Image-effect method and apparatus using critical points

Abstract

An image-effect apparatus which provides high quality motion pictures and image effects such as supper slow motion based on a small amount of image data. An image input unit inputs a first image and a second image. A matching processor performs pixel matching between the first image and the second image, and a result thereof is recorded as a corresponding point file. An intermediate image generator generates an intermediate image between the first image and the second image based on the corresponding point file. A speed controller controls the number of intermediate images to be generated, based on a user's instruction. As the number of intermediate images generated is increased, slow motion and super slow motion images are produced.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to image-effect techniques and more particularly relates to a method and apparatus for digital image effects.

2. Description of the Related Art

As a part of the digital revolution, many users have come to enjoy services on the Internet from personal computers and portable telephones. Now, the digital revolution is spreading to broadcast services and movies, including digital satellite broadcasts. Thus, a barrier that had previously existed between broadcasting and communications is quickly beginning to disappear. Moreover, as broadband communications grow, multimedia content and culture will experience significant development, and, as a part of this multimedia culture, the distribution of video or motion pictures will become a key technology.

When humans acquire information from the outside world, images are capable of conveying much more information than audio. Besides being used for entertainment and recreational purposes, it is believed that images will also serve as a vital part of a software infrastructure which will support a wide range of aspects of human life and culture. As images are used more and more in a digital form, image-effect technology will expand into many fields with additional applications in computer graphics (CG) and image processing technologies.

Various image effects have been proposed and used in image processing. For example, known effects include slow motion, walk-through, multi-viewpoint image, special filtering, pseudo stereoscopic vision and so forth. However, many of these effects require expensive equipment that may be difficult to operate or require extensive human input or provide only low quality output. As the importance of images grows in the future, it is important that these and other image effects be provided with efficiency, cost-effectiveness and improved quality.

SUMMARY OF THE INVENTION

The present invention has been made in view of the forgoing circumstances and an object of the present invention is to provide a new image effect method and apparatus for motion pictures.

Though the present invention relates to an image-effect technology, the use of the technology is not limited to image effects only. For example, a compression effect of motion pictures is equally realized by the new technology, and it lies of course within the scope of the use of the present invention.

An embodiment according to the present invention relates to an image-effect apparatus that includes: an intermediate image generator which acquires a first image, a second image, and a corresponding point file for the first image and the second image, and which generates an intermediate image between the two images; and a speed controller which controls an operation of the intermediate image generator with respect to a speed at which the intermediate image is generated and/or reproduced. The apparatus may further include a speed specifying unit which receives from a user a desired speed, and the speed controller may control the operation of the intermediate image generator according to the desired speed. In particular, the speed controller may control the number of intermediate images generated by the intermediate image generator.

In this embodiment, when a slow speed is desired or specified (so-called slow motion pictures are demanded), the slow motion pictures are realized by generating many intermediate images and displaying them. The interval at which the intermediate images are displayed may also be varied. Setting the speed very low provides super slow motion images that may be beyond the shooting capabilities of an actual camera.

Another embodiment of the present invention relates also to an image-effect apparatus. This apparatus includes: an image input unit which acquires a first image and a second image; a matching processor which computes a matching between the first image and the second image, and which then outputs a matching result as a corresponding point file; an intermediate image generator which generates an intermediate image between the first image and the second image based on the corresponding point file; and a speed controller which controls the intermediate image generator with respect to a speed at which the intermediate image is generated. According to this apparatus, the corresponding point file can be generated within the apparatus itself, so that any processing up to generation of the intermediate image is completed simply after the input of the first image and the second image. The apparatus may also include a display unit which displays the first image, the intermediate image, and the second image as a moving picture.

In these embodiments, the corresponding point file may describe lattice points of a mesh taken on the first image and a positional relation of points in the second image which correspond to the lattice points. The matching processor may generate the corresponding point file in a manner such that a destination polygon in the second image is defined for a source polygon that constitutes a mesh on the first image.

Further, the matching processor may perform a pixel-by-pixel matching computation based on correspondence between critical points detected through a two-dimensional search on the first image and critical points detected through a two-dimensional search on the second image.

Moreover, in this case the matching processor may multiresolutionalize the first image and the second image by respectively extracting the critical points, then may perform a pixel-by-pixel matching computation between related multiresolution levels while also inheriting a result of a pixel-by-pixel matching computation at a different multiresolution level in order to acquire a pixel-by-pixel correspondence relation at a finest level of resolution at a final stage.

These above-described matching methods utilizing the critical points may be an application of the technology (hereinafter referred to as the “premised technology”) proposed earlier in Japanese Patent No. 2927350 by inventors of this patent specification, and are suitable for the matching processor. However, the premised technology does not touch on features of the present invention, such as those relating to the lattice points or the polygons determined thereby. Introduction of a novel techniques such as the use of polygons allows a significant reduction in the size of the corresponding point file.

As an example, in a case where the first and second images have n×m pixels respectively, there are (n×m)² combinations required to describe pixel-by-pixel correspondence, so that the size of the corresponding point file may become extremely large. However, if, this correspondence is modified by describing the correspondence relation between the lattice points or, substantially equivalently, the correspondence relation between polygons determined by the lattice points, the data amount is reduced significantly.

Still another embodiment of the present invention relates also to an image-effect apparatus. This apparatus includes: an intermediate image generator which acquires a first image and a second image which are extracted, as frame images, from a motion picture, and also acquires a corresponding point file between the two images, and then generates one or more intermediate images between the two images by performing an interpolation computation thereon; a speed controller which controls the intermediate image generator with respect to a speed at which the intermediate images are generated; and a speed specifying unit which receives from a user a specification with respect to the speed at which the images are generated, and the speed controller controls the number of the intermediate images generated by the intermediate image generator according to the specification from the user.

In this embodiment, the number of intermediate images generated may be substantially greater than a number of slow motion frame images capable of being generated by an image shooting apparatus which captured the motion picture. According to this embodiment, advanced super slow motion images can be generated which may exceed the super slow motion capability of current cameras, such as television cameras.

Moreover, in the above embodiments, where appropriate, the speed specifying unit, the speed controller and the intermediate image generator may operate even during generation of intermediate images such that the intermediate image generator may change a number of the intermediate images generated according to the specification from the user. Thus, the speed specifying unit may receive, even during generation, reproduction or display of the intermediate image, an instruction as to the desired speed and the speed controller may suitably change, even during generation or display of the intermediate image, a speed for the intermediate image generator, and the intermediate image generator may suitably change the number of intermediate images generated according to a speed from the speed controller. Thus, the speed may be adjusted in real time by a user.

Still another embodiment of the present invention relates also to an image-effect method that includes: acquiring a first image and a second image which are extracted, as frame images, from a motion picture, and also acquiring a corresponding point file between the first image and the second image; generating an intermediate image between the two images by performing an interpolation computation; acquiring a user's instruction with respect to a speed at which the intermediate images are to be generated; and controlling the number of intermediate images which are generated according to the instruction.

In this embodiment, the controlling may include increasing the number of intermediate images so that the number of intermediate images generated is substantially greater than a number of slow motion images capable of being captured by an image shooting apparatus, such as a camera which captured the motion picture.

It is to be noted that the premised technology is not a prerequisite in the present invention. Moreover, it is also possible to have replacement or substitution of the above-described structural components and elements of methods in part or whole as between method and apparatus or to add elements to either method or apparatus. Also, the apparatuses and methods may be implemented by a computer program and saved on a recording medium or the like and are all effective as and encompassed by the present invention.

Moreover, this summary of the invention includes features that may not be necessary features such that an embodiment of the present invention may also be a sub-combination of these described features.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1( a) is an image obtained as a result of the application of an averaging filter to a human facial image.

FIG. 1( b) is an image obtained as a result of the application of an averaging filter to another human facial image.

FIG. 1( c) is an image of a human face at p^(5,0) obtained in a preferred embodiment in the premised technology.

FIG. 1( d) is another image of a human face at p^(5,0) obtained in a preferred embodiment in the premised technology.

FIG. 1( e) is an image of a human face at p^(5,1) obtained in a preferred embodiment in the premised technology.

FIG. 1( f) is another image of a human face at p^(5,1) obtained in a preferred embodiment in the premised technology.

FIG. 1( g) is an image of a human face at p^(5,2) obtained in a preferred embodiment in the premised technology.

FIG. 1( h) is another image of a human face at p^(5,2) obtained in a preferred embodiment in the premised technology.

FIG. 1( i) is an image of a human face at p^(5,3) obtained in a preferred embodiment in the premised technology.

FIG. 1( j) is another image of a human face at p^(5,3) obtained in a preferred embodiment in the premised technology.

FIG. 2(R) shows an original quadrilateral.

FIG. 2(A) shows an inherited quadrilateral.

FIG. 2(B) shows an inherited quadrilateral.

FIG. 2(C) shows an inherited quadrilateral.

FIG. 2(D) shows an inherited quadrilateral.

FIG. 2(E) shows an inherited quadrilateral.

FIG. 3 is a diagram showing the relationship between a source image and a destination image and that between the m-th level and the (m−1)th level, using a quadrilateral.

FIG. 4 shows the relationship between a parameter η (represented by x-axis) and energy C_f (represented by y-axis)

FIG. 5( a) is a diagram illustrating determination of whether or not the mapping for a certain point satisfies the bijectivity condition through the outer product computation.

FIG. 5( b) is a diagram illustrating determination of whether or not the mapping for a certain point satisfies the bijectivity condition through the outer product computation.

FIG. 6 is a flowchart of the entire procedure of a preferred embodiment in the premised technology.

FIG. 7 is a flowchart showing the details of the process at S1 in FIG. 6.

FIG. 8 is a flowchart showing the details of the process at S10 in FIG. 7.

FIG. 9 is a diagram showing correspondence between partial images of the m-th and (m−1)th levels of resolution.

FIG. 10 is a diagram showing source images generated in the embodiment in the premised technology.

FIG. 11 is a flowchart of a preparation procedure for S2 in FIG. 6.

FIG. 12 is a flowchart showing the details of the process at S2 in FIG. 6.

FIG. 13 is a diagram showing the way a submapping is determined at the 0-th level.

FIG. 14 is a diagram showing the way a submapping is determined at the first level.

FIG. 15 is a flowchart showing the details of the process at S21 in FIG. 6.

FIG. 16 is a graph showing the behavior of energy C_f^(m,s) corresponding to f^(m,s) (λ=iΔλ) which has been obtained for a certain f^(m,s) while changing λ.

FIG. 17 is a diagram showing the behavior of energy C_f⁽ⁿ⁾ corresponding to f⁽ⁿ⁾ (η=iΔη)(i=0, 1, . . . ) which has been obtained while changing η.

FIG. 18 shows how certain pixels correspond between the first image and the second image.

FIG. 19 shows a correspondence relation between a source polygon taken on the first image and a destination polygon taken on the second image.

FIG. 20 shows a procedure by which to obtain points in the destination polygon corresponding to points in the source polygon.

FIG. 21 is a flowchart showing a procedure for generating the corresponding point file, according to a present embodiment.

FIG. 22 is a flowchart showing a procedure for generating an intermediate image based on the corresponding point file, according to a present embodiment.

FIG. 23 shows a structure of an image-effect apparatus according to an embodiment.

DETAILED DESCRIPTION OF THE INVENTION

The invention will now be described based on the preferred embodiments, which do not intend to limit the scope of the present invention, but exemplify the invention. All of the features and the combinations thereof described in the embodiment are not necessarily essential to the invention.

First, the multiresolutional critical point filter technology and the image matching processing using the technology, both of which will be utilized in the preferred embodiments, will be described in detail as “Premised Technology”. Namely, the following sections [1] and [2] (below) belong to the premised technology, where section [1] describes elemental techniques and section [2] describes a processing procedure. These techniques are patented under Japanese Patent No. 2927350 and owned by the same assignees of the present invention. As described in more detail below following the discussion of the premised technology, according to embodiments of the present invention there is provided a mesh on an image, so that lattice points of the mesh represent a plurality of pixels of the image. Thus, even though application efficiency for a pixel-by-pixel matching technique as described in the premised technology is naturally high, it is to be noted that the image matching techniques provided in the present embodiments are not limited to the same levels. In particular, in FIGS. 18 to 23, image effects techniques and apparatus representing embodiments of the present invention and utilizing the premised technology will be described in a specific manner.

Premised Technology

[1] Detailed Description of Elemental Techniques

[1.1] Introduction

Using a set of new multiresolutional filters called critical point filters, image matching is accurately computed. There is no need for any prior knowledge concerning the content of the images or objects in question. The matching of the images is computed at each resolution while proceeding through the resolution hierarchy. The resolution hierarchy proceeds from a coarse level to a fine level. Parameters necessary for the computation are set completely automatically by dynamical computation analogous to human visual systems. Thus, There is no need to manually specify the correspondence of points between the images.

The premised technology can be applied to, for instance, completely automated morphing, object recognition, stereo photogrammetry, volume rendering, and smooth generation of motion images from a small number of frames. When applied to morphing, given images can be automatically transformed. When applied to volume rendering, intermediate images between cross sections can be accurately reconstructed, even when a distance between cross sections is rather large and the cross sections vary widely in shape.

[1.2] The Hierarchy of the Critical Point Filters

The multiresolutional filters according to the premised technology preserve the intensity and location of each critical point included in the images while reducing the resolution. Initially, let the width of an image to be examined be N and the height of the image be M. For simplicity, assume that N=M=2n where n is a positive integer. An interval [0, N]⊂R is denoted by I. A pixel of the image at position (i, j) is denoted by p^(i,j) where i,jεI.

Here, a multiresolutional hierarchy is introduced. Hierarchized image groups are produced by a multiresolutional filter. The multiresolutional filter carries out a two dimensional search on an original image and detects critical points therefrom. The multiresolutinal filter then extracts the critical points from the original image to construct another image having a lower resolution. Here, the size of each of the respective images of the m-th level is denoted as 2^m×2^m (0<m<n). A critical point filter constructs the following four new hierarchical images recursively, in the direction descending from n.p_(i,j)^(m,0)=min(min(p_(2i,2j)^(m+1,0),p_(2i,2j+1)^(m+1,0)),min(p_(2i+1,2j)^(m+1,0),p_(2i+1,2j+1)^(m+1,0)))p_(i,j)^(m,1)=max(min(p_(2i,2j)^(m+1,1),p_(2i,2j+1)^(m+1,1)),min(p_(2i+1,2j)^(m+1,1),p_(2i+1,2j+1)^(m+1,1)))p_(i,j)^(m,2)=min(max(p_(2i,2j)^(m+1,2),p_(2i,2j+1)^(m+1,2)),max(p_(2i+1,2j)^(m+1,2),p_(2i+1,2j+1)^(m+1,2)))p_(i,j)^(m,3)=max(max(p_(2i,2j)^(m+1,3), p_(2i,2j+1)^(m+1,3)),max(p_(2i+1,2j)^(m+1,3), p_(2i+1,2j+1)^(m+1,3)))  (1)where we letp_(i,j)^(n,0)=p_(i,j)^(n,1)=p_(i,j)^(n,2)=p_(i,j)^(n,3)=p_(i,j)  (2)

The above four images are referred to as subimages hereinafter. When min_x≦t≦x+1 and max_x≦t≦x+1 are abbreviated to α and β, respectively, the subimages can be expressed as follows:P^(m,0)=α(x)α(y)p^(m+1,0)P^(m,1)=α(x)β(y)p^(m+1,1)P^(m,2)=β(x)α(y)p^(m+1,2)P^(m,2)=β(x)β(y)p^(m+1,3)

Namely, they can be considered analogous to the tensor products of α and β. The subimages correspond to the respective critical points. As is apparent from the above equations, the critical point filter detects a critical point of the original image for every block consisting of 2×2 pixels. In this detection, a point having a maximum pixel value and a point having a minimum pixel value are searched with respect to two directions, namely, vertical and horizontal directions, in each block. Although pixel intensity is used as a pixel value in this premised technology, various other values relating to the image may be used. A pixel having the maximum pixel values for the two directions, one having minimum pixel values for the two directions, and one having a minimum pixel value for one direction and a maximum pixel value for the other direction are detected as a local maximum point, a local minimum point, and a saddle point, respectively.

By using the critical point filter, an image (1 pixel here) of a critical point detected inside each of the respective blocks serves to represent its block image (4 pixels here) in the next lower resolution level. Thus, the resolution of the image is reduced. From a singularity theoretical point of view, α(x) α(y) preserves the local minimum point (minima point), α(x) β(y) preserves the local maximum point (maxima point), α(x) β(y) and β(x) α(y) preserve the saddle points.

At the beginning, a critical point filtering process is applied separately to a source image and a destination image which are to be matching-computed. Thus, a series of image groups, namely, source hierarchical images and destination hierarchical images are generated. Four source hierarchical images and four destination hierarchical images are generated corresponding to the types of the critical points.

Thereafter, the source hierarchical images and the destination hierarchical images are matched in a series of resolution levels. First, the minima points are matched using p^(m,0). Next, the first saddle points are matched using p^(m,1) based on the previous matching result for the minima points. The second saddle points are matched using p^(m,2). Finally, the maxima points are matched using p^(m,3).

FIGS. 1 c and 1d show the subimages p^(5,0) of the images in FIGS. 1a and 1b, respectively. Similarly, FIGS. 1e and 1f show the subimages p^(5,1), FIGS. 1g and 1h show the subimages p^(5,2), and FIGS. 1i and 1j show the subimages p^(5,3). Characteristic parts in the images can be easily matched using subimages. The eyes can be matched by p^(5,0) since the eyes are the minima points of pixel intensity in a face. The mouths can be matched by p^(5,1) since the mouths have low intensity in the horizontal direction. Vertical lines on both sides of the necks become clear by p^(5,2). The ears and bright parts of the cheeks become clear by p^(5,3) since these are the maxima points of pixel intensity.

As described above, the characteristics of an image can be extracted by the critical point filter. Thus, by comparing, for example, the characteristics of an image shot by a camera with the characteristics of several objects recorded in advance, an object shot by the camera can be identified.

[1.3] Computation of Mapping between Images

Now, for matching images, a pixel of the source image at the location (i,j) is denoted by p_(i,j)⁽ⁿ⁾ and that of the destination image at (k,l) is denoted by q_(k,l)⁽ⁿ⁾ where i, j, k, l ε I. The energy of the mapping between the images (described later in more detail) is then defined. This energy is determined by the difference in the intensity of the pixel of the source image and its corresponding pixel of the destination image and the smoothness of the mapping. First, the mapping f^(m,0):p^(m,0)→q^(m,0) between p^(m,0) and q^(m,0) with the minimum energy is computed. Based on f^(m,0), the mapping f^(m,1) between p^(m,1) and q^(m,1) with the minimum energy is computed. This process continues until f^(m,3) between p^(m,3) and q^(m,3) is computed. Each f^(m,i) (i=0, 1, 2, . . . ) is referred to as a submapping. The order of i will be rearranged as shown in the following equation (3) in computing f^(m,i) for reasons to be described later.f^(m,i):p^(m,σ(i))→q^(m,σ(i))  (3)where σ(i)ε{0, 1, 2, 3}.[1.3.1] Bijectivity

When the matching between a source image and a destination image is expressed by means of a mapping, that mapping shall satisfy the Bijectivity Conditions (BC) between the two images (note that a one-to-one surjective mapping is called a bijection). This is because the respective images should be connected satisfying both surjection and injection, and there is no conceptual supremacy existing between these images. It is to be noted that the mappings to be constructed here are the digital version of the bijection. In the premised technology, a pixel is specified by a co-ordinate point.

The mapping of the source subimage (a subimage of a source image) to the destination subimage (a subimage of a destination image) is represented by f^(m,s):I/2^n−m×I/2^n−m→I/2^n−m×I/2^n−m (s=0, 1, . . . ), where f_(i,j)^(m,s) =(k,l) means that p_(i,j)^(m,s) of the source image is mapped to q_(k,l)^(m,s) of the destination image. For simplicity, when f(i,j)=(k,l) holds, a pixel q_(k,l) is denoted by q_f(i,j).

When the data sets are discrete as image pixels (grid points) treated in the premised technology, the definition of bijectivity is important. Here, the bijection will be defined in the following manner, where i, j, k and l are all integers. First, a square region R defined on the source image plane is consideredp_(i,j)^(m,s)p_(i+1,j)^(m,s)p_(i+1,j+1)^(m,s)p_(i,j+1)^(m,s)  (4)where i=0, . . . , 2^m−1, and j=0, . . . , 2^m−1. The edges of R are directed as follows:{right arrow over (p_(i,j)^(m,s)p_(i+1,j)^(m,s))}{right arrow over (p_(i,j)^(m,s)p_(i+1,j)^(m,s))}{right arrow over (p_(i,j)^(m,s)p_(i+1,j)^(m,s))}{right arrow over (p_(i,j)^(m,s)p_(i+1,j)^(m,s))},{right arrow over (p_(i+1,j)^(m,s)p_(i+1,j+1)^(m,s))}{right arrow over (p_(i+1,j)^(m,s)p_(i+1,j+1)^(m,s))}{right arrow over (p_(i+1,j)^(m,s)p_(i+1,j+1)^(m,s))}{right arrow over (p_(i+1,j)^(m,s)p_(i+1,j+1)^(m,s))}, {right arrow over (p_(i+1,j+1)^(m,s)p_(i,j+1)^(m,s))}{right arrow over (p_(i+1,j+1)^(m,s)p_(i,j+1)^(m,s))}{right arrow over (p_(i+1,j+1)^(m,s)p_(i,j+1)^(m,s))}{right arrow over (p_(i+1,j+1)^(m,s)p_(i,j+1)^(m,s))} and {right arrow over (p_(i,j+1)^(m,s)p_(i,j)^(m,s))}{right arrow over (p_(i,j+1)^(m,s)p_(i,j)^(m,s))}{right arrow over (p_(i,j+1)^(m,s)p_(i,j)^(m,s))}{right arrow over (p_(i,j+1)^(m,s)p_(i,j)^(m,s))}  (5)

This square region R will be mapped by f to a quadrilateral on the destination image plane:q_f(i,j)^(m,s)q_f(i+1,j)^(m,s)q_f(i+1,j+1)^(m,s)q_f(i,j+1)^(m,s)  (6)This mapping f^(m,s) (R), that is,f^(m,s)(R)=f^(m,s)(p_(i,j)^(m,s)p_(i+1,j)^(m,s)p_(i+1,j+1)^(m,s)p_(i,j+1)^(m,s)=q_f(i,j)^(m,s)q_f(i+1,j)^(m,s)q_f(i+1,j+1)^(m,s)q_f(i,j+1)^(m,s))should satisfy the following bijectivity conditions(referred to as BC hereinafter):

• 1. The edges of the quadrilateral f^(m,s)(R) should not intersect one another.
• 2. The orientation of the edges of f^(m,s)(R) should be the same as that of R (clockwise in the case shown in FIG. 2, described below).
• 3. As a relaxed condition, a retraction mapping is allowed.

Without a certain type of a relaxed condition as in, for example, condition 3 above, there would be no mappings which completely satisfy the BC other than a trivial identity mapping. Here, the length of a single edge of f^(m,s) (R) may be zero. Namely, f^(m,s) (R) may be a triangle. However, f^(m,s) (R) is not allowed to be a point or a line segment having area zero. Specifically speaking, if FIG. 2R is the original quadrilateral, FIGS. 2A and 2D satisfy the BC while FIGS. 2B, 2C and 2E do not satisfy the BC.

In actual implementation, the following condition may be further imposed to easily guarantee that the mapping is surjective. Namely, each pixel on the boundary of the source image is mapped to the pixel that occupies the same location at the destination image. In other words, f(i,j)=(i,j) (on the four lines of i=0, i=2^m−1, j=0, j=2^m−1). This condition will be hereinafter referred to as an additional condition.

[1.3.2] Energy of Mapping

[1.3.2.1] Cost Related to the Pixel Intensity

The energy of the mapping f is defined. An objective here is to search a mapping whose energy becomes minimum. The energy is determined mainly by the difference in the intensity between the pixel of the source image and its corresponding pixel of the destination image. Namely, the energy C_(i,j)^(m,s) of the mapping f^(m,s) at(i,j) is determined by the following equation (7).C_(i,j)^(m,s)=|V(p_(i,j)^(m,s))−V(q_(i,j)^(m,s))|²  (7)where V(p_(i,j)^(m,s)) and V(q_f(i,j)^(m,s)) are the intensity values of the pixels p_(i,j)^(m,s) and q_(i,j)^(m,s), respectively. The total energy C^(m,s) of f is a matching evaluation equation, and can be defined as the sum of C_(ij)^(m,s) as shown in the following equation (8)

$\begin{array}{cc}{C}_f^{\left(m,s\right)}=\sum _{i=0}^{i=2^m-1}\sum _{j=0}^{j=2^m-1}{C}_{\left(i,j\right)}^{\left(m,s\right)}& \left(8\right)\end{array}$ [1.3.2.2] Cost Related to the Locations of the Pixel for Smooth Mapping

In order to obtain smooth mappings, another energy D_f for the mapping is introduced. The energy D_f is determined by the locations of p_(i,j)^(m,s) and q_f(i,j)^(m,s) (i=0, 1, . . . , 2^m−1 j=0, 1, . . . , 2^m−1), regardless of the intensity of the pixels. The energy D_(i,j)^(m,s) of the mapping f^(m,s) at a point (i,j) is determined by the following equation (9).D_(i,j)^(m,s)=ηE_0(i,j)^(m,s)+E_1(i,j)^(m,s)  (9)where the coefficient parameter η which is equal to or greater than 0 is a real number. And we haveE_0(i,j)^(m,s)=∥(i,j)−f^(m,s)(i,j)∥²  (10)

$\begin{array}{cc}{E}_{1_{\left(i,j\right)}}^{\left(m,s\right)}=\sum _{i^{\prime }=i-1}^i\sum _{j^{\prime }=j-1}^j{\left(f^{\left(m,s\right)}\left(i,j\right)-\left(i,j\right)\right)-\left(f^{\left(m,s\right)}\left(i^{\prime },j^{\prime }\right)-\left(i^{\prime },j^{\prime }\right)\right)}^2/4& \left(11\right)\end{array}$ where∥(x,y)∥=√{square root over (x²+y²)}  (12)i′ and j′ are integers and f(i′,j′) is defined to be zero for i′<0 and j′<0. E₀ is determined by the distance between (i,j) and f(i,j). E₀ prevents a pixel from being mapped to a pixel too far away from it. However, as explained below, E₀ can be replaced by another energy function. E₁ ensures the smoothness of the mapping. E₁ represents a distance between the displacement of p(i,j) and the displacement of its neighboring points. Based on the above consideration, another evaluation equation for evaluating the matching, or the energy D_f is determined by the following equation:

$\begin{array}{cc}{D}_f^{\left(m,s\right)}=\sum _{i=0}^{i=2^m-1}\sum _{j=0}^{j=2^m-1}{D}_{\left(i,j\right)}^{\left(m,s\right)}& \left(13\right)\end{array}$ [1.3.2.3] Total Energy of the Mapping

The total energy of the mapping, that is, a combined evaluation equation which relates to the combination of a plurality of evaluations, is defined as λC_f^(m,s) +D_f^(m,s), where λ≧0 is a real number. The goal is to detect a state in which the combined evaluation equation has an extreme value, namely, to find a mapping which gives the minimum energy expressed by the following:_f^min{λC_f(m,s)+D_f^(m,s)}  (14)

Care must be exercised in that the mapping becomes an identity mapping if λ=0 and η=0 (i.e., f^(m,s)(i,j)=(i,j) for all i=0, 1, . . . , 2^m−1 and j=0, 1, . . . , 2^m−1). As will be described later, the mapping can be gradually modified or transformed from an identity mapping since the case of λ=0 and η=0 is evaluated at the outset in the premised technology. If the combined evaluation equation is defined as C_f^(m,s)+λD_f^(m,s) where the original position of λ is changed as such, the equation with λ=0 and η=0 will be C_f^(m,s) only. As a result thereof, pixels would randomly matched to each other only because their pixel intensities are close, thus making the mapping totally meaningless. Transforming the mapping based on such a meaningless mapping makes no sense. Thus, the coefficient parameter is so determined that the identity mapping is initially selected for the evaluation as the best mapping.

Similar to this premised technology, differences in the pixel intensity and smoothness are considered in a technique called “optical flow” that is known in the art. However, the optical flow technique cannot be used for image transformation since the optical flow technique takes into account only the local movement of an object. However, global correspondence can also be detected by utilizing the critical point filter according to the premised technology.

[1.3.3] Determining the Mapping with Multiresolution

A mapping f_min which gives the minimum energy and satisfies the BC is searched by using the multiresolution hierarchy. The mapping between the source subimage and the destination subimage at each level of the resolution is computed. Starting from the top of the resolution hierarchy (i.e., the coarsest level), the mapping is determined at each resolution level, and where possible, mappings at other levels are considered. The number of candidate mappings at each level is restricted by using the mappings at an upper (i.e., coarser) level of the hierarchy. More specifically speaking, in the course of determining a mapping at a certain level, the mapping obtained at the coarser level by one is imposed as a sort of constraint condition.

We thus define a parent and child relationship between resolution levels. When the following equation (15) holds,

$\begin{array}{cc}\left(i^{\prime },j^{\prime }\right)=\left(\lfloor \frac{i}{2}\rfloor ,\lfloor \frac{j}{2}\rfloor \right),& \left(15\right)\end{array}$ where └x┘ denotes the largest integer not exceeding x, p_(i′,j′)^(m−1,s) and q_(i′,j′)^(m−1,s) are respectively called the parents of p_(i,j)^(m,s) and q_(i,j)^(m,s). Conversely, p_(i,j)^(m,s) and q_(i,j)^(m,s) are the child of p_(i′,j′)^(m−1,s) and the child of q_(i′,j′)^(m−1,s), respectively. A function parent (i,j) is defined by the following equation (16):

$\begin{array}{cc}\mathrm{parent}\left(i,j\right)=\left(\lfloor \frac{i}{2}\rfloor ,\lfloor \frac{j}{2}\rfloor \right)& \left(16\right)\end{array}$

Now, a mapping between p_(i,j)^(m,s) and q_(k,l)^(m,s) is determined by computing the energy and finding the minimum thereof. The value of f^(m,s)(i,j)=(k,l) is determined as follows using f(m−1,s) (m=1, 2, . . . ,n). First of all, a condition is imposed that q_(k,l)^(m,s) should lie inside a quadrilateral defined by the following definitions (17) and (18). Then, the applicable mappings are narrowed down by selecting ones that are thought to be reasonable or natural among them satisfying the BC.q_{g(m,s)(i−1,j−1)}^(m,s)q_{g(m,s)(i−1,j+1)}^(m,s)q_{g(m,s)(i+1,j+1)}^(m,s)q_{g(m,s)(i+1,j−1)}^(m,s)  (17)whereg^(m−1,s)(i,j)=f^(m−1,s) (parent(i,j))+f^(m−1,s)(parent(i,j)+(1,1))  (18)

The quadrilateral defined above is hereinafter referred to as the inherited quadrilateral of p_(i,j)^(m,s). The pixel minimizing the energy is sought and obtained inside the inherited quadrilateral.

FIG. 3 illustrates the above-described procedures. The pixels A, B, C and D of the source image are mapped to A′, B′, C′ and D′ of the destination image, respectively, at the (m−1)th level in the hierarchy. The pixel p_(i,j)^(m,s) should be mapped to the pixel q_f(m)(i,j)^(m,s) which exists inside the inherited quadrilateral A′B′C′D′. Thereby, bridging from the mapping at the (m−1)th level to the mapping at the m-th level is achieved.

The energy E₀ defined above may now be replaced by the following equations (19) and (20):E_0(i,j)=∥f^(m,0)(i,j)−g^(m)(i,j)∥²  (19)E_0(i,j)=∥f^(m,s)(i,j)−f^(m,s−1)(i,j)∥²,(1≦i)  (20)for computing the submapping f^(m,0) and the submapping f^(m,s) at the m-th level, respectively.

In this manner, a mapping which maintains a low energy of all the submappings is obtained. Using the equation (20) makes the submappings corresponding to the different critical points associated to each other within the same level in order that the subimages can have high similarity. The equation (19) represents the distance between f^(m,s)(i,j) and the location where (i,j) should be mapped when regarded as a part of a pixel at the (m−1)th level.

When there is no pixel satisfying the BC inside the inherited quadrilateral A′B′C′D′, the following steps are taken. First, pixels whose distance from the boundary of A′B′C′D′ is L (at first, L=1) are examined. If a pixel whose energy is the minimum among them satisfies the BC, then this pixel will be selected as a value of f^(m,s)(i,j). L is increased until such a pixel is found or L reaches its upper bound L_max^(m).L_max^(m) is fixed for each level m. If no pixel is found at all, the third condition of the BC is ignored temporarily and such mappings that caused the area of the transformed quadrilateral to become zero (a point or a line) will be permitted so as to determine f^(m,s)(i,j). If such a pixel is still not found, then the first and the second conditions of the BC will be removed.

Multiresolution approximation is essential to determining the global correspondence of the images while preventing the mapping from being affected by small details of the images. Without the multiresolution approximation, it is impossible to detect a correspondence between pixels whose distances are large. In the case where the multiresolution approximation is not available, the size of an image will generally be limited to a very small size, and only tiny changes in the images can be handled. Moreover, imposing smoothness on the mapping usually makes it difficult to find the correspondence of such pixels. That is because the energy of the mapping from one pixel to another pixel which is far therefrom is high. On the other hand, the multiresolution approximation enables finding the approximate correspondence of such pixels. This is because the distance between the pixels is small at the upper (coarser) level of the hierarchy of the resolution.

[1.4] Automatic Determination of the Optimal Parameter Values

One of the main deficiencies of the existing image matching techniques lies in the difficulty of parameter adjustment. In most cases, the parameter adjustment is performed manually and it is extremely difficult to select the optimal value. However, according to the premised technology, the optimal parameter values can be obtained completely automatically.

The systems according to this premised technology include two parameters, namely, λ and η, where λ and η represent the weight of the difference of the pixel intensity and the stiffness of the mapping, respectively. In order to automatically determine these parameters, the are initially set to 0. First, λ is gradually increased from λ=0 while η is fixed at 0. As λ becomes larger and the value of the combined evaluation equation (equation (14)) is minimized, the value of C_f^(m,s) for each submapping generally becomes smaller. This basically means that the two images are matched better. However, if λ exceeds the optimal value, the following phenomena occur:

• 1. Pixels which should not be corresponded are erroneously corresponded only because their intensities are close.
• 2. As a result, correspondence between images becomes inaccurate, and the mapping becomes invalid.
• 3. As a result, D_f^(m,s) in equation (14) tends to increase abruptly.
• 4. As a result, since the value of equation (14) tends to increase abruptly, f^(m,s) changes in order to suppress the abrupt increase of D_f^(m,s). As a result, C_f^(m,s) increases.

Therefore, a threshold value at which C_f^(m,s) turns to an increase from a decrease is detected while a state in which equation (14) takes the minimum value with λ being increased is kept. Such λ is determined as the optimal value at η=0. Next, the behavior of C_f^(m,s) is examined while η is increased gradually, and η will be automatically determined by a method described later. λ will then again be determined corresponding to such an automatically determined η.

The above-described method resembles the focusing mechanism of human visual systems. In the human visual systems, the images of the respective right eye and left eye are matched while moving one eye. When the objects are clearly recognized, the moving eye is fixed.

[1.4.1] Dynamic Determination of λ

Initially, λ is increased from 0 at a certain interval, and a subimage is evaluated each time the value of λ changes. As shown in equation (14), the total energy is defined by λC_f^(m,s)+D_f^(m,s). D_(i,j)^(m,s) in equation (9) represents the smoothness and theoretically becomes minimum when it is the identity mapping. E₀ and E₁ increase as the mapping is further distorted. Since E₁ is an integer, 1 is the smallest step of D_f^(m,s). Thus, it is impossible to change the mapping to reduce the total energy unless a changed amount (reduction amount) of the current λC_(i,j)^(m,s) is equal to or greater than 1. Since D_f^(m,s) increases by more than 1 accompanied by the change of the mapping, the total energy is not reduced unless λC_(i,j)^(m,s) is reduced by more than 1.

Under this condition, it is shown that C_(i,j)^(m,s) decreases in normal cases as λ increases. The histogram of C_(i,j)^(m,s) is denoted as h(l), where h(l) is the number of pixels whose energy C_(i,j)^(m,s) is l². In order that λl²≧1 for example, the case of l²=1/λ is considered. When λ varies from λ₁ to λ₂, a number of pixels (denoted A) expressed by the following equation (21):

$\begin{array}{cc}A=\sum _{l=\lceil \frac{1}{{\lambda }_2}\rceil }^{\lfloor \frac{1}{{\lambda }_1}\rfloor }h\left(l\right)\cong {\int }_{l=\frac{1}{{\lambda }_2}}^{\frac{1}{{\lambda }_1}}h\left(l\right)dl=-{\int }_{{\lambda }_2}^{{\lambda }_1}h\left(l\right)\frac{1}{{\lambda }^{3/2}}d\lambda ={\int }_{{\lambda }_1}^{{\lambda }_2}\frac{h\left(l\right)}{{\lambda }^{3/2}}d\lambda & \left(21\right)\end{array}$ changes to a more stable state having the energy shown in equation(22):

$\begin{array}{cc}{C}_f^{\left(m,s\right)}-l^2=C_f^{\left(m,s\right)}-\frac{1}{\lambda }.& \left(22\right)\end{array}$

Here, it is assumed that the energy of these pixels is approximated to be zero. This means that the value of C_(i,j)^(m,s) changes by:

$\begin{array}{cc}\partial C_f^{\left(m,s\right)}=-\frac{A}{\lambda }& \left(23\right)\end{array}$ As a result, equation (24) holds.

$\begin{array}{cc}\frac{\partial C_f^{\left(m,s\right)}}{\partial \lambda }=-\frac{h\left(l\right)}{{\lambda }^{5/2}}& \left(24\right)\end{array}$ Since h(l)>0, C_f^(m,s) decreases in the normal case. However, when λ exceeds the optimal value, the above phenomenon, that is, an increase in C_f^(m,s) occurs. The optimal value of λ is determined by detecting this phenomenon.

When

$\begin{array}{cc}h\left(l\right)={\mathrm{Hl}}^k=\frac{H}{{\lambda }^{k/2}}& \left(25\right)\end{array}$ is assumed, where both H(H>0) and k are constants, the equation (26) holds:

$\begin{array}{cc}\frac{\partial C_f^{\left(m,s\right)}}{\partial \lambda }=-\frac{H}{{\lambda }^{5/2+k/2}}& \left(26\right)\end{array}$ Then, if k≠−3, the following equation (27) holds:

$\begin{array}{cc}{C}_f^{\left(m,s\right)}=C+\frac{H}{\left(3/2+k/2\right){\lambda }^{3/2+k/2}}& \left(27\right)\end{array}$ The equation (27) is a general equation of C_f^(m,s) (where C is a constant).

When detecting the optimal value of λ, the number of pixels violating the BC may be examined for safety. In the course of determining a mapping for each pixel, the probability of violating the BC is assumed as a value p₀ here.

In this case, since

$\begin{array}{cc}\frac{\partial A}{\partial \lambda }=\frac{h\left(l\right)}{{\lambda }^{3/2}}& \left(28\right)\end{array}$ holds, the number of pixels violating the BC increases at a rate of:

$\begin{array}{cc}{B}_0=\frac{h\left(l\right)p_0}{{\lambda }^{3/2}}& \left(29\right)\end{array}$ Thus,

$\begin{array}{cc}\frac{B_0{\lambda }^{3/2}}{p_{0}h\left(l\right)}=1& \left(30\right)\end{array}$ is a constant. If it is assumed that h(l)=Hl^k, the following equation (31), for example,B₀λ^3/2+k/2=p₀H  (31)becomes a constant. However, when λ exceeds the optimal value, the above value of equation (31) increases abruptly. By detecting this phenomenon, i.e. whether or not the value of B₀λ^3/2+k/22^m exceeds an abnormal value B_0thres, the optimal value of λ can be determined. Similarly, whether or not the value of B₁λ^3/2+k/22^m exceeds an abnormal value B_1thres, can be used to check for an increasing rate B₁ of pixels violating the third condition of the BC. The reason why the factor 2^m is introduced here will be described at a later stage. This system is not sensitive to the two threshold values B_0thres and B_1thres. The two threshold values B_0thres and B_1thres can be used to detect excessive distortion of the mapping which may not be detected through observation of the energy C_f^(m,s).

In the experimentation, when λ exceeded 0.1 the computation of f^(m,s) was stopped and the computation of f^(m,s+1) was started. That is because the computation of submappings is affected by a difference of only 3 out of 255 levels in pixel intensity when λ>0.1 and it is then difficult to obtain a correct result.

[1.4.2] Histogram h(l)

The examination of C_f^(m,s) does not depend on the histogram h(l), however, the examination of the BC and its third condition may be affected by h(l). When (λ, C_f^(m,s)) is actually plotted, k is usually close to 1. In the experiment, k=1 is used, that is, B₀λ² and B₁λ² are examined. If the true value of k is less than 1, B₀λ² and B₁λ² are not constants and increase gradually by a factor of λ^(1−k)/2. If h(l) is a constant, the factor is, for example, λ^1/2. However, such a difference can be absorbed by setting the threshold B_0thres appropriately.

Let us model the source image by a circular object, with its center at (x₀,y₀) and its radius r, given by:

$\begin{array}{cc}p\left(i,j\right)=\{\begin{array}{c}\frac{255}{r}c\left(\sqrt{{\left(i-x_0\right)}^2+{\left(j-y_0\right)}^2}\right)\dots \left(\sqrt{{\left(i-x_0\right)}^2+{\left(j-y_0\right)}^2}\le r\right)\\ 0\dots \left(\mathrm{otherwise}\right)\end{array}& \left(32\right)\end{array}$ and the destination image given by:

$\begin{array}{cc}q\left(i,j\right)=\{\begin{array}{c}\frac{255}{r}c\left(\sqrt{{\left(i-x_1\right)}^2+{\left(j-y_1\right)}^2}\right)\dots \left(\sqrt{{\left(i-x_1\right)}^2+{\left(j-y_1\right)}^2}\le r\right)\\ 0\dots \left(\mathrm{otherwise}\right)\end{array}& \left(33\right)\end{array}$ with its center at (x₁,y₁) and radius r. In the above, let c(x) have the form of c(x)=x^k. When the centers (x₀,y₀) and (x₁,y₁) are sufficiently far from each other, the histogram h(l) is then in the form:h(l)∝rl^k(k≠0)  (34)

When k=1, the images represent objects with clear boundaries embedded in the background. These objects become darker toward their centers and brighter toward their boundaries. When k=−1, the images represent objects with vague boundaries. These objects are brightest at their centers, and become darker toward their boundaries. Without much loss of generality, it suffices to state that objects in images are generally between these two types of objects. Thus, choosing k such that −1≦k≦1 can cover most cases and the equation (27) is generally a decreasing function for this range.

As can be observed from the above equation (34), attention must be directed to the fact that r is influenced by the resolution of the image, that is, r is proportional to 2^m. This is the reason for the factor 2^m being introduced in the above section [1.4.1].

[1.4.3] Dynamic Determination of η

The parameter η can also be automatically determined in a similar manner. Initially, η is set to zero, and the final mapping f⁽ⁿ⁾ and the energy C_f⁽ⁿ⁾ at the finest resolution are computed. Then, after η is increased by a certain value Δη, the final mapping f⁽ⁿ⁾ and the energy C_f⁽ⁿ⁾ at the finest resolution are again computed. This process is repeated until the optimal value of η is obtained. η represents the stiffness of the mapping because it is a weight of the following equation (35):E_0(i,j)^(m,s)=∥f^(m,s)(i,j)−f^(m,s−1)(i,j)∥²  (35)

If η is zero, D_f⁽ⁿ⁾ is determined irrespective of the previous submapping, and the present submapping may be elastically deformed and become too distorted. On the other hand, if η is a very large value, D_f⁽ⁿ⁾ is almost completely determined by the immediately previous submapping. The submappings are then very stiff, and the pixels are mapped to almost the same locations. The resulting mapping is therefore the identity mapping. When the value of η increases from 0, C_f⁽ⁿ⁾ gradually decreases as will be described later. However, when the value of η exceeds the optimal value, the energy starts increasing as shown in FIG. 4. In FIG. 4, the x-axis represents η, and y-axis represents C_f.

The optimum value of η which minimizes C_f⁽ⁿ⁾ can be obtained in this manner. However, since various elements affect this computation as compared to the case of λ, C_f⁽ⁿ⁾ changes while slightly fluctuating. This difference is caused because a submapping is re-computed once in the case of λ whenever an input changes slightly, whereas all the submappings must be re-computed in the case of η. Thus, whether the obtained value of C_f⁽ⁿ⁾ is the minimum or not cannot be determined as easily. When candidates for the minimum value are found, the true minimum needs to be searched by setting up further finer intervals.

[1.5] Supersampling

When deciding the correspondence between the pixels, the range of f^(mu,s) can be expanded to R×R (R being the set of real numbers) in order to increase the degree of freedom. In this case, the intensity of the pixels of the destination image is interpolated, to provide f^(m,s) having an intensity at non-integer points:V(q_f(m,s)(i,j)^(m,s))  (36)That is, supersampling is performed. In an example implementation, f^(m,s) may take integer and half integer values, andV(q_{(i,j)+(0.5,0.5)}^(m,s))  (37)is given by(V(q_(i,j)^(m,s))+V(q_(i,j)+(1,1)^(m,s)))/2  (38)[1.6] Normalization of the Pixel Intensity of Each Image

When the source and destination images contain quite different objects, the raw pixel intensity may not be used to compute the mapping because a large difference in the pixel intensity causes excessively large energy C_f^(m,s) and thus making it difficult to obtain an accurate evaluation.

For example, a matching between a human face and a cat's face is computed as shown in FIGS. 20(a) and 20(b). The cat's face is covered with hair and is a mixture of very bright pixels and very dark pixels. In this case, in order to compute the submappings of the two faces, subimages are normalized. That is, the darkest pixel intensity is set to 0 while the brightest pixel intensity is set to 255, and other pixel intensity values are obtained using linear interpolation.

[1.7] Implementation

In an example implementation, a heuristic method is utilized wherein the computation proceeds linearly as the source image is scanned. First, the value of f^(m,s) is determined at the top leftmost pixel (i,j)=(0,0). The value of each f^(m,s)(i,j) is then determined while i is increased by one at each step. When i reaches the width of the image, j is increased by one and i is reset to zero. Thereafter, f^(m,s)(i,j) is determined while scanning the source image. Once pixel correspondence is determined for all the points, it means that a single mapping f^(m,s) is determined.

When a corresponding point q_f(i,j) is determined for p_(i,j), a corresponding point q_f(i,j+1) of p_(i,j+1) is determined next. The position of q_f(i,j+1) is constrained by the position of q_f(i,j) since the position of q_f(i,j+1) satisfies the BC. Thus, in this system, a point whose corresponding point is determined earlier is given higher priority. If the situation continues in which (0,0) is always given the highest priority, the final mapping might be unnecessarily biased. In order to avoid this bias, f^(m,s) is determined in the following manner in the premised technology.

First, when (s mod 4) is 0, f^(m,s) is determined starting from (0,0) while gradually increasing both i and j. When (s mod 4) is 1, f^(m,s) is determined starting from the top rightmost location while decreasing i and increasing j. When (s mod 4) is 2, f^(m,s) is determined starting from the bottom rightmost location while decreasing both i and j. When (s mod 4) is 3, f^(m,s) is determined starting from the bottom leftmost location while increasing i and decreasing j. Since a concept such as the submapping, that is, a parameter s, does not exist in the finest n-th level, f^(m,s) is computed continuously in two directions on the assumption that s=0 and s=2.

In this implementation, the values of f^(m,s)(i,j) (m=0, . . . , n) that satisfy the BC are chosen as much as possible from the candidates (k,l) by imposing a penalty on the candidates violating the BC. The energy D_(k,l) of a candidate that violates the third condition of the BC is multiplied by φ and that of a candidate that violates the first or second condition of the BC is multiplied by ψ. In this implementation, φ=2 and ψ=100000 are used.

In order to check the above-mentioned BC, the following test may be performed as the procedure when determining (k,l)=f^(m,s)(i,j) Namely, for each grid point (k,l) in the inherited quadrilateral of f^(m,s)(i,j), whether or not the z-component of the outer product ofW={right arrow over (A)}×{right arrow over (B)}  (39)is equal to or greater than 0 is examined, where

$\begin{array}{cc}\overrightarrow{A}=\overrightarrow{q_{f^{\left(m,s\right)}\left(i,j-1\right)}^{\left(m,s\right)}{q}_{f^{\left(m,s\right)}\left(i+1,j-1\right)}^{\left(m,s\right)}}& \left(40\right)\\ \overrightarrow{B}=\overrightarrow{q_{f^{\left(m,s\right)}\left(i,j-1\right)}^{\left(m,s\right)}{q}_{\left(k,l\right)}^{\left(m,s\right)}}& \left(41\right)\end{array}$ Here, the vectors are regarded as 3D vectors and the z-axis is defined in the orthogonal right-hand coordinate system. When W is negative, the candidate is imposed with a penalty by multiplying D_(k,l)^(m,s) by ψ so that it is not as likely to be selected.

FIGS. 5( a) and 5(b) illustrate the reason why this condition is inspected. FIG. 5(a) shows a candidate without a penalty and FIG. 5(b) shows one with a penalty. When determining the mapping f^(m,s)(i,j+1) for the adjacent pixel at (i,j+1), there is no pixel on the source image plane that satisfies the BC if the z-component of W is negative because then q_(k,l)^(m,s) passes the boundary of the adjacent quadrilateral.

[1.7.1] The order of Submappings

In this implementation, σ(0)=0, σ(1) =1, σ(2)=2, σ(3)=3, σ(4)=0 are used when the resolution level is even, while σ(0)=3, σ(1)=2, σ(2)=1, σ(3)=0, σ(4)=3 are used when the resolution level is odd. Thus, the submappings are shuffled to some extent. It is to be noted that the submappings are primarily of four types, and s may be any of 0 to 3. However, a processing with s=4 is used in this implementation for a reason to be described later.

[1.8] Interpolations

After the mapping between the source and destination images is determined, the intensity values of the corresponding pixels are interpolated. In the implementation, trilinear interpolation is used. Suppose that a square p_(i,j)p_(i+1,j)p_(i+1,j+1)p_(i,j+1) on the source image plane is mapped to a quadrilateral q_f(i,j)q_f(i+1,j)q_f(i+1,j+1)q_f(i,j+1) on the destination image plane. For simplicity, the distance between the image planes is assumed to be 1. The intermediate image pixels r(x,y,t) (0≦x≦N−1, 0≦y≦M−1) whose distance from the source image plane is t (0≦t≦1) are obtained as follows. First, the location of the pixel r(x,y,t), where x,y,tεR, is determined by equation (42):

$\begin{array}{cc}\left(x,y\right)=\left(1-dx\right)\left(1-dy\right)\left(1-t\right)\left(i,j\right)+\left(1-dx\right)\left(1-dy\right)tf\left(i,j\right)+dx\left(1-dy\right)\left(1-t\right)\left(i+1,j\right)+dx\left(1-dy\right)tf\left(i+1,j\right)+\left(1-dx\right)dy\left(1-t\right)\left(i,j+1\right)+\left(1-dx\right)dy\mathrm{tf}\left(i,j+1\right)+dxdy\left(1-t\right)\left(i+1,j+1\right)+dxdytf\left(i+1,j+1\right)& \left(42\right)\end{array}$ The value of the pixel intensity at r(x,y,t) is then determined by equation (43):

$\begin{array}{cc}V\left(r\left(x,y,t\right)\right)=\left(1-dx\right)\left(1-dy\right)\left(1-t\right)V\left(p_{\left(i,j\right)}\right)+\left(1-dx\right)\left(1-dy\right)tV\left(q_{f\left(i,j\right)}\right)+dx\left(1-dy\right)\left(1-t\right)V\left(p_{\left(i+1,j\right)}\right)+dx\left(1-dy\right)tV\left(q_{f\left(i+1,j\right)}\right)+\left(1-dx\right)dy\left(1-t\right)V\left(p_{\left(i,j+1\right)}\right)+\left(1-dx\right)dytV\left(q_{f\left(i,j+1\right)}\right)+dxdy\left(1-t\right)V\left(p_{\left(i+1,j+1\right)}\right)+dxdytV\left(q_{f\left(i+1,j+1\right)}\right)& \left(43\right)\end{array}$ where dx and dy are parameters varying from 0 to 1.[1.9] Mapping to which Constraints are Imposed

So far, the determination of a mapping in which no constraints are imposed has been described. However, if a correspondence between particular pixels of the source and destination images is provided in a predetermined manner, the mapping can be determined using such correspondence as a constraint.

The basic idea is that the source image is roughly deformed by an approximate mapping which maps the specified pixels of the source image to the specified pixels of the destination image and thereafter a mapping f is accurately computed.

First, the specified pixels of the source image are mapped to the specified pixels of the destination image, then the approximate mapping that maps other pixels of the source image to appropriate locations are determined. In other words, the mapping is such that pixels in the vicinity of a specified pixel are mapped to locations near the position to which the specified one is mapped. Here, the approximate mapping at the m-th level in the resolution hierarchy is denoted by F^(m).

The approximate mapping F is determined in the following manner. First, the mappings for several pixels are specified. When n_s pixelsp(i₀,j₀),p(i₁,j₁), . . . , p(i_ns−1,j_ns−1)  (44)of the source image are specified, the following values in the equation (45) are determined.F⁽ⁿ⁾(i₀,j₀)=(k₀,l₀),F⁽ⁿ⁾(i₁,j₁)=(k₁,l₁), . . . ,F⁽ⁿ⁾(i_ns−1,j_ns−1)=(k_ns−1,l_ns−1)  (45)

For the remaining pixels of the source image, the amount of displacement is the weighted average of the displacement of p(i_h,j_h) (h=0, . . . , n_s−1). Namely, a pixel p_(i,j) is mapped to the following pixel (expressed by the equation (46)) of the destination image.

$\begin{array}{cc}{F}^{\left(m\right)}\left(i,j\right)=\frac{\left(i,j\right)+\sum _{h=0}^{h=n_s-1}\left(k_h-i_h,l_h-j_h\right)weigh{t}_h\left(i,j\right)}{2^{n-m}}\mathrm{where}& \left(46\right)\\ weigh{t}_h\left(i,j\right)=\frac{1/{\left(i_h-i,j_h-j\right)}^2}{\mathrm{total\_weight}\left(i,j\right)}\mathrm{where}& \left(47\right)\\ \mathrm{total\_weight}\left(i,j\right)=\sum _{h=0}^{h=n_s-1}1/{\left(i_h-i,j_h-j\right)}^2& \left(48\right)\end{array}$

Second, the energy D_(i,j)^(m,s) of the candidate mapping f is changed so that a mapping f similar to F^(m) has a lower energy. Precisely speaking, D_(i,j)^(m,s) is expressed by the equation (49):D_(i,j)^(m,s)=E_0(i,j)^(m,s)+ηE_1(i,j)^(m,s)+κE_2(i,j)^(m,s)  (49)where

$\begin{array}{cc}{E}_{2_{\left(i,j\right)}}^{\left(m,s\right)}=\{\begin{array}{cc}0,& \mathrm{if}{F^{\left(m\right)}\left(i,j\right)-f^{\left(m,s\right)}\left(i,j\right)}^2\le \lfloor \frac{{\rho }^2}{2^{2\left(n-m\right)}}\rfloor \\ {F^{\left(m\right)}\left(i,j\right)-f^{\left(m,s\right)}\left(i,j\right)}^2,& \mathrm{otherwise}\end{array}& \left(50\right)\end{array}$ where κ, ρ≧0. Finally, the resulting mapping f is determined by the above-described automatic computing process.

Note that E_2(i,j)^(m,s) becomes 0 if f^(m,s)(i,j) is sufficiently close to F^(m)(i,j) i.e., the distance therebetween is equal to or less than

$\begin{array}{cc}\lfloor \frac{{\rho }^2}{2^{2\left(n-m\right)}}\rfloor & \left(51\right)\end{array}$ This has been defined in this way because it is desirable to determine each value f^(m,s)(i,j) automatically to fit in an appropriate place in the destination image as long as each value f^(m's)(i,j) is close to F^(m)(i,j). For this reason, there is no need to specify the precise correspondence in detail to have the source image automatically mapped so that the source image matches the destination image.[2] Concrete Processing Procedure

The flow of a process utilizing the respective elemental techniques described in [1] will now be described.

FIG. 6 is a flowchart of the overall procedure of the premised technology. Referring to FIG. 6, a source image and destination image are first processed using a multiresolutional critical point filter (S1). The source image and the destination image are then matched (S2). As will be understood, the matching (S2) is not required in every case, and other processing such as image recognition may be performed instead, based on the characteristics of the source image obtained at S1.

FIG. 7 is a flowchart showing details of the process SI shown in FIG. 6. This process is performed on the assumption that a source image and a destination image are matched at S2. Thus, a source image is first hierarchized using a critical point filter (S10) so as to obtain a series of source hierarchical images. Then, a destination image is hierarchized in the similar manner (S11) so as to obtain a series of destination hierarchical images. The order of S10 and S11 in the flow is arbitrary, and the source image and the destination image can be generated in parallel. It may also be possible to process a number of source and destination images as required by subsequent processes.

FIG. 8 is a flowchart showing details of the process at S10 shown in FIG. 7. Suppose that the size of the original source image is 2ⁿ×2ⁿ. Since source hierarchical images are sequentially generated from an image with a finer resolution to one with a coarser resolution, the parameter m which indicates the level of resolution to be processed is set to n (S100). Then, critical points are detected from the images p^(m,0), p^(n,1), p^(m,2) and p^(m,3) of the m-th level of resolution, using a critical point filter (S101), so that the images p^(m−1,0), p^(m−1,1), p^(m−1,2) and p^(m−1,3) of the (m−1)th level are generated (S102). Since m=n here, p^(m,0)=p^(m,1)=p^(m,2)=p^(m,3)=p⁽ⁿ⁾ holds and four types of subimages are thus generated from a single source image.

FIG. 9 shows correspondence between partial images of the m-th and those of (m−1)th levels of resolution. Referring to FIG. 9, respective numberic values shown in the figure represent the intensity of respective pixels. p^(m,s) symbolizes any one of four images p^(m,0) through p^(m,3), and when generating p^(m−1,0), p^(m,0) is used from p^(m,s). For example, as for the block shown in FIG. 9, comprising four pixels with their pixel intensity values indicated inside, images p^(m−1,0), p^(m−1,1), p^(m−1,2) and p^(m−1,3) acquire “3”, “8”, “6” and “10”, respectively, according to the rules described in [1.2]. This block at the m-th level is replaced at the (m−1)th level by respective single pixels thus acquired. Therefore, the size of the subimages at the (m−1)th level is 2^m−1×2^m−1.

After m is decremented (S103 in FIG. 8), it is ensured that m is not negative (S104). Thereafter, the process returns to S101, so that subimages of the next level of resolution, i.e., a next coarser level, are generated. The above process is repeated until subimages at m=0 (0-th level) are generated to complete the process at S10. The size of the subimages at the 0-th level is 1×1.

FIG. 10 shows source hierarchical images generated at S10 in the case of n=3. The initial source image is the only image common to the four series followed. The four types of subimages are generated independently, depending on the type of critical point. Note that the process in FIG. 8 is common to S11 shown in FIG. 7, and that destination hierarchical images are generated through a similar procedure. Then, the process at S1 in FIG. 6 is completed.

In this premised technology, in order to proceed to S2 shown in FIG. 6a matching evaluation is prepared. FIG. 11 shows the preparation procedure. Referring to FIG. 11, a plurality of evaluation equations are set (S30). The evaluation equations may include the energy C_f^(m,s) concerning a pixel value, introduced in [1.3.2.1], and the energy D_f^(m,s) concerning the smoothness of the mapping introduced in [1.3.2.2]. Next, by combining these evaluation equations, a combined evaluation equation is set (S31). Such a combined evaluation equation may be λC_(i,j)^(m,s)+D_f^(m,s). Using η introduced in [1.3.2.2], we have

$\begin{array}{cc}\sum \sum (\lambda C_{\left(i,j\right)}^{\left(m,s\right)}+\eta E_{0_{\left(i,j\right)}}^{\left(m,s\right)}+E_{1_{\left(i,j\right)}}^{\left(m,s\right)}& \left(52\right)\end{array}$ In the equation (52) the sum is taken for each i and j where i and j run through 0, 1, . . . , 2^m−1. Now, the preparation for matching evaluation is completed.

FIG. 12 is a flowchart showing the details of the process of S2 shown in FIG. 6. As described in [1], the source hierarchical images and destination hierarchical images are matched between images having the same level of resolution. In order to detect global correspondence correctly, a matching is calculated in sequence from a coarse level to a fine level of resolution. Since the source and destination hierarchical images are generated using the critical point filter, the location and intensity of critical points are stored clearly even at a coarse level. Thus, the result of the global matching is superior to conventional methods.

Referring to FIG. 12, a coefficient parameter η and a level parameter m are set to 0 (S20). Then, a matching is computed between the four subimages at the m-th level of the source hierarchical images and those of the destination hierarchical images at the m-th level, so that four types of submappings f^(m,s) (s=0, 1, 2, 3) which satisfy the BC and minimize the energy are obtained (S21). The BC is checked by using the inherited quadrilateral described in [1.3.3]. In that case, the submappings at the m-th level are constrained by those at the (m−1)th level, as indicated by the equations (17) and (18). Thus, the matching computed at a coarser level of resolution is used in subsequent calculation of a matching. This is called a vertical reference between different levels. If m=0, there is no coarser level and this exceptional case will be described using FIG. 13.

A horizontal reference within the same level is also performed. As indicated by the equation (20) in [1.3.3], f^(m,3), f^(m,2) and f^(m,1) are respectively determined so as to be analogous to f^(m,2), f^(m,1) and f^(m,0). This is because a situation in which the submappings are totally different seems unnatural even though the type of critical points differs so long as the critical points are originally included in the same source and destination images. As can been seen from the equation (20), the closer the submappings are to each other, the smaller the energy becomes, so that the matching is then considered more satisfactory.

As for f^(m,0), which is to be initially determined, a coarser level by one may be referred to since there is no other submapping at the same level to be referred to as shown in the equation (19). In this premised technology, however, a procedure is adopted such that after the submappings were obtained up to f^(m,3), f^(m,0) is recalculated once utilizing the thus obtained subamppings as a constraint. This procedure is equivalent to a process in which s=4 is substituted into the equation (20) and f^(m,4) is set to f^(m,0) anew. The above process is employed to avoid the tendency in which the degree of association between f^(m,0) and f^(m,3) becomes too low. This scheme actually produced a preferable result. In addition to this scheme, the submappings are shuffled in the experiment as described in [1.7.1], so as to closely maintain the degrees of association among submappings which are originally determined independently for each type of critical point. Furthermore, in order to prevent the tendency of being dependent on the starting point in the process, the location thereof is changed according to the value of s as described in [1.7].

FIG. 13 illustrates how the submapping is determined at the 0-th level. Since at the 0-th level each sub-image is consitituted by a single pixel, the four submappings f^(0,s) are automatically chosen as the identity mapping. FIG. 14 shows how the submappings are determined at the first level. At the first level, each of the sub-images is constituted of four pixels, which are indicated by solid lines. When a corresponding point (pixel) of the point (pixel) x in p^(1,s) is searched within q ^(1,s), the following procedure is adopted:

• 1. An upper left point a, an upper right point b, a lower left point c and a lower right point d with respect to the point x are obtained at the first level of resolution.
• 2. Pixels to which the points a to d belong at a coarser level by one, i.e., the 0-th level, are searched. In FIG. 14, the points a to d belong to the pixels A to D, respectively. However, the pixels A to C are virtual pixels which do not exist in reality.
• 3. The corresponding points A′ to D′ of the pixels A to D, which have already been defined at the 0-th level, are plotted in q^(1,s). The pixels A′ to C′ are virtual pixels and regarded to be located at the same positions as the pixels A to C.
• 4. The corresponding point a′ to the point a in the pixel A is regarded as being located inside the pixel A′, and the point a′ is plotted. Then, it is assumed that the position occupied by the point a in the pixel A (in this case, positioned at the lower right) is the same as the position occupied by the point a′ in the pixel A′.
• 5. The corresponding points b′ to d′ are plotted by using the same method as the above 4 so as to produce an inherited quadrilateral defined by the points a′ to d′.
• 6. The corresponding point x′ of the point x is searched such that the energy becomes minimum in the inherited quadrilateral. Candidate corresponding points x′ may be limited to the pixels, for instance, whose centers are included in the inherited quadrilateral. In the case shown in FIG. 14, the four pixels all become candidates.

The above described is a procedure for determining the corresponding point of a given point x. The same processing is performed on all other points so as to determine the submappings. As the inherited quadrilateral is expected to become deformed at the upper levels (higher than the second level), the pixels A′ to D′ will be positioned apart from one another as shown in FIG. 3.

Once the four submappings at the m-th level are determined in this manner, m is incremented (S22 in FIG. 12). Then, when it is confirmed that m does not exceed n (S23), return to S21. Thereafter, every time the process returns to S21, submappings at a finer level of resolution are obtained until the process finally returns to S21 at which time the mapping f⁽ⁿ⁾ at the n-th level is determined. This mapping is denoted as f⁽ⁿ⁾(η=0) because it has been determined relative to η=0.

Next, to obtain the mapping with respect to other different η, η is shifted by Δη and m is reset to zero (S24). After confirming that new η does not exceed a predetermined search-stop value η_max (S25), the process returns to S21 and the mapping f⁽ⁿ⁾(η=Δη) relative to the new η is obtained. This process is repeated while obtaining f⁽ⁿ⁾(η=iΔη) (i=0, 1, . . . ) at S21. When η exceeds η_max, the process proceeds to S26 and the optimal η=η_opt is determined using a method described later, so as to let η⁽ⁿ⁾(η=η_opt) be the final mapping f⁽ⁿ⁾.

FIG. 15 is a flowchart showing the details of the process of S21 shown in FIG. 12. According to this flowchart, the submappings at the m-th level are determined for a certain predetermined η. In this premised technology, when determining the mappings, the optimal λ is defined independently for each submapping.

Referring to FIG. 15, s and λ are first reset to zero (S210). Then, obtained is the submapping f^(m,s) that minimizes the energy with respect to the then λ (and, implicitly, η) (S211), and the thus obtained submapping is denoted as f^(m,s)(λ=0). In order to obtain the mapping with respect to other different λ, λ is shifted by Δλ. After confirming that the new λ does not exceed a predetermined search-stop value λ_max (S213), the process returns to S211 and the mapping f^(m,s)(λ=Δλ) relative to the new λ is obtained. This process is repeated while obtaining f^(m,s)(λ=iΔλ)(i=0, 1, . . . ). When λ exceeds λ_max, the process proceeds to S214 and the optimal λ=λ_opt is determined, so as to let f⁽ⁿ⁾ (λ=λ_opt) be the final mapping f^(m,s) (S214).

Next, in order to obtain other submappings at the same level, λ is reset to zero and s is incremented (S215). After confirming that s does not exceed 4 (S216), return to S211. When s=4, f^(m,0) is renewed utilizing f^(m,3) as described above and a submapping at that level is determined.

FIG. 16 shows the behavior of the energy C_f^(m,s) corresponding to f^(m,s)(λ=iΔλ)(i=0, 1, . . . ) for a certain m and s while varying λ. As described in [1.4], as λ increases, C_f^(m,s) normally decreases but changes to increase after λ exceeds the optimal value. In this premised technology, λ in which C_f^(m,s) becomes the minima is defined as λ_opt. As observed in FIG. 16, even if C_f^(m,s) begins to decrease again in the range λ>λ_opt, the mapping will not be as good. For this reason, it suffices to pay attention to the first occurring minima value. In this premised technology, λ_opt is independently determined for each submapping including f⁽ⁿ⁾.

FIG. 17 shows the behavior of the energy C_f^(m,s) corresponding to f⁽ⁿ⁾(η=iΔη)(i=0, 1, . . . ) while varying η. Here too, C_f⁽ⁿ⁾ normally decreases as η increases, but C_f⁽ⁿ⁾ changes to increase after n exceeds the optimal value. Thus, η in which C_f⁽ⁿ⁾ becomes the minima is defined as η_opt. FIG. 17 can be considered as an enlarged graph around zero along the horizontal axis shown in FIG. 4. Once η_opt is determined, f⁽ⁿ⁾ can be finally determined.

As described above, this premised technology provides various merits. First, since there is no need to detect edges, problems in connection with the conventional techniques of the edge detection type are solved. Furthermore, prior knowledge about objects included in an image is not necessitated, thus automatic detection of corresponding points is achieved. Using the critical point filter, it is possible to preserve intensity and locations of critical points even at a coarse level of resolution, thus being extremely advantageous when applied to object recognition, characteristic extraction, and image matching. As a result, it is possible to construct an image processing system which significantly reduces manual labor.

Some further extensions to or modifications of the above-described premised technology may be made as follows:

• (1) Parameters are automatically determined when the matching is computed between the source and destination hierarchical images in the premised technology. This method can be applied not only to the calculation of the matching between the hierarchical images but also to computing the matching between two images in general.

For instance, an energy E₀ relative to a difference in the intensity of pixels and an energy E₁ relative to a positional displacement of pixels between two images may be used as evaluation equations, and a linear sum of these equations, i.e., E_tot=αE₀+E₁, may be used as a combined evaluation equation. While paying attention to the neighborhood of the extrema in this combined evaluation equation, α is automatically determined. Namely, mappings which minimize E_tot are obtained for various α's. Among such mappings, α at which E_tot takes the minimum value is defined as an optimal parameter. The mapping corresponding to this parameter is finally regarded as the optimal mapping between the two images.

Many other methods are available in the course of setting up evaluation equations. For instance, a term which becomes larger as the evaluation result becomes more favorable, such as 1/E₁ and 1/E₂, may be employed. A combined evaluation equation is not necessarily a linear sum, but an n-powered sum (n=2, ½, −1, −2, etc.), a polynomial or an arbitrary function may be employed when appropriate.

The system may employ a single parameter such as the above α, two parameters such as η and λ as in the premised technology, or more than two parameters. When there are more than three parameters used, they may be determined while changing one at a time.

• (2) In the premised technology, a parameter is determined in a two-step process. That is, in such a manner that a point at which C_f^(m,s) takes the minima is detected after a mapping such that the value of the combined evaluation equation becomes minimum is determined. However, instead of this two-step processing, a parameter may be effectively determined, as the case may be, in a manner such that the minimum value of a combined evaluation equation becomes minimum. In this case, αE₀+βE₁, for example, may be used as the combined evaluation equation, where α+β=1 may be imposed as a constraint so as to equally treat each evaluation equation. The automatic determination of a parameter is effective when determining the parameter such that the energy becomes minimum.
• (3) In the premised technology, four types of submappings related to four types of critical points are generated at each level of resolution. However, one, two, or three types among the four types may be selectively used. For instance, if there exists only one bright point in an image, generation of hierarchical images based solely on f^(m,3) related to a maxima point can be effective to a certain degree. In this case, no other submapping is necessary at the same level, thus the amount of computation relative on s is effectively reduced.
• (4) In the premised technology, as the level of resolution of an image advances by one through a critical point filter, the number of pixels becomes ¼. However, it is possible to suppose that one block consists of 3×3 pixels and critical points are searched in this 3×3 block, then the number of pixels will be 1/9 as the level advances by one.
• (5) In the premised technology, if the source and the destination images are color images, they would generally first be converted to monochrome images, and the mappings then computed. The source color images may then be transformed by using the mappings thus obtained. However, as an alternate method, the submappings may be computed regarding each RGB component.Preferred Embodiments Concerning Image Effects

Image-effect techniques and image-effect apparatus utilizing aspects of the above described premised technology will now be described with reference to FIGS. 18–23.

FIG. 18 shows a first image I1 and a second image I2, which serve as key frames, where certain points or pixels p₁(x₁, y₁) and p₂(x₂, y₂) correspond therebetween. The correspondence between these pixels is obtained using the premised technology described above.

Referring to FIG. 19, when a mesh is provided on the first image I1, a corresponding mesh can be formed on the second image I2. Now, a polygon R1 on the first image I1 is determined by four lattice points A, B, C and D. This polygon R1 is called a “source polygon.” As has been shown in FIG. 19, these lattice points A, B, C and D have respectively corresponding points A′, B′, C′ and D′ on the second image I2, and a polygon R2 formed by the corresponding points is called a “destination polygon.” In this embodiment, the source polygon is generally a rectangle while the destination polygon is generally a quadrilateral. In any event, according to the present embodiment, the correspondence relation between the first and second images is not described pixel by pixel, instead, the corresponding pixels are described with respect to the lattice points of the source polygon. Such a description is made available in a corresponding point file. By directing attention to the lattice points, storage requirements (data volume) for the corresponding point file can be reduced significantly.

The corresponding point file is utilized for generating an intermediate image between the first image I1 and the second image I2. As described in the premised technology section above, intermediate images at arbitrary temporal position can be generated by interpolating positions between the corresponding points. Thus, storing the first image I1, the second image I2 and the corresponding point file allows morphing between two images and the generation of smooth motion pictures between two images, thus providing a compression effect for motion pictures.

FIG. 20 shows a method for computing the correspondence relation between points other than the lattice points, from the corresponding point file. Since the corresponding point file includes information on the lattice points only, data corresponding to interior points of the polygon need to be computed separately. FIG. 20 shows a correspondence between a triangle ABC which corresponds to a lower half of the source polygon R1 shown in FIG. 19 and a triangle A′B′C′ which corresponds to that of the destination polygon R2 shown in FIG. 19. Now, suppose that an interior point Q, of the triangle ABC, interior-divides the line segment AC in the ratio t:(1−t) and the point Q interior-divides a line segment connecting such the interior-divided point and a point B in the ratio s:(1−s). Thus, it may be thought of in a manner that a corresponding point Q′, which corresponds to the point Q, in a triangle A′B′C′ in a destination polygon side interior-divides a line segment A° C.′, in the ratio t:(1−t) and the point Q′ interior-divides a line segment connecting such the interior-divided point and a point B′ corresponding to B in the ratio s:(1−s). In this case, it is preferable that the source polygon is divided into triangles, and interior points of the destination polygon are determined in the forms of interior-division of vectors concerning the triangle. When expressed in a vector skew field, the above becomesBQ=(1−s){(1−t)BA+tBC},thus, we haveB′Q′=(1−s){(1−t)B′A′+tB′C′}

Of course, a similar process may be performed on a triangle ACD which corresponds to an upper half of the source polygon R1 shown and a triangle A′C′D′ which corresponds to that of the destination polygon R2.

FIG. 21 shows the above-described processing procedure. Firstly, the matching results on the lattice points taken on the first image I1 are acquired (S10) as shown in FIG. 19. It is preferable that the pixel-by-pixel matching according to the premised technology is performed, so that a portion corresponding to the lattice points is extracted from those results. It is to be noted that the matching results on the lattice points may also be specified based on other matching techniques such as optical flow and block matching, instead of using the premised technology.

Thereafter, destination polygons are defined on the second image I2 (S12), as shown in the right side of FIG. 19. Once all destination polygons are defined, the corresponding point file is output to memory, data storage or the like (S14). The first image I1, the second image I2 and the corresponding point file can be stored on an arbitrary recording device or medium, or may be transmitted directly via a network or broadcast or the like.

FIG. 22 shows a procedure to generate intermediate images by using the corresponding point file. Firstly, the first image I1 and the second image I2 are read in (S20), and then the corresponding point file is read in (S22). Thereafter, the correspondence relation between points in source polygons and those of destination polygons is computed using a method such as that described with regard to FIG. 20 (S24). At this time, the correspondence relation for all pixels within the images can be acquired. As described in the premised technology, the coordinates and brightness or colors of points corresponding to each other are interior-divided in the ratio u:(1−u), so that an intermediate image in a position which interior-divides temporally in the ratio u:(1−u) between the first image I1 and the second image I2 can be generated (S26). However, different from the premised technology, in this embodiment, the colors are not interpolated, and the color of each pixel of the first image I1 is simply used as such without any alteration thereto. It is to be noted that not only interpolation but also extrapolation may be performed.

FIG. 23 shows a structure of an image-effect apparatus 10 which generates or reproduces moving pictures at various speeds. The image-effect apparatus 10 includes: an image input unit 12 which acquires the first image I1 and second image I2 from an external storage device, a camera, a network or some other source as is known in the art; a matching processor 14 which performs a matching computation on these images using the premised technology or other technique, a corresponding point file storage unit 16 which stores the corresponding point file F generated by the matching processor 14, an intermediate image generator 18 which generates one or more intermediate images from the first image I1, the second image I2 and the corresponding point file F, and a display unit 20 which displays the first image I1, intermediate images, and the second image I2 as a motion picture. Moreover, a communication unit 22 may also send out the first image I1, the second image I2 and the corresponding point file F to a transmission infrastructure, such as a network or broadcast or the like, according to an external request. As shown in FIG. 23, mesh data, such as the size of the mesh, the positions of the lattice points and so forth, may also be input in the matching processor 14 either as fixed values or interactively.

The apparatus 10 further includes a speed specifying unit 100, which acquires an instruction from a user as to a speed at which a motion picture is reproduced, and a speed controller 102 which controls the number of intermediate images generated by the intermediate image generator 18, based on the acquired instruction. In the case where the apparatus 10 is a computer terminal such as a PC or the like, the speed specifying unit 100 may be, for example, a button-like graphical user interface (GUI) element which appears on a screen and is activated by user input through a mouse or a keyboard or the like. In the case where the apparatus 10 is a digital camera or a video reproduction apparatus, the speed specifying unit 100 may be, for example, a physical button or dial or a remote control, respectively.

By implementing the above-described structure, the first image I1 and the second image I2, which were input in the image input unit 12, are sent to the matching processor 14. The matching processor 14 performs a pixel-by-pixel matching computation between the images I1, I2. The matching processor 14 generates the corresponding point file F based on the mesh data, and the thus generated corresponding point file F is output to the storage unit 16.

The intermediate image generator 18 reads out the corresponding point file F and generates one or more intermediate image. The speed controller 102 interprets the instruction input by the user through the speed specifying unit 100, and then adjusts the number of intermediate images to be generated. For example, the user may choose among various levels of slow motion by increasing or decreasing the number of intermediate images to be generated between the first image I1 and the second image I2 by operating an up-down button on a remote control. In this case, if the up button designates an increase in the number of intermediate images, pressing the up button provides more intermediate images and thus, “slower” slow motion, while pressing the down button provides fewer intermediate images and thus having the motion picture closer to its original or normal speed.

The first image I1 and the second image I2 may be extracted from moving pictures distributed via many methods, such as a broadcast network, the Internet, satellite or the like. In one example, the image input unit 12 may be configured as including a sampling unit which samples images or frames periodically and stores them temporarily and a selection unit which selects two of the sampled images as the first image I1 and the second image I2 when the user demands slow motion images. In this case, one or more intermediate images may be generated from the selected first image I1 and the second image I2.

As another example, the image input unit 12 may be configured to include a first unit which acquires an image being displayed at the moment when the user demands slow motion images as the second image I2, and a second unit which acquires an image reversed therefrom by a predetermined duration of time as the first image I1, so that one or more intermediate images may be generated thereby. In this case, similar to the example above, images need to be kept available for a predetermined amount of time in a buffer or the like.

As still anther example, the apparatus 10 or the image input unit 12 may further include a selecting unit by which the user specifies two timings for images previously captured or recorded and which extracts the two images that existed at the timings, as the first image I1 and the second image I2, so that one or more intermediate image may be generated based on the two extracted images. Alternatively, the selecting unit may display the captured or recorded images in a selection or glancing-through manner such as thumbnail images, so that the user may specify two images among many captured or recorded images rather than the timings of the images.

In the above examples, the recording of images may be made according to a user's instruction, may be automatic, or may be for a predetermined time, however, the image input unit 12 may be configured as a sampling unit which records images endlessly in the background in a free-running state, for example, when the user is enjoying a television broadcast. In this case, the user can enjoy seeing slow motion or super slow motion images for scenes of his/her interest at any time. It is noted that the speed specifying unit 100, in some form, may be used by the user for specifying the display of the slow motion images and may be used to set a speed of slow motion through the speed controller 102.

At any rate, the intermediate image or images generated are sent to the display unit 20, and are displayed there at a specified speed as a moving picture. As evident from this operation, the intermediate image generator 18 and the display unit 20 may be provided in a remote terminal (not shown) which is separate from the apparatus 10, for example, a remote terminal connected to a network which is also connected to communication unit 22 as described below. In this case, the terminal can receive relatively light data (low data volume) comprised of the first image I1, the second image I2 and the corresponding point file F and can independently reproduce intermediate frames and motion pictures.

The communication unit 22 is structured and provided on the basis that there is provided a remote terminal as described above. The communication unit 22 sends out the first image I1, the second image I2 and the corresponding point file F via a network or broadcast or the like, so that motion pictures can be displayed at the remote terminal side. Of course, the remote terminal may also be provided for the purpose of storage instead of display. For example, the apparatus 10 may be used such that the first image I1, the second image I2 and the corresponding point file F therefor are input from a remote terminal or an external unit via a network or the like via the communication unit 22 and these data are then transferred to the intermediate image generator 18 where interpolation is performed to generate one or more intermediate images for display. A data path P for this purpose is shown in FIG. 23.

Experiments have been carried out generally according to the processing described for the present embodiments. In these experiments, smooth slow motion effects which are from ten to some hundreds of times slower than conventional slow motion were obtained. Such precise slow motion image effects can not be achieved even by state-of-the-art high-speed cameras, and therefore images which are physically impossible to capture or shoot are realized by using image processing according to the present invention. Since, theoretically speaking, there is no upper limit for the number of intermediate images generated using the apparatus 10, any level of slow motion is possible.

Moreover, further experiments were carried out to observe effects in which the processing is performed exclusively on the lattice points. For example, when using images of 256×256 pixels or a similar size for the first image I1 and second image I2, satisfactory motion pictures and image effects such as slow motion were obtained by setting the lattice points at intervals of 10 to some tens of pixels. In these cases, the size of the corresponding point file F was generally under approximately 10 kilobytes, and it was confirmed that high image quality with a small data amount could be achieved.

Although the present invention has been described by way of exemplary embodiments, it should be understood that many changes and substitutions may be made by those skilled in the art without departing from the spirit and the scope of the present invention which is defined by the appended claims.

Claims

1. An image-effect apparatus, comprising: an intermediate image generator which acquires a first image, a second image and a corresponding point file for the first image and the second image and generates an intermediate image between the first image and the second image;a speed controller which controls an operation of said intermediate image generator with respect to a speed at which the intermediate image is generated; andan output unit for outputing the first image and intermediate image,wherein the corresponding point file describes lattice points of a mesh taken on the first image, wherein the lattice points represent less than all of the pixels in the first image, and a positional relation of points in the second image which correspond to the lattice points.

2. An apparatus according to claim 1, further comprising a speed specifying unit which receives from a user a desired speed, wherein said speed controller controls said intermediate image generator according to the desired speed.

3. An apparatus according to claim 1, wherein said intermediate image comprises a plurality of intermediate images and said speed controller controls the number of intermediate images generated by said intermediate image generator.

4. An apparatus according to claim 1, further comprising a display unit which displays the first image, the intermediate image, and the second image as a moving picture.

5. An image-effect apparatus, comprising: an image input unit which acquires a first image and a second image;a matching processor which computes a matching between the first image and the second image and then outputs a matching result as a corresponding point file;an intermediate image generator which generates an intermediate image between the first image and the second image based on the corresponding point file;a speed controller which controls said intermediate image generator with respect to a speed at which the intermediate image is generated; andan output unit for outputing the first image and the intermediate image,wherein said matching processor generates the corresponding point file in a manner such that a destination polygon in the second image corresponds to a source polygon of a mesh defined on the first image, wherein the mesh represents less than all of the pixels in the first image.

6. An apparatus according to claim 5, wherein said matching processor performs a pixel-by-pixel matching computation based on correspondence between a critical point detected through a two-dimensional search on the first image and a critical point detected through a two-dimensional search on the second image.

7. An apparatus according to claim 6, wherein said matching processor initially multiresolutionalizes the first image and the second image using the critical points then performs the pixel-by-pixel matching computation between related multiresolution levels while also inheriting a result of a pixel-by-pixel matching computation at a different multiresolution level in order to acquire a pixel-by-pixel correspondence relation at a finest resolution level at a final stage.

8. An apparatus according to claim 5, further comprising a communication unit which outputs the corresponding point file to an external unit.

9. An apparatus according to claim 8, wherein said intermediate image comprises a plurality of intermediate images and said speed controller controls the number of intermediate images generated by said intermediate image generator.

10. An apparatus according to claim 5, wherein said intermediate image comprises a plurality of intermediate images and said speed controller controls the number of intermediate images generated by said intermediate image generator.