplying the coordinates with the new constant k, and writes the coordinate-converted image data in the third left side image memory 283. Thereafter, the above-mentioned operations are repeated until the correlation value δ s becomes equal to or smaller than the predetermined value. After the correlation value δ s becomes equal to or smaller than the predetermined value, a synthesizing process circuit (not shown) synthesizes image data respectively output from the second left side image memory 262 and the right side image memory 232 R , thus obtaining a high-fine synthesized image signal from which the mis-registration amounts of images caused by a difference between the image formation magnifications of the right and left imaging optical systems 11 R and 11 L are corrected. Since a finally obtained constant k 0 indicates the ratio of image formation magnifications of the right and left imaging optical systems 11 R and 11 L , the magnification correlation calculation process portion 281 may calculate a correction signal according to the finally obtained constant k 0 , and may execute the correction control methods described in the embodiments shown in Figs. 21A to 25B. In order to shorten the correlation calculation time of the magnification correlation calculation process portion 281, the correlation calculation may be executed using only image signals in a hatched region (a region obtained by narrowing a horizontal process portion) having as its center a line Y-Y' passing through a point O on the object surface 2 and perpendicular to the plane including two optical axes L R and L L , as shown in Fig. 29. Since this region has symmetricity from the arrangement conditions of the right and left side imaging optical systems 11 R and 11 L , and suffers from a common image distortion, a difference between the image formation magnifications can be easily calculated. In order to shorten the correlation calculation time of the magnification correlation calculation process portion 281, a positional deviation correlation in the vertical direction may be calculated by the method described in the embodiment shown in Figs. 26A and 26B using only image signals in two upper and lower hatched regions which have as their center a line Y-Y' passing through the point O on the object surface 2 and perpendicular to the plane including two optical axes L R and L L , and which are separated from the point O, as shown in Fig. 30. When representative points of these regions are represented by Q and R, and when images of these representative points Q and R on the left side image sensor 12 L are represented by Q L ' and R L ' and images of these representative points Q and R on the right side image sensor 12 R are represented by Q R ' and R R ', a ratio of a line Q L ' - R L ' to a line Q R ' and R R ' is calculated to obtain the final constant k 0 . This technique utilizes the fact that the detection sensitivity of the difference between the image formation magnifications can be improved toward the periphery of the frame, and the fact that the difference between the image formation magnifications can be regarded as a positional deviation in a small region. The final constant k 0 is obtained as described above, and the following correction control can be made on the basis of this constant k 0 . (1) When the zoom motors 25 R and 25 L have response characteristics necessary for correcting the mis-registration amounts of images caused by the difference between the image formation magnifications to be equal to or smaller than a predetermined value (allowable value), servo control is executed by supplying a correction signal to one or both of the zoom motors 25 R and 25 L . (2) When it is difficult for the zoom motors 25 R and 25 L to obtain response characteristics necessary for correcting the mis-registration amounts due to the influence of the non-sensitive bands or the like, correction control by changing the scanning loci of the electron beams or correction control by converting the coordinates of the image memory is suitably executed. In this case, an interpolation calculation process of image data may be performed as needed. Each of the multi-lens imaging apparatuses according to the above-mentioned embodiments of the present invention comprises two imaging systems. However, the present invention can also be applied to an apparatus using three or more imaging systems. An embodiment of an apparatus for displaying images while partially overlapping image fields using a plurality of imaging systems, e.g., for obtaining a panoramic image or a 3D-2D mixed image is disclosed. Fig. 31 shows the basic arrangement of a panoramic multi-lens imaging system according to the present invention. The system includes a common object surface 1, and first and second imaging optical systems 102 and 202 having equivalent specifications, and normally comprising zoom lenses. The system also includes image sensors 103 and 203 similarly having equivalent specifications. Each of the image sensors 103 and 203 comprises a camera tube such as a saticon or a solid state imaging element such as a CCD. (Although Fig. 31 illustrates a single-sensor type (or single-tube type) image sensor for the sake of simplicity, versatility will not be disturbed even when a two-sensor type (two-tube type) image sensor or three-sensor type (three-tube type) image sensor via a color separation system is used.) Optical axes 101 and 201 of these image sensors are arranged to be inclined through about  symmetrically about a normal 0-0' to the object surface 1 so as to satisfy a condition that image fields to be picked up by these sensors overlap each other by a predetermined amount. Note that 2 will be referred to as the convergence angle, and is changed according to the image formation magnifications of the imaging optical systems (the object distances and the focal lengths of photographing lenses). Fig. 32 shows the detailed arrangement of the imaging optical systems and the image sensors. In Fig. 32, a support structure such as a lens barrel is not shown. The first and second imaging optical systems 102 and 202 are respectively constituted by lens groups 102a, 102b, 102c, and 102d, and lens groups 202a, 202b, 202c, and 202d. In particular, the lens groups 102b and 202b are zoom lens groups, and the lens groups 102d and 202d are focus lens groups. The zoom lens groups 102b and 202b are respectively driven by drive systems (zoom motors) 106 and 206, and similarly, the focus lens groups 102d and 202d are respectively driven by drive systems (focus motors) 107 and 207. Encoders (zoom encoders) 108 and 208 are provided to the zoom lens groups 102b and 202b of the imaging optical systems so as to obtain position information, in the optical axis direction, of the corresponding lens groups. Focal lengths f of the imaging optical systems 102 and 202 can be obtained based on signals output from the encoders 108 and 208. Note that the lens groups 102d and 202d also have a function of compensating for image surface movement upon movement of the zoom lens groups in addition to the focus function. Since the arrangement of the zoom lens is well known, a detailed description thereof will be omitted. Encoders (focus encoders) 109 and 209 are provided to the focus lens groups 102d and 202d of the imaging optical systems so as to obtain position information, in the optical axis direction, of the corresponding lens groups. These encoders may comprise, e.g., externally attached members such as potentiometers, or may comprise systems such as pulse motors for detecting the position information, in the optical axis direction, of the lens by the drive systems themselves according to their drive method. The system of this embodiment further includes mechanism systems (not shown) for integrally rotating the optical system 102 and the image sensor 103, and the optical system 202 and the image sensor 203 in opposite directions by the same amount in planes respectively including optical axes 101 and 201, and drive systems (convergence angle motors) 104 and 204 for attaining such rotations. The system also includes rotational angle information detecting means 105 and 205. These means may comprise, e.g., externally attached members such as rotary encoders, or may comprise systems such as pulse motors for detecting the position information, in the optical axis direction, of angle information by the drive systems themselves according to their drive method. A method of obtaining mis-registration amounts on the basis of image signals will be described below with reference to Figs. 33 and 34. Image memories 111 and 211 temporarily store signals of the overlapping portion of image signals 110 and 210. Assume that image data are mis-registered due to a deviation in convergence angle. A horizontal image shift process portion 20 shifts the coordinates of image data in the image memory 111 in the horizontal direction by a predetermined amount X (e.g., one pixel), and writes the shifted image data in a image memory 112. Furthermore, control for calculating a difference δ s between the contents of the image memories 112 and 211 is performed using a correlation calculation process portion 21 including a subtraction calculation process circuit and the like while sequentially changing the shift amount X so as to obtain a shift amount X 0 for minimizing the difference δ s . At this time, the shift amount X 0 is normally obtained by an interpolation calculation process by, e.g., approximating the relationship between the difference δ s and the shift amount X by, e.g., a function. In order to shorten the correlation calculation time, a method using only image data at the central portion of the frame of the overlapping portion, i.e., a region which includes a point 0 on the object surface 1 and whose vertical and horizontal widths are shortened is effective. Alternatively, coarse adjustment may be attained by commonly using the encoders 105 and 205 for outputting convergence angle information, and fine adjustment may be attained by the above-mentioned detection using the image signals, so as to further reduce the area of a region to be subjected to a correlation calculation. The correlation calculation method described here is normally called a matching method. However, the present invention is not particularly limited to this method, and other methods such as a gradient method may be used. The shift amount X 0 corresponding to the minimum value indicates a relative mis-registration amount Δy' itself of a image output from each imaging system, which mis-registration occurs due to a deviation of the optical axis 101 or 201 (Fig. 31) from an ideal optical axis. Therefore, convergence angle correction control is performed using a correction signal 10 for canceling the mis-registration amount Δy' of the image. The method of obtaining the mis-registration amount will be described below. Assume that an imaging operation is performed while the convergence angle has a deviation from a predetermined value, i.e., the optical axis 101 or 201 has an angular deviation Δ1 or Δ2 with respect to an axis having a predetermined angle . Under this assumption, the relationship between the angular deviation Δ1 or Δ2 and the mis-registration amount Δy' of a image will be described below. For the sake of simplicity, a mis-registration amount Δy' of a image output from each imaging system, which amount is generated since the optical axis 101 is deviated to an axis 101', as shown in Fig. 34, will be described below. The mis-registration amount with respect to the optical axis 201 can be obtained by the same equations, as is obvious to those who are skilled in the art from the arrangement of the optical systems, and even when both the optical axes 101 and 201 have deviations, the mis-registration amount can be obtained as a sum of the two deviations. Therefore, a method of obtaining the mis-registration amount with respect to one optical axis will be described below, and a description of the method for the other axis will be omitted. Note that reference symbols shown in Fig. 34 are used. Furthermore, under an assumption that Δ1 is very small, geometrically, we have: S 0 tanΔ1 = Δy· cos where Δy is the deviation (PP' in Fig. 34), generated in the object surface, of an intersection P of the optical axis 101 and the object surface 1 from a predetermined value, and S 0 is the distance from the front-side principal point of the imaging optical system (lens) 102 to an object (similarly, S 0 ' is the distance from the rear-side principal point to the image surface). If the image formation magnification of the imaging optical system 102 is represented by β, the magnification β can be expressed from its definition by: β = Δy'/Δy If the focal length of the imaging system (lens) is represented by f, we have: S 0 = f(β - 1)/β From equations (1), (2), and (3), the mis-registration amount Δy' is given by: Δy' = tanΔ1·f((β - 1)/cos The zoom lens group 102b of the imaging optical system shown in Fig. 32 is provided with the encoder (zoom encoder) 108 for obtaining position information, in the optical axis direction, of the lens group, and the focal length f of the imaging optical system 102 can be obtained based on a signal output from the encoder 108. Similarly, the focus lens group 102d of the imaging optical system is provided with the encoder (focus encoder) 109 for obtaining position information, in the optical axis direction, of the lens group, and the image formation magnification β of the imaging optical system 102 can be obtained based on both the signals from the zoom encoder 108 and the focus encoder 109. Assume that the focal lengths f and the image formation magnifications β of the two imaging optical systems 102 and 202 are caused to always coincide with each other by separately controlling the drive systems 105, 107, 206, and 207 on the basis of the signals from the encoders 108, 109, 208, and 209. As described above, the mis-registration amount Δy' of a image is obtained by a image signal process system, and the convergence angle 2, the focal length f, and the image formation magnification β are obtained by the encoders provided to each mechanism system. Based on these signals, a calculation control portion 22 obtains all the parameters except for Δ1 in equation (4). The calculated angular deviations Δ1 and Δ2 are supplied to a convergence angle control portion 23. Note that the convergence angle motors 104 and 204 have sufficient response performance for angular precision necessary for correcting Δy' to be equal to or smaller than a predetermined value (allowable value) Δy0'. The control portion 23 supplies Δ1 to the convergence angle motor 104 as a correction signal, and supplies Δ2 to the convergence angle motor 204 as a direct control target value. Alternatively, the sum of Δ1 and Δ2 may be supplied to one of the convergence angle motors 104 and 204. Fig. 35 shows the flow of these signals. In this manner, after the mis-registration amounts of the image signals 110 and 210 output from the corresponding imaging systems are mechanically corrected to be equal to or smaller than the predetermined value (allowable value) Δy0', images of the overlapping portion are subjected to a joint process, and thereafter, the image signals 110 can be synthesized to a single image signal 11 using, e.g., the image memories 111 and 211, an addition process circuit 24, and the like. Fig. 36 shows the flow of these signals. When such processes are sequentially performed as needed, a good panoramic image can always be obtained. A panoramic image is generally an image corresponding to a short focal length. However, as can be understood from equation (4), when the focal length f of the imaging optical system is large, or when the allowable value of the mis-registration amount of a image is small, the correction signals Δ1 and Δ2 also assume small values (on the order of several seconds), and it is difficult to obtain angular response performance necessary for correcting the mis-registration under the influence of, e.g., non-sensitive bands of the convergence angle motors 104 and 204. In this case, a method of correcting the mis-registration amount of a image output from each imaging system by a means other than the convergence angle motor 104 or 204 is effective. Such an embodiment will be described below. The basic arrangement of the embodiment shown in Fig. 37 is substantially the same as that of the embodiment shown in Fig. 32, except that precision correction means 103a and 203a are added. The first and second imaging optical systems 102 and 202 are respectively constituted by lens groups 102a, 102b, 102c, and 102d, and lens groups 202a, 202b, 202c, and 202d. In particular, the lens groups 102b and 202b are zoom lens groups, and the lens groups 102d and 202d are focus lens groups. The zoom lens groups 102b and 202b are respectively driven by drive systems (zoom motors) 106 and 206, and similarly, the focus lens groups 102d and 202d are respectively driven by drive systems (focus motors) 107 and 207. Encoders (zoom encoders) 108 and 208 are provided to the zoom lens groups 102b and 202b of the imaging optical systems so as to obtain position information, in the optical axis direction, of the corresponding lens groups. Similarly, encoders (focus encoders) 109 and 209 are provided to the focus lens groups 102d and 202d of the imaging optical systems so as to obtain position information, in the optical axis direction, of the corresponding lens groups. These encoders may comprise, e.g., externally attached members such as potentiometers, or may comprise systems such as pulse motors for detecting the position information, in the optical axis direction, of the lens by the drive systems themselves according to their drive method. The system of this embodiment further includes mechanism systems (not shown) for integrally rotating the optical system 102 and the image sensor 103, and the optical system 202 and the image sensor 203 in opposite directions by the same amount in planes respectively including optical axes 101 and 201, and drive systems (convergence angle motors) 104 and 204 for attaining such rotations. The system also includes rotational angle information detecting means 105 and 205. These means may comprise, e.g., externally attached members such as rotary encoders, or may comprise systems such as pulse motors for detecting the position information, in the optical axis direction, of angle information by the drive systems themselves according to their drive method. However, since the above-mentioned encoders are used for the auxiliary purpose, they are not always necessary in this embodiment. As has been described above with reference to Fig. 33, image memories 111 and 211 temporarily store signals of the overlapping portion of image signals 110 and 210. A horizontal image shift process portion 20 shifts the coordinates of image data in the image memory 111 in the horizontal direction by a predetermined amount X (e.g., one pixel), and writes the shifted image data in a image memory 112. Furthermore, control for calculating a difference δ s between the contents of the image memories 112 and 211 is performed using a correlation calculation process portion 21 including a subtraction calculation process circuit and the like while sequentially changing the shift amount X so as to obtain a shift amount X 0 for minimizing the difference δ s . At this time, the shift amount X 0 may be obtained by an interpolation calculation process by, e.g., approximating the relationship between the difference δ s and the shift amount X by, e.g., a function. When a swing motion in the vertical direction occurs as well due to insufficient precision of the mechanism system for driving the convergence angle motors, the same process as that for the horizontal direction may be performed for the vertical direction, and a two-dimensional (plane) mis-registration amount can be obtained. Note that a mis-registration amount Δy' (vertical) of a image in the vertical direction is given by: Δy' (vertical) = tanΔ1·f(β - 1) In order to shorten the correlation calculation time, a method using only image data at the central portion of the frame of the overlapping portion, i.e., a region which includes a point 0 on the object surface 1 and whose vertical and horizontal widths are shortened is effective. Alternatively, coarse adjustment may be attained by commonly using the encoders 105 and 205 for outputting convergence angle information, and fine adjustment may be attained by the above-mentioned detection using the image signals, so as to further reduce the area of a region to be subjected to a correlation calculation. The correlation calculation method described here is normally called a matching method. However, the present invention is not particularly limited to this method, and other methods such as a gradient method may be used. The shift amount X 0 corresponding to the minimum value indicates a relative mis-registration amount Δy' itself of a image output from each imaging system, which mis-registration occurs due to a deviation of the optical axis 101 or 201. Therefore, in this embodiment, correction control of the positions in a plane of the sensors is performed using a correction signal 10 according to the mis-registration amount Δy' of a image. More specifically, the image sensors 103 and 203 are provided with drive systems 103a and 203a capable of shifting the sensors in the horizontal and vertical directions. Signals calculated by a calculation control portion 22, which received various signals, are received by a sensor position control portion 25, and correction drive control is executed using the drive systems 103a and 203a. Each of the drive systems 103a and 203a comprises, e.g., a piezo element or a piezoelectric bimorph. Fig. 38 shows the flow of these signals. After the mis-registration amounts of the image signals 110 and 210 output from the imaging systems are corrected to be equal to or smaller than Δy0' as a predetermined allowable value, two images can be synthesized using, e.g., image memories and an addition process circuit like in the above embodiment. Since the flow of signals in this synthesizing process portion is common to that shown in Fig. 36, its illustration will be omitted here. The movable ranges of the drive systems 103a and 203a may be defined as follows. That is, in order to prevent a region to be subjected to aberration correction of the imaging optical system from being increased very much, and to prevent the load on the specifications of the drive system from being increased, the convergence angle encoders 105 and 205 may also be used, and the correction amount may be classified into coarse and fine levels with reference to a predetermined level, so that coarse adjustment is attained by driving the convergence angle motors 104 and 204, and fine adjustment is attained by driving the drive systems 103a and 203a. Fig. 39 shows still another embodiment of the present invention. In this embodiment, the image sensors 103 and 203 described in the embodiment shown in Fig. 37 are specified to camera tubes, and systems for driving the image sensors in the horizontal or vertical direction are not used. The arrangement except for the drive systems 103a and 203a and the method of obtaining the correction signal 10 are common to those in the above embodiment, and a detailed description thereof will be omitted. In general, the camera tubes read image signals by scanning electron beams. Therefore, camera tube electron beam scanning locus control drivers 103b and 203b for controlling the scanning loci of electron beams upon reading of the image signals are provided. As described above, signals calculated by the calculation control portion 22 which received various signals are received by an electron beam scanning locus control portion 26, and correction control for shifting the scanning loci of electron beams using the drivers 103b and 203b is executed. With this control, images defined by the image signals 110 and 210 output from the image sensors 103 and 203 can be registered. Fig. 40 shows the flow of these signals. Note that the above-mentioned technique for registering images by changing the scanning loci of electron beams is a general technique as DRC (Digital Registration Correction) in, e.g., a three-tube color television system. After the mis-registration amounts of the image signals 110 and 210 output from the imaging systems are corrected to be equal to or smaller than a predetermined value (allowable value) Δy0', two images can be synthesized using, e.g., image memories and an addition process circuit like in the above embodiment (since the flow of signals in this synthesizing process portion is common to that shown in Fig. 36, its illustration will be omitted here). Fig. 41 shows still another embodiment of the present invention, wherein the image sensors comprise solid-state imaging device in place of the camera tubes, and systems for driving the sensors in the horizontal or vertical direction are not used. More specifically, in this embodiment, the image sensors 103 and 203 described in the embodiment shown in Fig. 39 specifically use solid-state imaging device. Therefore, the basic arrangement and the method of obtaining the correction signal 10 are common to those in the embodiments shown in Figs. 37 and 39, and a detailed description thereof will be omitted. As shown in Fig. 42, signals calculated by a calculation control portion 22, which received various signals, are received by a image position control portion 27. Image memories 111 and 211 temporarily store image signals 110 and 210. Images defined by image data in this stage are not registered due to convergence angle errors. A correction conversion portion 28 converts the coordinates of image data. More specifically, the portion 28 executes control for shifting image data in the memory 111 by the calculated mis-registration amount Δy' of a image, and writing the shifted image data in a image memory 112. Although the image memories 112 and 111 are independently arranged for the sake of simplicity, a common memory may be used in place of these memories. When the coordinates of image data are shifted, a data interpolation calculation process may be performed as needed. In this embodiment, the coordinates of image data in the image memory 111 are shifted. Of course, the coordinates of image data in the image memory 211 may be shifted. Then, two images can be synthesized based on image data in the image memories 112 and 211, as shown in Fig. 36, using, e.g., the image memories and an addition process circuit like in the above embodiment. In the above embodiment, correction control of the mis-registration amounts Δy' of images due to convergence angle errors is executed. In some cases, mis-registration amounts of images due to a difference between image formation magnifications of imaging optical systems must also be taken into consideration. Such mis-registration amounts can also be detected using image signals independently of the encoders 108 and 109 for obtaining position information, in the optical axis direction, of the lenses. Such an embodiment will be described below. Fig. 43 shows still another embodiment of the present invention. The basic arrangement of this embodiment is the same as that of the embodiment shown in Fig. 37, and since the same reference numerals in Fig. 43 denote the same parts as in Fig. 37, a detailed description thereof will be omitted. The image memories 111 and 211 temporarily store image signals of the overlapping portions of the image signals 110 and 210. In this stage, images defined by image data are not registered due to a difference between the image formation magnifications of the imaging optical systems 102 and 202. In this case, assume that mis-registration amounts (Δy' described above) of the central positions of two images have already been detected by, e.g., the method described in the embodiments shown in Figs. 32 to 42, and the central positions of the two images have been corrected. As one method of a magnification correlation calculation process, the following method is known. More specifically, a magnification calculation process portion 29 converts the coordinates of image data in the image memory 111 by multiplying the coordinates with a constant k proportional to the distance from the center of the frame, and writes the coordinate-converted image data in a image memory 112. A difference δ m between the contents of the image memories 112 and 211 is then calculated using a subtraction process circuit 30. The above-mentioned subtraction process is repeated while sequentially changing the constant k, thereby obtaining a constant k 0 corresponding to the minimum difference δ m . Fig. 44 shows the flow of these signals. The constant k 0 represents the ratio of the image formation magnification of the imaging optical system 102 to that of the imaging optical system 202, and is defined as a correction signal 12. Fig. 45 shows a method of shortening the above-mentioned magnification correlation process time. In Fig. 45, only image signal portions 110a1 and 110a2, and 210a1 and 210a2 corresponding to two upper and lower regions 111A1 and 111A2 and two upper and lower regions 211A1 and 211A2, which portions respectively include a line Y-Y' passing through a point 0 on an object surface 1 and perpendicular to a plane including the optical axes 101 and 201, and are separated from the central portion 0, are used. Representative points of these regions on the object surface are represented by Q and R, and images of these points are represented by Q1', R1', Q2', and R2'. The positional deviation correlation, in the vertical direction of these points may be calculated by, e.g., the method described in the embodiments shown in Figs. 32 to 42, and the ratio of a length Q1'-R1' to a length Q2'-R2' may be calculated to obtain the constant k 0 . This technique utilizes the fact that the detection sensitivity of the difference between the image formation magnifications can be improved toward the periphery of the frame, and the fact that the difference between the image formation magnifications can be regarded as a positional deviation in a small region. The constant k 0 is obtained, as described above, and the following correction control can be executed based on this constant. More specifically, as a mis-registration correction method, when the zoom motors 106 and 206 have response performance necessary for obtaining a constant k 0 for correcting the mis-registration amounts of images caused by the difference between the image formation magnifications to be equal to or smaller than a predetermined value (allowable value), servo control is executed by supplying a correction signal to one or both of the zoom motors 106 and 206 so as to compensate for the magnifications. When it is difficult for the zoom motors 106 and 206 to obtain response performance necessary for correcting the mis-registration amounts due to the influence of the non-sensitive bands, correction control by changing the scanning loci of the electron beams described above with reference to Fig. 39 or correction control by converting the coordinates of the image memory in the above embodiment may be suitably executed. In this case, upon coordinate conversion of the image memory, an interpolation calculation process of image data may be performed as needed. As described above, an imaging apparatus which can obtain a panoramic image in which the boundary line is not conspicuous can be provided. In the above embodiment, a relatively large aspect ratio is set. However, an image having a desired aspect ratio can be obtained by changing the convergence angle 2. Fig. 46 shows the principle of a synthesizing system. In Fig. 46, an image having a new aspect ratio is obtained by synthesizing images from right and left side imaging systems. In this case, although the basic arrangement is the same as that shown in Fig. 31, the convergence angle 2 is selected to be smaller than that of a panoramic image. More specifically, the optical axes 101 and 201 shown in Fig. 31 are set to be symmetrically inclined through  with respect to the normal O-O' to the object surface 1, so that two image fields overlap each other by a predetermined amount according to a selected aspect ratio of a frame. For example, Fig. 47 shows a mode for converting an aspect ratio of 4 : 3 of images picked up by NTSC image sensors into an aspect ratio of 16 : 9 of an HD system. Therefore, a desired aspect ratio is determined first, and the convergence angle corresponding to the determined aspect ratio is set by a setting means 115 (Fig. 48) by driving the convergence angle motors 104 and 204. Thereafter, the registration compensation method described in each of the above embodiments is applied to obtain a desired image. The descriptions of the above embodiments have been made under an assumption that an object is a substantially flat one or can be regarded as a flat object. Next, an embodiment that can be applied to an object whose depth cannot be ignored will be described below. Fig. 49 shows a basic arrangement of a multi-lens imaging system according to still another embodiment of the present invention. The system shown in Fig. 49 includes a common object surface 1, and first and second imaging optical systems 102 and 202 having equivalent specifications, and normally comprising zoom lenses, as will be described later. Image sensors 103 and 203 similarly have equivalent specifications, and comprise camera tubes such as saticons, or solid-state imaging device such as CCDs. Although Fig. 49 illustrates a single-sensor type (or single-tube type) image sensor for the sake of simplicity, versatility will not be disturbed even when a two-sensor type (two-tube type) image sensor or three-sensor type (three-tube type) image sensor via a color separation system is used. Optical axes 101 and 201 of these imaging optical systems are set to cross at a point O on the object surface 1 and to be symmetrically inclined through  with respect to a normal O-O' to the object surface 1 while passing the point O. Note that 2 is defined as the convergence angle, and imaging operations are performed by changing the convergence angle according to a change in object distance S. Fig. 50 shows the detailed arrangement of the imaging optical systems 102 and 202, and Fig. 51 is a block diagram showing functions of the members constituting the imaging optical systems. The first and second imaging optical systems 102 and 202 are respectively constituted by lens groups 102a, 102b, 102c, and 102d, and lens groups 202a, 202b, 202c, and 202d. In particular, the lens groups 102b and 202b are zoom lens groups, and the lens groups 102d and 202d are focus lens groups. The zoom lens groups 102b and 202b are respectively driven by drive systems (zoom motors) 106 and 206, and similarly, the focus lens groups 102d and 202d are respectively driven by drive systems (focus motors) 107 and 207. The system of this embodiment further includes mechanism systems (not shown) for integrally rotating the optical system 102 and the image sensor 103, and the optical system 202 and the image sensor 203 in opposite directions by the same amount in planes respectively including optical axes 101 and 201, and drive systems (convergence angle motors) 104 and 204 for attaining such rotations. Angle encoders (rotational angle detecting means) 105 and 205 respectively measure the rotational angles of the imaging optical systems 102 and 202. Zoom encoders 108 and 208 respectively measure the moving amounts of the zoom lens groups 102b and 202b to obtain zoom ratios. Focus encoders 109 and 209 measure the positions of the focus lens groups. Image signals 110 and 210 are output from the image sensors 103 and 203, and are stored in image memories 111 and 211. Functions of a calculation control portion 12, a correlation calculation portion 13, and a correction calculation portion 14 will be described later. Detection of position information of an object when imaging operations are performed in an arrangement shown in Fig. 52 will be described below. As shown in Fig. 52, x-, y- and z-axes are defined to have the above-mentioned point O on the object surface as an origin. The intersections between the imaging optical systems 102 and 202 and their optical axes 101 and 201 are represented by Q R and Q L , the distance from the front-side principal point of the imaging optical system (lens) 102 or 202 to the above-mentioned point O is represented by S 0 , and the distance from the rear-side principal point to the image sensor 103 or 203 is represented by S 0 ' - A method of obtaining coordinates P 2 (x 0 , z 0 ) on the object surface 1 in the x-z plane shown in Fig. 53 will be briefly described below. If the intersections between the imaging optical systems 102 and 202 and their optical axes 101 and 201 are respectively represented by Q R (x 1 , -z 1 ) and Q L (-x 1 , -z 1 ), the coordinates x 1 and z 1 can be geometrically expressed as follows using the imaging condition S 0 and the convergence angle : x 1 = S 0 sin z 1 = S 0 cos Similarly, as for intersections O R ' (x 2 , -z 2 ) and O L ' (-x 2, -z 2 ) between the image sensors 103 and 203 and the optical axes 101 and 201, their coordinates are expressed by: x 2 = (S 0 + S 0 ')sin z 2 = (S 0 + S 0 ')cos As shown in Fig. 53, if image points on the image sensors 103 and 203 with respect to an object point P 2 (x 0 , z 0 ) on an object are respectively represented by P R ' (x R , -z R ) and P L ' (-x L , -z L ), and the image heights on the image sensors 103 and 203 are respectively represented by X R ' and X L ', geometrically, we have: x R = (S 0 + S 0 ')sin - x R 'cos z R = (S 0 + S 0 ')cos + x R 'sin x L = (S 0 + S 0 ')sin + x L 'cos z L = (S 0 + S 0 ')cos - x L 'sin At this time, if a line passing the points P R ' and Q R is represented by f R (S 0 , S 0 ', , x R '), and a line passing the points P L ' and Q L is represented by f L (S 0 , S 0 ', , x L '), the point P 2 (x 0 , z 0 ) on the object surface corresponds to the coordinates of the intersection of these two lines according to the definition. Also, as shown in Fig. 52, y 0 can be expressed as follows in association with the imaging optical system 102: y 0 = y R 'S R '/S R S R is the distance from the object point P 2 (x 0, z 0 ) to the front-side principal point of the imaging optical system 102 in Fig. 53, and S R ' is the distance from the rear-side principal point of the imaging optical system 102 to the image pint P R ' on the image sensor 103 in Fig. 53. At this time, a point P (x 0 , y 0 , z 0 ) in Fig. 52 is defined by: p = f(S 0 , S 0 ', , x R ', x L ', y R(L) ') That is, the point P is expressed by a function of imaging conditions (S 0 , S 0 ', ) and an output image (x R ', x L ', y R(L) ') of each image sensor, and position information on the object surface can be obtained by detecting these parameters. The method of obtaining parameters in the above-mentioned process will be described below with reference to Figs. 50 and 51. First, the convergence angle 2 is detected by the rotational angle detecting means 105 and 205 such as rotary encoders. The encoders (zoom encoders) 108 and 208 for obtaining position information, in the optical axis direction, of the corresponding lens groups are used, and the focal lengths f of the imaging optical systems 102 and 202 are obtained based on the signals output from these encoders. Similarly, the encoders (focus encoders) 109 and 209 for obtaining position information, in the optical axis direction, of the corresponding lens groups are provided to the focus lens groups 102d and 202d of the imaging optical systems. These encoders may comprise, e.g., externally attached members such as potentiometers, or may comprise systems such as pulse motors for detecting the position information, in the optical axis direction, of the lens by the drive systems themselves according to their drive method. The calculation control portion 12 calculates the object distances S 0 to the imaging optical systems 102 and 202 on the basis of the signals from the focus encoders 109 and 209. Furthermore, the portion 12 calculates lens backs S 0 ' of the imaging optical systems 102 and 202 together with the focal lengths f of the imaging optical systems 102 and 202. Note that the focal lengths f and the lens backs S 0 ' of the two imaging optical systems 102 and 202 are caused to always coincide with each other by independently controlling the drive systems 106, 107, 206, and 207 on the basis of the signals from the encoders 108, 109, 208, and 209. As described above, the calculation control portion 12 calculates S 0 (the distance from the front-side principal point of the imaging optical system (lens) to the intersection of the corresponding optical axis), S 0 ' (the distance from the rear-side principal point of the imaging optical system (lens) to the image surface), and  (convergence angle) on the basis of the signals from the encoders 105, 108, 109, 205, 208, and 209. The image memories 111 and 211 temporarily store image signals 110 and 210. The correlation calculation process portion 13 performs a correlation calculation about image data stored in the image memories 111 and 211. Figs. 54A and 54B show the principle of a correlation calculation process. In the process, as shown in Fig. 54B, a pixel data group 112 having pixel data R ij at a point (x iR ', y jR ') as a center is defined as one block, and a correlation calculation is performed between this block and a corresponding image block on the image memory 211. Fig. 55 illustrates the relationship between a correlation value and an x' (y') axis coordinate in the correlation calculation in the horizontal and vertical directions. In Fig. 55, X L ' (y L ') corresponding to a maximum correlation value is obtained with a precision equal to or lower than the sampling pitch of the image sensor by, e.g., approximating the relationship near the correlation peak by a function. The block 112 is also defined for other pixel data R ij on the image memory 111, and a similar calculation process is executed to obtain X L ' and y L ' for each pixel data. The coordinates P R (x 0, y 0 , z 0 ) on the object surface corresponding to each pixel data R ij on the image sensor 103 can be calculated from the relationship given by equation (5) using the image information (x iR ', x L ', y jR ') obtained by these series of processes, and the imaging conditions (S 0 , S 0 ', ). The same calculation process is executed for each pixel data L ij (x iL ', Y jL ') of the image sensor 203 to obtain x R ' and y R ' for each pixel, and the coordinates P L (x 0 , y 0 , z 0 ) on the object surface corresponding to each pixel data L ij on the image sensor 203 are then calculated. Note that the coordinates P R and P L on the object surface do not always coincide with each other. The correction process portion 14 executes a process on the basis of the coordinates P R and P L obtained by the above-mentioned process. In the correction process portion 14, a desired view position is input. At this time, when the view position is input, as shown in Fig. 56, image points (x', y') corresponding to the coordinate values can be obtained as follows using the above-mentioned imaging conditions S 0 and S 0 ' and the coordinates P R(L) (x 0 , y 0 , z 0 ) on the object surface: x' = x 0 S 0 '/(S 0 + z 0 ) y' = y 0 S 0 '/(S 0 + z 0 ) The coordinates (x iR(L) ', Y iR(L) ') on each image memory are coordinate-converted by a calculation process on the basis of equations (6-a) and (6-b), and the converted data are written in a image memory 15. The mis-registration amounts have been removed from the image data stored in the image memory 15, and the image data is ideally twice image data output from the image sensors 103 and 203. As a result, a high-fine output image can be obtained. The embodiment described above with reference to Fig. 49 and subsequent drawings can be applied to a panoramic image and images having various aspect ratios. In this case, since an operation for extracting corresponding points on at least partial regions of a plurality of images is required, the images must partially overlap each other. A plurality of imaging optical systems of every embodiment does not always lie in the same mode. For a different purpose, a different mode imaging optical system is sometimes used. With the above-mentioned arrangements of the present invention, the following effects can be expected. Even when images obtained by imaging systems suffer from keystone distortions, the keystone distortions can be removed, and the images can be converted into desired images, thus obtaining a high-fine image free from keystone distortions. Since at least one of a mechanism system or image process system is controlled so as to correct a mis-registration amount detected by a detecting means to be equal to or smaller than a predetermined value, images obtained by imaging systems can be registered and synthesized. For this reason, an apparatus which can obtain a high-fine image by picking up an image of a common object using a plurality of imaging systems can be provided. Also, an apparatus capable of obtaining an image having very high image quality and a desired aspect ratio, and an apparatus capable of obtaining a panoramic image free from a conspicuous boundary line can be provided. When a multi-lens imaging apparatus of the present invention is connected to a display device such as a CRT via an image process apparatus, it can be utilized as a high-performance panoramic TV system, a 3D TV system, an HDTV system, and the like. Similarly, when the apparatus of the present invention is connected to a recording apparatus via the image process apparatus, it can be utilized as a high-performance recording system. This invention relates to a multi-lens imaging apparatus and, more particularly, to a multi-lens imaging apparatus for obtaining a single high-fine image by synthesizing a plurality of images obtained by picking up an image of a common object using a plurality of imaging systems and to an apparatus which can provide an image having an aspect ratio different from that of an image obtained by a single imaging apparatus, especially, a panoramic image, by synthesizing a plurality of images using a plurality of imaging systems. This invention has as its object to obtain a high-fine image by synthesizing images from a plurality of imaging systems and, more specifically, to correct mis-registration such as keystone distortions generated in the images.

Claims: A multi-lens imaging apparatus comprising: a plurality of imaging optical systems (10 R , 10 L ), image sensing means (12 R , 12 L ) for sensing images of an object corresponding to said plurality of imaging optical systems via said plurality of imaging optical systems, detection means (28 R , 28 L , 41 R , 41 L , 42 R , 42 L ) for detecting displacement amounts of registration of the images of the object obtained from said plurality of imaging optical systems, including convergence angle detection means (28 R , 28 L ) for detecting an angle defined between optical axes (L R , L L ) of said plurality of imaging optical systems, zoom encoders (41 R , 41 L ) for detecting focal lengths of said imaging optical systems, and focus encoders (42 R , 42 L ) for detecting object distances to said imaging optical systems, correction means for correcting the displacement amounts to be less than a predetermined value using the detection output signals of said convergence angle detection means, said zoom encoders and said focus encoders, and synthesizing means (38) for synthesizing the corrected images of the object. An apparatus according to claim 1, wherein said image sensing means (12 R , 12 L ) comprise camera tubes, and said apparatus further comprises correction signal generation means for generating a correction signal of the displacement amounts of registration on the basis of output signals from said convergence angle detection means (28 R , 28 L ), said zoom encoders (41 R , 41 L ), and said focus encoders (42 R , 42 L ), and camera tube electron beam scanning locus control drivers (31 R , 31 L ) for controlling electron beams of said camera tubes on the basis of the correction signal. An apparatus according to claim 1, wherein said image sensing means (12 R , 12 L ) comprise solid-state image pickup elements, and said apparatus further comprises image memories (72 R , 72 L ) for storing a plurality of image data from said solid-state image pickup elements, correction conversion means (52 R , 52 L ) for obtaining the displacement amounts of registration of the plurality of image data, and executing coordinate conversion of the image data, and executing coordinate conversion of the image data to cancel the displacement amounts of registration, and synthesizing process means (38) for synthesizing the plurality of image data. An apparatus according to claim 1, wherein optical axes of said plurality of image pickup optical systems (10 R , 10 L ) are not parallel to each other, and said displacements of registration are caused by keystone distortions of the images of the object. An apparatus according to claim 1, wherein the displacements of registration are caused by a difference between image formation magnifications of said plurality of imaging optical systems (10 R , 10 L ), and said apparatus comprises a magnification correlation calculation process portion (281) and a calculation process portion (282). An apparatus according to claim 5, wherein said magnification correlation calculation process portion (281) calculates positional deviations associated with distances from a center to corresponding positions on a plurality of frames, and inputs a constant for correcting the positional deviations to said calculation process portion (282). An apparatus according to claim 6, wherein said magnification correlation calculation process portion (281) executes a correlation calculation using image signals in a partial region having a line passing central portions of the plurality of frames and perpendicular to a plane including the optical axes of at least two of said imaging optical systems (10 R , 10 L ) defined as a center. An apparatus according to claim 1, further comprising: a plurality of imaging optical systems (10 R , 10 L ) whose optical axes are not parallel to each other; and keystone distortion correction means (32 R , 32 L ) for correcting a keystone distortion generated in at least one image obtained through said image sensing means (12 R , 12 L ), wherein said synthesizing means (38) synthesizes the plurality of images. An apparatus according to claim 8, wherein said keystone distortion correction means (32 R , 32 L ) corrects the keystone distortion with reference to focal lengths, image formation magnifications, and inclination angles of the optical axes with respect to an object surface of said plurality of imaging optical systems (10 R , 10 L ). An apparatus according to claim 8, wherein said keystone distortion correction means (32 R , 32 L ) executes a conversion process of images obtained by said plurality of imaging optical systems (10 R , 10 L ) on the basis of focal lengths and image formation magnifications of said plurality of imaging optical systems (10 R , 10 L ) using an arbitrary conversion variable so as to obtain a difference between the converted images, and corrects the keystone distortion using the conversion variable to minimize the difference between the images. An apparatus according to claim 8, wherein said keystone distortion correction means (32 R , 32 L ) detects a distortion amount of the keystone distortion using, as parameters which are focal lengths, image formation magnifications, and inclination angles of the optical axes with respect to an object surface of said plurality of imaging optical systems (10 R , 10 L ), calculates a difference between an image from which the keystone distortion is corrected according to the detected distortion amount and a desired image, and sets up the inclination angles to minimize the difference, thereby correcting the keystone distortion. An apparatus according to claim 8, wherein said image sensing means (12 R , 12 L ) comprise camera tubes. An apparatus according to claim 8, wherein said image sensing means (12 R , 12 L ) comprise solid-state imaging devices. An apparatus according to claim 1, wherein said plurality of imaging optical systems (10 R , 10 L ) pick up an image while image fields at least partially overlap each other, said apparatus further comprising: detection means (28 R , 28 L , 41 R , 41 L , 42 R , 42 L ) for extracting image signals of the overlapping portion of images obtained from said plurality of imaging optical systems, and detecting a displacement amount of registration of the overlapping portion. An apparatus according to claim 14, further comprising convergence angle changing means for making an angle formed between optical axes of said plurality of imaging optical systems (10 R , 10 L ) change. An apparatus according to claim 1, further comprising: means for detecting imaging conditions of said plurality of imaging optical systems (10 R , 10 L ); means for detecting position information of the object from the image signals from said image sensing means (12 R , 12 L ); and wherein said image synthesizing means (38) synthesizes the plurality of images on the basis of the imaging conditions and the position information so that corresponding points of the plurality of images coincide with each other. An apparatus according to claim 16, wherein said image synthesizing means (38) forms a synthesized image with reference to a predetermined view position. An apparatus according to claim 1, further comprising: detection means (28 R , 28 L , 41 R , 41 L , 42 R , 42 L ) for detecting three-dimensional position information of a plurality of points in each of the images obtained by said image sensing means (12 R , 12 L ); and wherein said synthesizing means (38) generates a synthesized image of the plurality of images on the basis of the position information. An apparatus according to claim 1, further comprising: a recording apparatus for executing an image process of an image signal from said multi-lens imaging apparatus, and recording the processed image signal. An apparatus according to claim 1, further comprising: an image process apparatus for synthesizing a plurality of image signals from said multi-lens imaging apparatus (10 R , 10 L ); and a display apparatus (40) for displaying an image according to an image signal from said image process apparatus.

Inventors: KATAYAMA TATSUSHI, NIWA YUKICHI, SUDA SHIGEYUKI, KATAYAMA, TATSUSHI, NIWA, YUKICHI, SUDA, SHIGEYUKI, Katayama, Tatsushi, c/o Canon Kabushiki Kaisha, Niwa, Yukichi, c/o Canon Kabushiki Kaisha, SUDA, SHIGEYUKI, C/O CANON KABUSHIKI KAISHA
Applicants: CANON KK, CANON KABUSHIKI KAISHA
Application year: 1993
Main classification: H04N13
IPC codes: H04N13, H04N3, G06T3