text:
|Publication number
|Publication type
|Application number
|Publication date
|Jun 30, 1987
|Filing date
|Jun 27, 1983
|Priority date
|Jun 27, 1983
|Fee status
|Publication number
|Edwin P. Berlin, Jr., Geoffrey Y. Gardner, Robert M. Gelman, Michael N. Gershowitz
|Original Assignee
|Grumman Aerospace Corporation
|Export Citation
|BiBTeX, EndNote, RefMan
|Patent Citations (11), Non-Patent Citations (8), Referenced by (94), Classifications (10), Legal Events (7)
|External Links: USPTO, USPTO Assignment, Espacenet
B.sub.1 X+B.sub.2 Y+B.sub.3 Z+B.sub.4 ○R 0
a.sub.1 =q.sub.7.sup.2 -4q.sub.0 q.sub.1
a.sub.2 =q.sub.9.sup.2 -4q.sub.0 q.sub.3
a.sub.3 =2q.sub.7 q.sub.9 -4q.sub.0 q.sub.6
a.sub.4 =(2q.sub.7 q.sub.8 -4q.sub.0 q.sub.4)f
a.sub.5 =(2q.sub.8 q.sub.9 -4q.sub.0 q.sub.5)f
a.sub.6 =(q.sub.8.sup.2 -4q.sub.0 q.sub.2)f.sup.2
a.sub.1 h.sup.2 +a.sub.2 v.sup.2 +a.sub.3 hv+a.sub.4 h+a.sub.5 v+a.sub.6 =0
e.sub.1 =B.sub.4.sup.2 q.sub.1 -B.sub.1 B.sub.4 q.sub.7 +q.sub.0 B.sub.1.sup.2
e.sub.2 =B.sub.4.sup.2 q.sub.3 -B.sub.3 B.sub.4 q.sub.9 +q.sub.0 B.sub.3
e.sub.3 =B.sub.4.sup.2 q.sub.6 -B.sub.1 B.sub.4 q.sub.9 -B.sub.3 B.sub.4 q.sub.7 +2B.sub.1 B.sub.3 q.sub.0
e.sub.4 =(B.sub.4.sup.2 q.sub.4 -B.sub.2 B.sub.4 q.sub.7 -B.sub.1 B.sub.4 q.sub.8 +2B.sub.1 B.sub.2 q.sub.0)f
e.sub.5 =(B.sub.4.sup.2 q.sub.5 -B.sub.2 B.sub.4 q.sub.9 -B.sub.3 B.sub.4 q.sub.8 +2B.sub.2 B.sub.3 q.sub.0)f
e.sub.6 =(B.sub.4.sup.2 q.sub.2 -B.sub.2 B.sub.4 q.sub.8 +B.sub.2.sup.2 q.sub.0)f.sup.2
e.sub.1 h.sup.2 +e.sub.2 v.sup.2 +e.sub.3 hv+e.sub.4 h+e.sub.5 v+e.sub.6 =0.
l.sub.1 =B.sub.1-1 /B.sub.4-1 -B.sub.1-2 /B.sub.4-2
l.sub.2 =B.sub.3-1 /B.sub.4-1 -B.sub.3-2 /B.sub.4-2
l.sub.3 =B.sub.2-1 /B.sub.4-1 -B.sub.2-2 /B.sub.4-2
l.sub.1 h+l.sub.2 v+l.sub.3 =0.
t.sub.1 =B.sub.1 /B.sub.4 -q.sub.7 /2q.sub.0
t.sub.2 =B.sub.3 /B.sub.4 -q.sub.9 /2q.sub.0
t.sub.3 =(B.sub.3 /B.sub.4 -q.sub.8 /2q.sub.0)f
P.sub.xi =J.sub.xi sin (φ.sub.xi y)+K.sub.xi sin (ψ.sub.xi z)
P.sub.yj =J.sub.yj sin (φ.sub.yj x)+K.sub.yj sin (ψ.sub.yj z)
W.sub.1 =1/2+(3√2/8)d-(√2/16)d.sup.3
W.sub.2 =1-W.sub.1
P.sub.xi =J.sub.xi sin (φ.sub.xi y)+K.sub.xi sin (ψ.sub.xi z)
P.sub.yj =J.sub.yj sin (φ.sub.yj x)+K.sub.yj sin (ψ.sub.yj z)
W.sub.1 =1/2+(3√2/8)d-(√2/16)d.sup.3
W.sub.2 =1-W.sub.1
This invention relates to computer image generation (CIG) systems in general, and in particular to dynamic (real time) CIG systems which model objects by means of nonlinear surfaces.
In order to achieve the high data rates required for real-time displays, a number of current CIG systems employ linear modeling techniques. Each object in the viewable scene displayed by such prior art image generators is defined as a polygon (or polyhedron) whose projection into the image plane consists of linear edges. Examples of such systems may be found in U.S. Pat. Nos. 3,602,702; 3,621,214; 3,736,564; 4,179,824; and 4,276,029; issued respectively to Warnock; Romney et al; Watkins; Marsh, and Gibson et al.
One advantage--indeed, the major justification--of linearization is simplified computation. By their nature, however, edge systems produce a stylized scene feature characterized more by linear artifacts than by the true nature of the desired imagery. Furthermore, scene content and detail are severely limited by the edge-count capacity of the system.
Of course, improvements in hardware capability have significantly enhanced the edge count of present CIG designs. Scene modeling still remains a problem, though, because even a small number of objects may include thousands of edges or faces which must each be positioned and linked in a reference coordinate system. Because actual reference coordinates, rather than descriptive features, are used to model objects in edge systems, automation of the modeling--i.e., off-line data base construction--is quite complicated and will typically require a significant investment in off-line equipment.
In addition to providing gross details of each modeled object, many CIG systems enhance scene content by texturing or varying the image intensity from pixel to pixel to create the illusion of a non-smooth surface. Texturing is accomplished, in general, in one of three ways. Most straightforward is the mapping of a stored texture pattern onto the image plane projection of the modeled object. This method is conceptually illustrated by the decor simulation method of U.S. Pat. No. 3,683,779; issued to Lifton. In a CIG system, of course, the texture pattern transparencies of Lifton would be implemented by means of memory storage devices with various patterns stored as digitized images. Scaling may be achieved by interpolation, but the data base for stored texture patterns is nonetheless extremely inefficient.
A second method of texturing takes advantage of the indeterminate nature of natural surface detail by simply varying color or intensity in a random fashion across the surface to be textured. Without relating the intensity variation in some way to object model coordinates, though, perspective validity cannot be maintained in a dynamic sequence.
Texture functions, a third general method for texturing, alleviate some of the problems discussed above, since they may be implemented with less memory than stored texture patterns and they may be mapped onto modeled objects, without change from frame-to-frame, to ensure perspective validity. An example of a system which uses preselected address bits for regulating texture is shown in U.S. Pat. No. 4,225,861, issued to Langdon et al. Existing texture functions, however, have certain drawbacks. Simple functions tend to produce regular unnatural patterns, while more complex functions add to computational expense and thereby exacerbate the problem of real time generation. It is clear, then, that desirable features in a CIG texture generator include correct representation of the indeterminate nature of natural surface textures, frame-to-frame coherence, and low storage and computational overhead.
A still further item of interest in CIG systems is antialiasing. Each frame in a dynamic image must be represented by a finite number of spatially sampled picture elements or pixels arranged in a raster format with equal spacing. The Nyquist Sampling theorem states that no spatial frequencies in the sampled signal greater than one half the sample frequency defined by the pixel width can be properly represented. Of course, the ideal solution to aliasing is to pre-filter the image before sampling to suppress all spatial frequencies greater than the Nyquist frequency. Unfortunately, implementation of an ideal low pass spatial filter is computationally prohibitive for real time frame rates.
Because ideal filtering is so computationally expensive, a number of approximate techniques have been developed. In one such method, each pixel is subdivided into an nxn subpixel array and the intensity adjusted in accordance with the number of subpixels in each different intensity or color area. No prior art antialiasing techniques have been developed, however, which completely eliminate the crawling, jumping and scintillation effects which characterize a dynamic sequence of aliased images. General discussions of antialiasing centering on more recent methods may be found in "Filtering Edges for Gray-Scale Displays", by Gupta and Sproull, Computer Graphics, Vol. 15, No. 3, August 1981; and "Anti-Aliasing through the Use of Coordinate Transformations", by K. Turkowski, ACM Transactions on Graphics, Vol. 1, No. 3, July 1982.
A principal object of the present invention is to provide a CIG system which will produce images free of the linear artifacts characteristic of edge type systems.
Another related object is to provide such a system in which scene modeling is characterized by the use of descriptive parameters.
A still further object of the present invention is the provision of a CIG system capable of producing dynamic images in real time.
Yet another object of this invention is to provide a system capable of implementing a texture generator with full perspective validity.
It is one still further object of the present invention to provide a CIG system with effective antialiasing.
In keeping with the foregoing objects, several preferred embodiments of the inventive CIG system and compatible modeling, texturing and antialiasing techniques are described. In one embodiment, a real time dynamic system is characterized by a highly modular architecture in which the projection of each viewable object in a scene model is processed by a dedicated object processor, and the image plane is divided into a plurality of uniform, contiguous subframes each processed by a dedicated subframe processor. A general purpose computer accesses a bulk storage device, and transfers object parameters therefrom to an available object processor as each object enters the viewable scene. A routing processor ensures that each object processor's output is passed to the appropriate subframe processors.
The modular assignment of computational tasks minimizes the necessity of intercommunication among the various elements. Each object processor, for example, produces a subframe bit map indicating which subframe or subframes are superimposed by the projection of the object being processed by that object processor. Thus, the routing processor need only receive the bit maps from each object processor, and each subframe processor need only receive information from the appropriate object processors. In a similar fashion, the system architecture is designed to minimize the bandwidth of each other critical data link as well.
Another feature of the real time system is the provision of double buffered input and output memories for each object and subframe processor. Each individual object or subframe processor is thus allowed to perform its assigned task using the most current data completely in parallel with every other processor, making real time image generation possible.
The real time image generation capability of the present invention makes the system especially suitable for flight training simulators. A preferred embodiment adapted for such use includes a simulated flight control console which continuously outputs updated viewpoint parameters for a simulated flight platform. The viewpoint parameters specify the location and orientation of the flight platform in the same object model space or reference coordinate system used to specify the object parameters in the bulk storage. In turn, the general purpose computer uses the viewpoint parameters to assign an available object processor to each object viewable in the image plane defined by the viewpoint parameters. The updated viewpoint parameters are also passed to each active object processor for exact determination of image plane curve coordinates defining the perspective projection of each object in the current image plane defined by the viewpoint parameters.
For applications not requiring real time image generation, the present invention is adaptable to off-line systems. One such system uses a general purpose computer to implement, in sequential fashion, the tasks of object and subframe processing performed by special-purpose, dedicated hardware modules operating in parallel in the real time system.
Further advantages and applications of the present inventive system will become clear upon reading the detailed descriptions of preferred embodiments which follow.
Reference is made in the detailed description to the appended drawings, in which:
FIG. 1 is a schematic block diagram of a preferred embodiment of the present invention;
FIG. 2 is a detailed block diagram of an object processor from FIG. 1;
FIG. 3 is a detailed block diagram of a subframe processor from FIG. 1;
FIG. 4 is a detailed block diagram of the routing processor from FIG. 1;
FIG. 5 is a schematic showing the relationship between a simulated image plane and model space ground plane;
FIG. 6 shows a typical division of the ground plane of FIG. 5 into contiguous areas for arranging object parameters into blocks in a storage memory;
FIGS. 7-12 illustrate the use of quadric surfaces for modeling scene objects;
FIG. 13 illustrates the determination of intraobject visibility;
FIG. 14 shows a portion of the image plane in which two regions of different intensities are separated by a boundary curve;
FIG. 15 shows the frequency response for an ideal low pass spatial filter in two dimensions;
FIG. 16 shows the frequency response for a rotation invariant low pass filter;
FIG. 17 shows the impulse response of the filter whose frequency response is shown in FIG. 16; and
FIG. 18 shows an approximate intensity weighting function for the filter whose frequency response is shown in FIG. 16.
Referring to FIG. 1, the inventive CIG system 10 is embodied in a flight simulator with a simulated flight control console 12 and video display 14. As indicated by data link 16, flight console 12 outputs digitized viewpoint parameters in response to actions by a flight trainee operating the console. The viewpoint parameters are updated once during each passage of a desired frame period, the frame rate being selected so as to bring about compatibility with available video display devices.
The updated viewpoint parameters are received by a mainframe (general purpose) computer 18 programmed to access a bulk memory means such as a disc drive 20. Information in the form of object lists is stored in bulk memory 20, each object list including a plurality of object parameters indicating the size, shape, orientation, location and texture of one of a multiplicity of objects making up the modeled region. The viewpoint parameters indicate the location and orientation of the flight platform simulated by console 12 over the modeled region stored in bulk memory 20. By appropriate interpretation of the viewpoint parameters, the computer 18 keeps track of which modeled objects are viewable in the image plane simulated by video display 14. The object lists for the currently viewable objects and transferred, via data link 22, from bulk memory 20 to the computer 18.
The object parameters for each viewable object are first processed by one of a plurality of object processors 24. As each object enters the viewable scene, it is assigned an object processor by the computer 18 and its object list is transferred to that processor. In addition to keeping track of which objects are currently viewable, computer 18 monitors the availability of each object processor, reclaiming those whose assigned objects leave the viewable scene. Thus, the data link 26 connecting computer 18 with object processors 24 need not be of a sufficient bandwidth to supply each active object processor with a new object list during each frame. In addition to passing the updated viewpoint parameters, link 26 is only required to transfer object lists to newly assigned object processors.
During each frame period, each object processor provides an updated set of coefficients for image plane curves for its assigned object from the viewpoint parameters and the corresponding shape, size, orientation and location object parameters. The image plane curve coefficients represent a perspective projection of the object in image plane coordinates, without regard to the occulting of one object by another. Thus, no intercommunication is necessary among the object processors, and all of the image plane curve coefficients may be computed in parallel during each frame period.
In order to create a video display from the object processor outputs, it is necessary to update an intensity level during each frame period for each of a multiplicity of pixels corresponding to sample points on the image plane. Since a typical video raster may include on the order of 105 to 106 individual pixels, pixel generation in the present CIG system is performed by a plurality of subframe processors 28. Each such processor is associated with a subframe defined by one of a plurality of uniform contiguous areas forming the image plane. It is anticipated that each subframe may include on the order of 32�32 pixels.
Since the image plane curves are updated for each frame, all of the object processor 24 outputs must be transmitted over data link 30 once per frame period. Not all of this information, is needed by each subframe processor 28, however, because for a given frame, most objects will appear in only one subframe or a small group of contiguous subframes. Conversely, few subframes will be required to receive a large number of object processor outputs. In the embodiment of FIG. 1, then, a routing processor 32 governs the transfer of image plane curve coefficients, object parameters, and viewpoint parameters over data link 30. Under control of the routing processor 32, each active object processor 24 output is transmitted only once per frame period and is received only by those subframe processors 28, whose associated image plane areas are intersected by the projection of the associated object.
The digitized pixel intensity levels from subframe processor 28 are received by display driver 34 over data link 36. The pixels are arranged in video raster format by display driver 34, which is preferably a standard digital-to-analog video converter with appropriate timing and synchronizing hardware, so that video signal 38 may be utilized directly by video display 14.
The internal architecture of the object processors 24 is shown in FIG. 2. Preferably, a standard format, such as that of Table A below, is used for all of the object lists. Hence, the identical architecture is employed in a preferred embodiment for all of the object processors 24.
With reference to TABLE A and FIG. 2, an object list transmitted over data link 26 first enters an input buffer 36. At the start of each frame period, the contents of the input buffer 36 are transferred into a working input memory 38. An address register 40 accesses memory 38, allowing individual words therein to be shifted into a data buffer 42. From buffer 42, input words are shifted, by means of a buffer bus 44, to a mask register 46.
TABLE A______________________________________Object List FormatWord Number Parameter(s) # Bits Required______________________________________1 List length 7 Planar surface count 32-4 Location all5-7 Size, Shape all 8-10 Orientation all11-12 Quadric surface texture all13-15 1st Planar surface location all16-17 1st Planar surface texture all18-20 2nd Planar surface location all21-22 2nd Planar surface texture all. . . . . . . . .______________________________________
In order to provide as compact as possible an object model data base, some of the words in the object list format are used for multiple parameters. In the TABLE A format, for example, a seven bit field stores the object list length, while other directory parameters are stored in different fields of the first object list word. Accordingly, register 46 is used to justify and mask off the various partial word parameters from buffer 42.
Once isolated by register 46, the object and viewpoint parameters are made available on a program bus 48. Temporary storage for the parameters is provided by an array of working registers 50 responsive to program bus 48. Three arithmetic logic units, an adder 52, a multiplier 54, and a sine unit 56, preferably a lookup table, are also responsive to program bus 48. Adder 52 and multiplier 54 are additionally responsive to an accumultor bus 58 which in turn is responsive to the sine generator 56 and at least one of the working registers 50. The outputs from the arithmetic logic units 52, 54, and 56 and at least one of the working registers 50 may be loaded into the data buffer 42 or the mask register 46 by means of buffer bus 44.
The clocking, loading and enabling of the various registers, logic units and memories is performed by a control section or program unit including a program sequencer 60, a program store unit 62 and an instruction decoder 64. Because of the high throughput requirement for object processors 24, the instruction sequence stored in unit 62 is preferably implemented in microcoded firmware. Use of a pre-programmed read only memory (ROM) or a random access memory (RAM) loaded from the mainframe for program store unit 62 adds a desirable flexibility to the system, allowing the object processors to be adapted to different data word length or additional parameters such as color information to be added to the object lists by simply replacing the ROM's in each object processor, or by changing the program loaded into the RAM's. Means of loading the RAM's must be provided and will be obvious to those skilled in the art.
It will be noted that the data links in FIG. 2 show only the paths over which data words and memory addresses are transferred. Those skilled in the art will appreciate that various logical outputs from the instruction decoder 64 are used for controlling and timing of the data processing sections. In addition, to accommodate the variations permitted in the object list format of TABLE A--e.g. differences in the number of surfaces defining each modeled object which will necessitate different memory addresses to be loaded from instruction decoder 64 to address register 40--program sequencer 60 preferably includes a number of flag registers responsive to logical signals from the data processing sections. The flag registers, in turn, are used by the program sequencer to adjust a program pointer in response to the particular processing requirements of each object list.
The output from object processor 24 for each frame period is placed in an output memory 66 responsive to address register 40 and data buffer 42. Concurrent with the transfer of input parameters from buffer 36 to memory 38 at the beginning of each frame period, the object processor outputs stored in memory 66 during the previous frame period are transferred to an output buffer 68 for transmission over data link 30.
As shown in FIG. 3, the architecture of the subframe processors 28 is similar to that of object processors 24. In particular, the input buffer 70, the input memory 72, the data buffer 74, the address register 75, the buffer bus 76, the mask register 78, the program bus 80, the working register array 82, the adder 84, the multiplier 86, the sine unit 87, the accumulator bus 88, the program sequencer 90, the program store unit 92, the instruction decoder 94, the output memory 96, and the output buffer 98 of FIG. 3 all function similarly to the like named elements of object processor 24. The higher data throughput and parameter access required at the subframe processing level, however, imposes the requirement of several additional memory addressing modes. This is reflected in the inclusion of an address register array 100 and scratchpad memory 102. As shown, the additional address registers 100, like register 75, are responsive to the program bus 80, and words are loaded into the scratchpad memory 102 from input memory 72 or from memory 102 into output memory 96 according to the addresses in register 100. In a preferred embodiment, subframe outputs are loaded into the scratchpad memory 102 from buffer bus 76, and subframe processor inputs in memory 102 are made available on accumulator bus 88. As with the object processors, the subframe processing sequence stored in unit 92 will correspond to the output format from the object processors stored in the input buffer 70, and flag registers in program sequencer 90 are used to adjust the processing sequence in accordance with the number of object processor outputs received, etc.
FIG. 4 shows a preferred arrangement for the routing processor 32. As shown, the routing processor includes an object processor strobe 104 which addresses the object processors over an object identification bus 106. Included in each object processor 24 is a gate logic circuit 108 responsive to bus 106 and a gate 110 connecting the corresponding object output buffer 68 to data link 30. Similarly, each subframe processor 28 includes an input enable latch 112 responsive to a subframe line identification bus 114 from the routing processor. A subframe group strober 116 addresses predetermined groups of subframe processors over bus 114. A data link monitor 117 responsive to link 30 checks the object outputs for errors or overloads, and communicates any such conditions to mainframe 18 over bus 117b. Bus 117b may also be used to inform monitor 117 of newly assigned or reclaimed object processors, identification of currently active processors in turn being passed, as by signal 117c, to the object processor strobe.
During each frame period, then, object strobe 104 sequentially addresses each active object processor. Each gate logic circuit 108 is arranged to open its associated gate 110 in response to a unique address for the corresponding object processor being transmitted over bus 106. Thus, at any given time, only one object output buffer 68 will be connected to data link 30, allowing the corresponding object output to be transmitted to the subframe processors.
In accordance with the present invention, the first data words in each object output buffer transmitted over data link 30 comprise a subframe bit map. Each object processor generates a new subframe bit map as part of its calculations for each frame period to indicate which subframe processors are to receive its output for that frame. As indicated, an object may lie in several contiguous subframes; therefore, a multiplexed bit map format is used, with each bit in the map corresponding to a designated subframe processor. Since the number of subframes will presumably be greater than the bit length of each data word, several object output buffer words are used to store the bit map, each such bit map word corresponding to a predetermined group of subframe processors.
As each bit map word is transmitted over data link 30, subframe group strober outputs 116 a group identification code over bus 114 to identify the subframe processors corresponding to that group. A unique bit in the subframe bit map may thus be defined for each subframe processor as the logical conjunction of a predefined group code on bus 114 and a predefined data bit from link 30. Recognition of subframe processors designated to receive the output from the currently addressed object processor, then, occurs during transmission of the bit map, the designated subframes in a given bit-map word group being recognized simultaneously by appropriate logic in the associated enable latches 112 as the corresponding bit map word is transmitted over data link 30. In turn, the enable latch 112 for each subframe so recognized is arranged to set an input enable signal 118 to its associated subframe input buffer 70, so that the current object output following the bit map will be simultaneously received by all the bit-map designated subframe processors.
With regard to the sequencing of data from buffers 68 to buffers 70, it will be noted that each group code from subframe group strobe 116 identifies the position of an associated bit map word in the object output buffer. In practice, then, buffer addressing and subframe group identification may be derived from a single counter which is reset by the object strobe 104. The signal on bus 114, incremented for each data word and reset by signal 119 for each object output, may be used directly for parallel addressing of buffers 68 as indicated by address inputs 68a. Since more than one object output may be routed to any given subframe processor, address inputs 70a to buffers 70 are derived from the bus 114 signal by appropriate logic in each enable latch 112.
It is anticipated that the object outputs will not be uniform in length. To lessen the required bandwidth and to avoid possible overloads on data link 30, then, monitor 117 preferably suppresses the transmission of unused words in each buffer 68. In practice, each object processor may pack its output in the upper portion of its output buffer. A flag stored after the last valid output word in each object buffer 68 could then be sensed by appropriate logic in monitor 117, and object strobe 104 accordingly instructed to address the next active object processor. Alternatively, monitor 117 may instruct subframe group strobe/buffer address register 116 to skip addresses not containing currently valid output words.
FIG. 5 schematically illustrates the relation between an object model space ground plane 120 and the image plane 122 modeled by video display 14. In a preferred scheme for modeling objects, the location of each object is represented by three Cartesian coordinates defining a location point in a reference coordinate system. Particular width and depth axes, x and y, define the ground plane 120 and an elevation axis z is perpendicular to ground plane 120. The viewpoint parameters, then, include x, y, and z coordinates of observer 124 in the simulated flight platform.
In addition to indicating observer location with respect to the object model space, the viewpoint parameters, as pointed out earlier, must define the orientation of observer 124 as well. Although an observer line-of-sight (normal to image plane 122) may be represented in vector form by three Cartesian coordinates, the viewpoint orientation parameters must further define any rotation of the image plane about its normal. Such rotation may be represented by a fourth viewpoint orientation parameter specifying an angular measurement.
Alternatively, the viewpoint orientation may be completely defined by three angular measurements. Such a scheme is easily envisioned by considering the yaw, pitch and roll of the simulated flight platform. Thus, the first viewpoint orientation parameter indicates yaw or ground direction, and would be defined as an angular measurement in the ground plane with respect to the x or the z axis. The second parameter corresponds to pitch and indicates an angle with respect to the z axis or the ground plane. Finally, the third orientation parameter specifies roll, and is identical to the fourth parameter in the four-parameter scheme discussed above. An advantage to the three parameter scheme is that yaw, pitch, and roll may be easily derived from the simulated aircraft controls on console 12.
The viewpoint parameters are used by mainframe computer 18 to define a view window 126 in the ground plane 120. FIG. 6 shows two successive view windows 126a and 126b superimposed over a plurality of contiguous rectangular areas 120a-120w in ground plane 120. In a preferred scheme for transferring data from bulk storage means 20 to object processors 24, all the object lists are grouped into blocks of data, each block including all the object lists from one of the contiguous areas in the ground plane. Preferably, the areas are defined such that each includes approximately the same number of modeled objects, whereby the data blocks are substantially equivalent in size. This, the definition of areas 120a-120w depends on the relative density of modeled objects throughout image plane 120. As shown, areas 120f and 120n, for example, cover densely modeled areas, while objects in areas 120i and 120w are more spread out.
The grouping of the object lists into blocks representing contiguous areas in the ground plane facilitates the transfer of object lists by mainframe computer 18, since accessing data from a magnetic disc device is most efficiently accomplished by transferring large blocks of data at one time. The size of each block and corresponding ground plane 120 area, then should be such as to maximize the data transfer efficiency from storage device 20.
To further facilitate the transfer of data to object processors 24, a preferred embodiment of the present inventive CIG system further includes a high speed memory 128 for accessing individual object lists, shown in FIG. 1 in dashed lines. As each image plane area enters the view window, then, all of the object lists in the corresponding block are first transferred to memory 128, where they are temporarily stored pending assignment to an object processor. Conversely, as each area leaves the view window, its associated object lists may be delected from memory 128 to accommodate newly entering areas. In FIG. 6 then, as the view window advances from 126a to 126b, blocks for areas 120r and 120u would be transferred from bulk memory to fast memory 128, and block 120a would be deleted from memory 128.
As pointed out earlier, each object list includes a number of parameters defining its size, shape, etc. In order to provide as compact as possible an object model data base, and at the same time eliminate the linear artifacts which characterize current edge-type CIG systems, the present system utilizes a single quadric surface to model each object. In particular, it has been found that objects can be acceptably represented by one of only two types of quadric surface--an ellipsoid or a hyperboloid. FIG. 7 shows the general configuration of an ellipsoid, while a two sheeted hyperboloid is illustrated in FIG. 8.
Referring to FIG. 7, then, an object 130 is modeled as an ellipsoid geometrically centered about is location point 132. Orthogonal object axes x130, y130, and z130, intersecting at point 132, are used to define the shape and size parameters for object 130. Thus, the object 130 shape and size parameters comprise three radical lengths X130, Y130, and Z130, (shown as heavy lines) taken along axes x130, y130 and z130 from location point 132 to the surface of the ellipsoid.
FIG. 8 shows an object 134 modeled by the lower part of a two sheeted hyperboloid geometrically centered about point 136. The bounding cone 138 for the hyperboloid is shown in long dashed lines. For convenience, the axes x134, y134, and z134, are defined as intersecting at the vertex 140 of the lower part of the hyperboloid. The shape and size parameters for object 134, then, comprise three linear measurements X134, Y134, and Z134, (again, shown in heavy lines) taken along axes x134, y134, and z134, from vertex 140 to the surface of bounding cone 138.
The object orientation parameters for each object comprise three angular measurements specifying, in a manner similar to that used to define the viewpoint orientation parameters, the angular relationship of the object axes with respect to the x, y and z axes of the reference coordinate system.
Further flexibility in object modeling is provided by the use of bounding planes in conjunction with each quadric surface. FIGS. 9-12 illustrate the use of bounding planes for modeling various objects.
FIG. 9 shows a tree 142 in which the foliage is modeled by an ellipsoid 144 and the trunk is represented by a sharp hyperboloid 146 bounded by two planar surfaces 148 and 150. Alternatively, the trunk could be modeled as a cylinder bounded by two planes, since a cylinder may be defined as a degenerate ellipsoid by specifying an infinite radius along one object axis. Of course, tree 142 requires two object lists, since it is defined by two quadric surfaces.
Another species of tree is illustrated in FIG. 10. As shown, tree 152 is modeled as a single quadric surface, hyperboloid 154, since its trunk is substantially invisible. One bounding plane 156 defines the lower limit of the tree 152 foliage, and a second bounding plane, not shown, is used to eliminate the upper part of hyperboloid 154.
FIG. 11 shows an aileron 158 modeled as a thin elliptical cone 160 bounded by three planes 162, 164 and 166. A cone is defined as a degenerate hyperboloid by specifying a zero distance from the vertex of the hyperboloid to the location point. Of course, this necessitates that the remaining two linear measurements be taken from another point on the hyperboloid's z axis, preferably at some standard predefined distance, such a unit, from the vertex.
FIG. 12 illustrates the use of hyperboloids for modeling a mountain range 168, which includes three peaks 170, 172 and 174. As shown, peaks 170 and 172 are modeled by single hyperboloids 176 and 178, while peak 174 is made up of two stacked hyperboloids 180 and 182. Hyperboloids 176, 178 and 180 are bounded by ground plane 120 below. Surface 182 is bounded below, and surface 180 above, by a common bounding plane 184. As described with respect to tree 152 of FIG. 10, hyperboloid surfaces 176, 178, and 182 must be bounded above, by planes, not shown, to eliminate the upper hyperboloid sheet. Also, surfaces 176 and 178 are bounded by a common plane 186, and surfaces 178 and 180 by plane 188.
It will be noted that some surface discontinuity is introduced by using a common bounding plane for abutting quadric surfaces. This is seen in FIG. 12 at bounding planes 184, 186 and 188. Thus, surface 176 intersects plane 186 along curve 190, while a different intersection curve 192 is presented by plane 186 and surface 178. Similarly, plane 188 intersects surfaces 178 and 180, respectively, at curves 194 and 196; and plane 184 intersects surface 180 and 182, respectively, at curves 198 and 200.
At first glance it might appear simpler to allow the quadric surfaces themselves to intersect along a single curve, and to eliminate the bounding plane. Of course scene modeling would be simplified by such a procedure, since the need to find common bounding planes with the closest possible intersection curves, to maximize surface continuity between adjoining quadric surfaces, would be obviated. Bearing in mind, however, that the image plane curve coordinates for each quadric surface are computed by a single object processor 24 having no data on any other quadric surfaces, the necessity of bounding planes becomes obvious.
A further impediment to representing the intersection curve of two quadric surfaces is the complexity of the mathematics involved. Those skilled in the art will appreciate that the intersection between any quadric surface and a plane is a simple second order curve. By contrast, the intersection between two quadric surfaces is, in general, a far more complex curve, and calculations involving projections of such complex curves into an image plane are beyond the capability of presently available hardware for purposes of real time calculations. A discussion of the mathematics of quadric surfaces may be found in Analytic Quadrics, by Barry Spain, Pergamon Press, 1960. Particular reference is made to Chapter V of the Spain treatise, on Central Quadrics, for background on ellipsoids and hyperboloids.
Preferably, the object list format is capable of accommodating any number, up to some convenient limit, of bounding planes. Three additional shape parameters are required, as shown in TABLE A, to describe the location of each bounding plane. Preferably, the location of each bounding plane is described by three vector coordinates defining a line segment normal to the bounding plane and extending from the object's location point to a point on the bounding plane. The vector coordinates may be in terms of the reference coordinate system, but are more easily modeled in terms of the object axes. For example, a bounding plane through the geometric center of hyperboloid 134 (FIG. 8), in terms of the object axes x134, y134, z134, would be described as vector (0, 0, Z134). Besides simplifying modeling, use of the object axes to describe bounding planes facilitates the implementation of moving models, since only an object's location and orientation parameters would change as it moves through the scene model space.
Prior to deriving two-axis image plane curve coordinates, each object processor preferably relates its assigned object parameters to the current frame viewpoint parameters by defining the quadric surface and bounding planes in terms of a three-axis eye coordinate system having axes X, Y and Z. The origin of the eye coordinate system is defined as the focal point of observer 124 (FIG. 5), and the Y axis passes through the center of the image plane rectangle 122. The remaining eye coordinate axes X and Z parallel horizontal and vertical axes h and v which define the image plane. The distance from the eye coordinate origin to the image plane is defined to be f, (i.e., the image plane intersects the Y-axis at (0,f,0)).
By appropriate rotation and translation of the object parameters, then, each quadric surface is reduced to ten quadric coordinates q1, q2, . . . , q9, q0 which define the surface function Q(X,Y,Z). The quadric surface, then, is the locus of points for which:
Q(X,Y,Z)=q.sub.1 X.sup.2 +q.sub.2 Y.sup.2 +q.sub.3 Z.sup.2 +q.sub.4 XY+q.sub.5 YZ+q.sub.6 XZ+q.sub.7 X+q.sub.8 Y+q.sub.9 Z+q.sub.0 =0
Similarly, each bounding plane is represented by four bounding plane coefficients B1, B2, B3 and B4 defining a bounding function P(X,Y,Z):
P(X,Y,Z)=B.sub.1 X+B.sub.2 Y+B.sub.3 Z+B.sub.4 ○R 0
where ○R is either ≦ or ≧ such that the inequality is satisfied for points on the side of the bounding plane for which the object is defined.
FIG. 13 shows a portion of image plane 122 with projection curves for an object modeled as an ellipsoid bounded by two planes. The image plane or projection curves are defined by the object processor in terms of h and v, the horizontal and vertical image plane axes. Visible portions of the image plane curves are shown in solid lines, while other portions are shown in broken lines.
The projection of the quadric surface silhouette, herein called the limb curve, is indicated in FIG. 13 as s. Since s is a perspective projection of a quadric surface, it may be represented by a planar function s(h,v):
s(h,v)=a.sub.1 h.sup.2 +a.sub.2 v.sup.2 +a.sub.3 hv+a.sub.4 h+a.sub.5 v+a.sub.6 =0
The image plane curve coefficients a1, a2, . . . , a6 for each limb curve may be derived from the associated quadric coefficients q1, q2, . . . , q0 and the focal point-to-image plane distance f by the following relations:
a.sub.1 =q.sub.7.sup.2 -4q.sub.0 q.sub.1
a.sub.2 =q.sub.9.sup.2 -4q.sub.0 q.sub.3
a.sub.3 =2q.sub.7 q.sub.9 -4q.sub.0 q.sub.6
a.sub.4 =(2q.sub.7 q.sub.8 -4q.sub.0 q.sub.4)f
a.sub.5 =(2q.sub.8 q.sub.9 -4q.sub.0 q.sub.5)f
a.sub.6 =(q.sub.8.sup.2 -4q.sub.0 q.sub.2)f.sup.2
Intersection curves g1 and g2 are projections of the intersections of each bounding plane with the quadric surface. Like the limb curve, each intersection curve may be represented by a quadratic function g in h and v of the general form:
g(h,v)=e.sub.1 h.sup.2 +e.sub.2 v.sup.2 +e.sub.3 hv+e.sub.4 h+e.sub.5 v+e.sub.6 =0
Both the quadric surface coefficients and the bounding plane coefficients associated with a particular intersection curve must be used to derive that curve's coefficients. It may be shown that the intersection curve coefficients e1, e2, . . . , e6 are given by:
e.sub.1 =B.sub.4.sup.2 q.sub.1 -B.sub.1 B.sub.4 q.sub.7 +q.sub.0 B.sub.1.sup.2
e.sub.2 =B.sub.4.sup.2 q.sub.3 -B.sub.3 B.sub.4 q.sub.9 +q.sub.0 B.sub.3.sup.2
e.sub.3 =B.sub.4.sup.2 q.sub.6 -B.sub.1 B.sub.4 q.sub.9 -B.sub.3 B.sub.4 q.sub.7 +2B.sub.1 B.sub.3 q.sub.0
e.sub.4 =(B.sub.4.sup.2 q.sub.4 -B.sub.2 B.sub.4 q.sub.7 -B.sub.1 B.sub.4 q.sub.8 +2B.sub.1 B.sub.2 q.sub.0)f
e.sub.5 =(B.sub.4.sup.2 q.sub.5 -B.sub.2 B.sub.4 q.sub.9 -B.sub.3 B.sub.4 q.sub.8 +2B.sub.2 B.sub.3 q.sub.0)f
e.sub.6 =(B.sub.4.sup.2 q.sub.2 -B.sub.2 B.sub.4 q.sub.8 +B.sub.2.sup.2 q.sub.0)f.sup.2
Intersection line L1-2 is a projection of the intersection between the two bounding planes represented in FIG. 13. Since the projection of the intersection between two planes must also be a line, an equation in general form for the intersection line becomes:
L.sub.1-2 (h,v)=l.sub.1 h+l.sub.2 v+l.sub.3 =0
Using a second subscript to distinguish between the bounding planes, the coefficients for the plane associated with g1 (h,v) become B1-1, B2-1, B3-1, B4-1 ; and the coefficients for the other plane become B1-2, B2-2, B3-2, B4-2. The image plane curve coefficients for intersection line L1-2 are then given by:
l.sub.1 =B.sub.1-1 /B.sub.4-1 -B.sub.1-2 /B.sub.4-2
l.sub.2 =B.sub.3-1 /B.sub.4-1 -B.sub.3-2 /B.sub.4-2
l.sub.3 =(B.sub.2-1 /B.sub.4-1 -B.sub.2-2 /B.sub.4-2)f
In addition to providing image plane curve coefficients representative of the limb curve, the intersection curves and the intersection lines, the object processor preferably resolves the intraobject visibility. That is, the object processor additionally provides information indicating which portions of the image plane curves are visible. Several preliminary calculations are necessary in order to provide such intraobject visibility information.
Visibility test lines T1 and T2 are defined as the projections on the image plane of the lines of intersection between the quadric silhouette plane and each bounding plane. As with the intersection lines, each visibility line may be represented by a linear equation in h and v:
T(h,v)=t.sub.1 h+t.sub.2 v+t.sub.3 =0
t.sub.1 =B.sub.1 /B.sub.4 -q.sub.7 /2q.sub.0
t.sub.2 =B.sub.3 /B.sub.4 -q.sub.9 /2q.sub.0
t.sub.3 =(B.sub.3 /B.sub.4 -q.sub.8 /2q.sub.0)f
Minimum and maximum points, with respect to the image plane vertical axis v, are determined for the limb curve and each intersection curve. These points are identified in FIG. 13 for curves s(h,v), g1 and g2, respectively, as vmin(s), vmax(s), vmin(g1) vmax(g1), vmin(g2), and vmax(g2). Calculation of each vminv and vmaxv (the v coordinate values for vmin and vmax) is performed in accordance with the following equations: ##EQU1## where V1, V2 and V3 are determined in accordance with the image plane curve coefficients for the limb curve or intersection curve. Letting n1, n2 . . . , n6 represent e1, e2, . . . , e6, or a1, a2, . . . a6, then, as appropriate, V1, V2 and V3 are given by:
V.sub.1 =n.sub.3.sup.2 -4n.sub.1 n.sub.2
V.sub.2 =2n.sub.3 n.sub.4 -4n.sub.1 n.sub.5
V.sub.3 =n.sub.4.sup.2 -4n.sub.1 n.sub.6
Also of interest in determining intraobject visibility are the points of contact or tangency between the limb curve and each intersection curve, cs1 (g1), cs2 (g1), cs1 (g2), and cs2 (g2). Calculation of the V coordinate each contact point cs1 and cs2, respectively, may be performed using the identical equations stated above for vmin and vmax by substituting the following values for V1, V2 and V3 :
V.sub.1 =(a.sub.1 t.sub.2 -a.sub.3 t.sub.1)t.sub.2 +a.sub.2 t.sub.1.sup.2
V.sub.2 =(a.sub.1 t.sub.2 -a.sub.3 t.sub.1)t.sub.3 +(a.sub.1 t.sub.3 -a.sub.4 t.sub.1)t.sub.2 +a.sub.5 t.sub.1.sup.2
V.sub.3 =(a.sub.1 t.sub.3 -a.sub.4 t.sub.1)t.sub.3 +a.sub.6 t.sub.1.sup.2
where a1, a2, . . . , a6 are the limb curve coefficients and t1, t2, t3 are the visibility test line coefficients for the associated intersection curve. In general, two contact points cs1 and cs2 exist for each intersection curve and can be determined, as indicated above, from the intersection of the visibility test line and the limb curve. Some intersection curves, it will be noted, may only contact the limb curved at one point (i.e., when (V2 /2V1)2 -V3 /V1 =0); still other intersection curves will not intersect the limb curve at all (i.e., (V2 /2V1)2 -V3 /V1 <0).
Still other key visibility points, in addition to the minimum and maximum limb and intersection curve points and the contact points, are defined by the points of intersection among the intersection lines and the intersection curves. The intersection points between an intersection line and one intersection curve will be identical to the intersection points between that line and the intersection curve associated with the other bounding plane defining the intersection line, as indicated by intersection points i1 (g1,g2) and i2 (g1,g2). In general, the v coordinate values for i1 and i2 may be calculated from the same formulas used to calculate the v coordinate values for cs1 and cs2 by substituting the coefficients for either associated intersection curve for the limb curve coefficients (i.e., substitute e1, e2, . . . , e6 for a1, a2, . . . , a6) and the intersection line coefficients for the visibility test line coefficients (i.e., substitute l1, l2, l3 for t1, t2, t3).
Although no intersection point between two intersection lines is shown in FIG. 13 (since there is only one intersection line), calculation of the v coordinate for such a point may be accomplished by the simultaneous solution for v from the intersection line equation. If a first intersection line set of coefficients is identified by an added "1" subscript, and a second set by an added "2" subscript, it may be shown that the solution for v value of the intersection point iv (L1,L2) is given by: ##EQU2##
In accordance with the present invention, intraobject visibility information is keyed to scan line bands which are defined by the v coordinate values for the key visibility points determined from the equations above. Specifically, the intraobject visibility information provided by each object processor may be arranged on a visibility list having rows corresponding to each scan line band and one column for each limb curve, intersection curve or intersection line. A visibility list for the projected object of FIG. 13 may be arranged as shown in TABLE B.
It will be noted that only the v coordinate values for visibility points which are actually visible are used to define the scanline bands in the list. Thus, as each key point is calculated, its visibility is tested by reference to the bounding plane definitions and the associated visibility test line and intersection line definitions. The necessary tests for each point depend on the kind of point being tested, i.e.:
1. limb curve minimum or maximum
2. intersection curve minimum or maximum
3. contact point (limb and intersection curves)
4. intersection point (intersection lines and curves)
TABLE B______________________________________Intraobject Visibility Listscan line band(upper v coor.value) s(h,v) g.sub.1 (h,v) g.sub.2 (h,v) L.sub.1-2 (h,v)______________________________________vmax.sub.v (s) LR 0 0 0vmax.sub.v (g.sub.1) LR LR 0 0cs.sub.2v (g.sub.1) R LR 0 0i.sub.2v (g.sub.1,g.sub.2) R R 0 1cs.sub.1v (g.sub.2) 0 R R 1i.sub.1v (g.sub.1,g.sub.2) 0 0 LR 0vmin.sub.v (g.sub.2) -- -- -- --______________________________________
Each limb curve minimum or maximum is first tested against each of the visibility test lines, one at a time, by the following relation:
T(h.sub.n,v.sub.n) ○R' 0
where hn and vn are the h and v coordinate values for the point being tested, and ○R' is an inequality relation defined from the associated boundary plane relation. Specifically, ○R' will be identical to ○R from the associated bounding plane relation if the constant term B4 in the relation is greater than 0. Otherwise, ○R' will be the opposite of ○R (i.e., if B4 >0 and ○R is "≦", ○R' will be "≧", and if B4 ≦0 and ○R is "≧", ○R' will be "≦"). The h coordinate value for a given point is found by solving the defining equation for the associated curve for the known v coordinate value.
Each intersection curve minimum or maximum is tested against the associated visibility test line only if the associated bounding plane faces away from the observer (i.e., if the observer 124 focal point is on the object side of the plane). To test which side of the plane the focal point is on the eye coordinates for the focal point (0, 0, 0) are substituted into the defining relation for the bounding plane, resulting in:
B.sub.4 ○R 0
Thus, if this relation is satisfied the intersection curve minimum and maximum must be tested further. As indicated, only the associated visibility test line is tested against. Also the opposite inequality relation to that used to test the limb curve must be used. That is, the intersection curve points will be visible if they fail the visibility line test stated for the limb curve. Again, however, if the focal point is on the opposite side of the object from the intersection curve's associated bounding plane as determined by the preliminary test above, (i.e., the plane faces the observer), both the minimum and maximum points for the associated intersection curve are accepted as having passed the visibility test line test.
For final determination of visibility, each limb and intersection curve minimum and maximum which satisfies all appropriate visibility test lines must be further tested against all intersection lines. Each such minimum or maximum will be visible if its coordinates hn and vn satisfy the following relation for each intersection line:
L(h.sub.n,v.sub.n) ○R' 0
where ○R' is the same relation used with the visibility test lines.
The visibility of each intersection point will depend on whether any of the intersecting planes face the observer. It will be noted that each intersection point between an intersection line and an intersection curve involves two planes and thus may be visible if either satisfies the preliminary test for intersection curve minima and maxima. Each intersection point between two intersection lines is potentially visible if any of three associated bounding planes faces the observer. P Final determination of visibility for each intersection point for which at least one associated bounding plane faces the observer, then, is performed by testing against the unrelated intersection lines. That is, the same test described for limb and intersection curve minima and maxima is used, but each potentially visible intersection point need only be tested against intersection lines which do not pass through that point.
Visibility of each contact point is also tested on the basis of the intersection line test. Contact points which are visible will satisfy the test for all intersection lines.
Referring again to FIG. 13, application of the key point visibility tests just described is illustrated. The limb curve minimum vmin(s) is found to be invisible when tested against visibility test line T2, while the maximum vmax(s) is visible since it satisfies T1,T2 and intersection line i1-2. Similarly, intersection curve g2 minimum vmin(g2) is visible because it satisfies both T2 and i1-2, but the maximum vmax(g2) fails to satisfy T2 and is therefore not visible. The minimum and maximum for g1 are not tested against the associated visibility test line T1 because the bounding plane defining g1 faces the observer. However, only the maximum vmax(g1) is visible because the minimum vmin(g1) fails to satisfy the test for intersection line i1-2. Contact points cs2 (g1) and cs1 (g2) are visible because they satisfy the intersection line, while cs2 (g2) and cs1 (g1) do not satisfy i1-2 and are therefore invisible. Since one of the planes defining i1-2 faces the observer, intersection points i1 (g1,g2) and i2 (g1,g2) are potentially visible, and the actual visibility of i1 (g1,g2) and i2 (g1,g2) is confirmed since there are no other intersection lines against which the points would be tested.
When all the key visibility points for an object have been calculated and tested for visibility, the v coordinate values are sorted into scan order as in the exemplary visibility list above. Thus, each scan line band is defined as a horizontal strip between two successive v coordinate values. As indicated, the entries in each column correspond to one of the limb or intersection curves or intersection lines, and indicate the visibility of that image plane curve in each scan line band.
Each entry in an intersection line column, it will be noted from the exemplary list, is either "0," indicating that the intersection line is not visible in the corresponding scan line band, or "1", indicating that the line is visible. Four different entry types are needed for the limb and intersection curve columns, since each scan line band will in general intersect a left and a right segment of a given second order curve. Thus, "0" indicates that neither segment is visible; "L" the left segment; "R" the right segment; and "LR" that both segments are visible in the corresponding scan line band.
Derivation of visibility list entries may be accomplished by testing the potentially visible curves in each scan line band with the same visibility tests used for the key visibility points. A limb curve is potentially visible in all the scan line bands defined for a particular object, while an intersection curve's potential visibility is further limited by its minimum and maximum. An intersection line is potentially visible only between its intersection points and only if at least one of its defining planes faces the observer. Prior to derivation of the final visibility list, then, the potential visibility information (i.e., the "end-points") for each image plane curve are preferably kept with the curve's coefficients.
The v coordinate value midway between the upper and lower limit of each scan line band (e.g., [vmaxv (s)+vmaxv (g1)]/2 for the first band on the visibility list above) may be used to test the visibility of potentially visible segments in the band. The h values for each potentially visible curve in the band are solved using the mid-v value, resulting in one point for each potentially visible intersection line and two points (left and right) for each potentially visible limb or intersection curve. Limb and intersection curve points are then tested in the same manner as the corresponding minima and maxima, while intersection line points are tested against any other intersection lines, similarly to intersection points.
Although the foregoing intraobject visibility determination example applies specifically to an ellipsoid-defined object, the mathematical relations are equally applicable to hyperboloid projections. Those knowledgeable in mathematics will realize that the limb curve for a hyperboloid, as defined above, will not necessarily have a minimum and maximum, and that the same will be true for intersection curves associated with such hyperboloid. In such cases, the upper and lower scan line bands will be defined by other key visibility points.
In preparing its subframe bit map, each object processor must save, in addition to the vertical coordinate values from the visibility list, the left most and right most horizontal coordinate values. Although exact computations for the horizontal minimum and maximum are not described, it is generally sufficient to simply use the minimum and maximum h coordinate values for visible points found in each scan line band. Each subframe will have an associated set of minimum and maximum h and v coordinate values which may be compared to the minimum and maximum h and v values for the object to determine the appropriate bit entry for the subframe.
As indicated earlier, the high level information from object processors 24 is utilized by subframe processors to determine intensity levels for a plurality of pixels arranged in raster format to simulate the desired image plane. Video rasters typically will include as many as 1024 rows or lines; each line may include as many as 1024 pixels. The total number of pixels used depends on the required resolution for a particular system.
FIG. 14 shows a portion of a video raster, with pixel centers indicated by cross marks, superimposed by a corresponding portion of a desired image plane including two regions of different intensities, I1 and I2, separated by a boundary curve 202. It is understood that curve 202, in practice, need not be linear, but may be defined by any of the second order image plane curve coefficients output by object processors 24. The regional intensity levels I1, (cross hatched region), and I2 are derived by subframe processors 28 by known mathematical techniques using additional surface and illumination information from the object processors. As shown, the pixels are all square and of uniform width d (center-to-center). Only those pixels referred to in the following discussion are identified by specific call-out numbers drawn to the pixel center cross mark.
Any image plane may generally be described as an intensity function in two spatial dimensions, characterized by continuously varying spatial frequencies. Those knowledgeable in information theory will appreciate that for any sampled image, no intensity variation therein representing a spatial frequency greater than one half the sample frequency will be properly represented. The result of such undersampling is called aliasing, and is particularly pronounced at sharp surface boundaries such as curve 202, where infinite spatial frequency components are present. The ideal solution to aliasing is to low pass filter the image plane prior to sampling, eliminating all spatial frequencies greater than one half the sampling frequency defined by the pixel width. The computational complexity of the ideal approach, however, takes it far beyond the possibility of real time implantation. A preferred antialiasing scheme implemented by subframe processors 28 will be presently explained with reference to FIG. 14.
Sampling of the image plane is first implemented by assigning to each pixel the intensity of the unfiltered image plane at the pixel center. Pixels 204 and 206, for example, would be assigned intensity level I1, while pixels 208 and 210 would be assigned intensity level I2. Then, all those pixels within a predetermined area about boundary curve 202 are identified as aliased pixels. The predetermined area about any image plane curve defining a boundary curve such as curve 202 is defined as that area including all pixel centers within a specified cutoff distance of the boundary curve, the cutoff distance preferably being equal to √2d. In FIG. 14, this predetermined area is shown as the area between dashed lines 212.
For each aliased pixel, a weighting distance w is calculated as the distance (in pixel widths) from the pixel center to the boundary curve. For this calculation, it is necessary to derive a linear approximation for the boundary curve within a radius of √2d of each aliased pixel center. This is illustrated in FIG. 14 by pixel 214. Since pixel 214 lies within the area bounded by lines 212, it is an aliased pixel. The portion of curve 202 shown as a heavy line lies within a radius of √2 d of pixel 214, as shown by circle 216, although no linear approximation is necessary since curve 202 is linear. The weighting distance w for pixel 214 is shown.
Each weighting distance is used to derive two intensity weights, W1 and W2, which are used, in turn, to calculate an antialiased intensity level, I, for the pixel according to an expression:
I=W.sub.1 I.sub.1 +W.sub.2 I.sub.2
The derivation of intensity weights W1 and W2 from weighting distance w is explained with reference to FIGS. 14-17.
As pointed out earlier, the theoretically correct solution to aliasing is to filter the image plane prior to sampling. FIG. 15 shows the spatial frequency domain transfer function for an ideal sampling filter. The abcissa, fh, represents horizontal spatial frequencies in the image plane intensity function, while vertical frequencies are represented on the ordinate, fv. Only those spatial frequencies in the shaded region would remain after ideal pre-sampling filtering. However, such ideal filtering would require computation of the impulse response of the filter of FIG. 15 convolved with the unsampled image plane intensity function, and, as indicated, would be computationally prohibitive.
To simplify the calculation of W1 and W2 for each aliased pixel, it is preferable, then, to base the calculation on a rotationally invariant pre-sample filter having a frequency domain transfer function shown in FIG. 16. It will be noted that the rotation invariant filter of FIG. 16 will attenuate some frequencies which would be passed by the ideal filter of FIG. 15, but rotational invariance implies that intensity weights may be calculated based only on the weighting distance w (FIG. 14) without regard to the slope of the boundary curve 202.
The rotational invariance of the FIG. 16 filter is further illustrated by examining its impulse response, h(r): h(r)=J1 (r)/r where J1 is the first Bessel function. As shown in FIG. 17, h(r) is seen to depend only on a polar coordinate r. Because h(r) is infinite in extent and sometimes negative, it is desirable to approximate h(r) by a function h1 (r) which is positive for |r|<√2 and zero elsewhere. A radius of √2 is preferred because a circular (rotational invariant) impulse response with a smaller response cannot prevent antialiasing along a diagonal boundary curve.
Using the assumptions that within a small region boundary curves are approximately linear and that image plane intensities remain approximately constant within the regions separated by a boundary curve, the antialiased intensity level, I, is given by the convolution of h1 (r) with the image plane intensity function: ##EQU3## where I1 is the image plane intensity of the pixel center, w is the distance from the pixel center to the boundary curve, and I2 is the image plane intensity of the region opposite the boundary curve from the pixel center. This is seen to be the situation of pixel 214 in FIG. 14.
From the foregoing, it will be further appreciated that the intensity weights W1 and W2 are, indeed, a function of weighting distance w. Assuming h1 (r) to be normalized, it becomes clear that W1 will be zero for w<-√2 and one for w>√2. FIG. 17 shows the functional relationship between W1 and d. Since antialiasing is only performed when w<√2, it has been found that, in this region, W1 may be approximated by a third degree polynomial:
W.sub.1 =1/2+(3√2/8)w-(√2/16)w.sup.3
Although as described in reference to FIG. 13, weighting distance w assumes only positive values, it should be clear that a negative distance simply implies that the pixel center lies in the region whose intensity is identified as I2. Thus, the second intensity weight for each pixel, W2, may be found by negating the weighting distance used in the expression above for W1, or, alternatively, by the expression:
W.sub.2 =1-W.sub.1
A further feature of a preferred embodiment of the present invention is the implementation of texturing by subframe processors 28. As shown in TABLE A, each quadric or planar surface includes accommodation in the associated object list for two data words specifying surface texture. It will be understood that the texture data in the object list itself need not be the actual parameters used in the texture function to be described. Rather, the object list texture data may be directory in nature, referencing parameters from a stored texture parameter list; or, alternatively, the object list data may be used by an algorithm to generate texture parameters.
For each visible surface with a specified texture, the subframe processors first identify all of the pixels in the image plane area circumscribed by that surface's image plane curves. For each such superimposed pixel are determined three Cartesian coordinates, x, y and z, of a point on the surface for which the point's image plane projection falls in the pixel center. Preferably, x, y and z are based not on the reference coordinate system, but instead on the object axes of the associated object, so that perspective validity is maintained for moving objects. Next, an intensity modulating factor, T, is calculated for each superimposed pixel using a general texture function with the associated texture parameters for the surface, the arguments for the texture function being the Cartesian coordinates x, y and z, as determined for each pixel.
The actual texture parameters will preferably include spatial frequencies and associated weighting factors statistically related to each object. Derivation of these parameters, then, may be based on Fourier analysis of actual photographs of generically similar objects. Further texture parameters, described herein as phase shift factors, may be derived by similar methods.
It has been found that a great variety of texture patterns giving a very natural appearance may be generated by using a single general formula for the computation of the intensity modulating factor T at each pixel: ##EQU4## where spatial frequencies are indicated as ω, the weighting factors as C, and the phase shift components as P. It is seen that a number m of the spatial frequencies, ωxi, are related, along with associated weighting factors Cxi and phase shift components Pxi, in sum terms to the x coordinate and a number, n, of spatial frequencies ωyj, weighting factors Cyj, and phase shift components Pyj are related to the y coordinate in similar sum terms. It has been found that three frequencies in either direction (x and y) are sufficient to simulate most natural surfaces, and in general the same frequencies can be used in both directions. Still further testing has established that the product of sums format of the equation above yields more natural looking patterns than does a sum of products.
The purpose of the phase shift components is to break up the regularity of the generated pattern. Obviously, if the same frequencies are related to both the x and y coordinates and no phase shifting is employed, a checkerboard like pattern will result. Using different frequencies of x and y will generate a tartan-like pattern. A natural randomness is simulated by shifting each of the sine waves before summing. The x coordinate phase shift components Pxi, are preferably made dependent on the y and z coordinates, while the y coordinate phase shift components, Pyj, are based on the x and z coordinates:
P.sub.xi =J.sub.xi sin (φ.sub.xi y)+K.sub.xi sin (ψ.sub.xi z)
P.sub.yj =J.sub.yj sin (φ.sub.yj x)+K.sub.yj sin (ψ.sub.yj z)
wherein the individual phase shift factors, J, φ, K, and ψ may be stored in each object list, looked up, or derived from the associated spatial frequencies and weighting factors.
The described texturing function, it will be noted, may be adapted to simulate translucence by using the same general formula in conjunction with an assigned translucence limit for each object to be displayed as translucent. Those pixels for which the translucence limit is exceeded by the texture modulating factor would display the object behind the translucent object (i.e., the second rank object).
The modeling of natural foliage, in particular, may be enhanced using a modification of the simulated translucence technique. Specifically, a translucence limit which varies in proportion to the distance from the foliage object boundary is compared to the texture modulating factor for each pixel. As a result, the edge of the foliage appears shaggy and more natural than would be possible using a simple boundary curve.
To implement a variable translucence limit, then, the distance of each pixel on the foliage surface to the surface boundary may be calculated, scaled, and compared to the texture modulating factor. As pointed out in the antialiasing section above, however, exact distance calculation involves the computation of a square root. Preferably, then, an alternate variable translucence limit is used which does not require a costly square root computation for each interior pixel on the foliage surface.
Typically, a foliage object will be modeled as an ellipsoid bounded only on the bottom (e.g., tree 142, FIG. 9) or a hyperboloid lower sheet bounded at the bottom (e.g., tree 152, FIG. 10). The foliage surface, then, will be bounded by a limb curve, s(h, v)=0, as described above. The image region or bounded interior surface may be defined as all points satisfying the expression
s(h, v)<0
The plane quadratic function s(h, v) will therefore have some minimum point inside the boundary which is the geometric center of the limb curve. This minimum, denoted sm, may be calculated from the limb curve coefficients: ##EQU5## A variable translucence limit, r(h, v), may thus be defined, for each interior pixel, as:
r(h, v)=s(h, v)/s.sub.m
As defined, r(h, v) will vary from 0 at the object boundary (limb curve) to 1 at the object center.
The calculation of r(h, v) may be expedited, it will be noted, by computing s(h, v) as a second order function of h of the form:
s(h, v)=R.sub.1 h.sup.2 +R.sub.2 h+R.sub.3
R.sub.1 =a.sub.1
R.sub.2 =a.sub.3 v+a.sub.4
R.sub.3 =a.sub.2 v.sup.2 +a.sub.5 v+a.sub.6
Since v remains constant for each scan line, R1, R2 and R3 would only need to be computed once at the beginning of each line. Further streamlining of scan line computation may be accomplished by dividing R1, R2 and R3 by sm and implementing the second order equation for r directly in an incremental form that involves only two additions without multiplication.
The above variable translucence technique may also be used to model other natural objects, such as mountains or clouds. In some applications, such as mountains, additional stipulations must be made in the variable translucence limit to prevent "holes" from appearing in the modeled object.
Those skilled in the art will appreciate that the foregoing description addresses a structure which may be modified in a variety of ways to suit specific applications. It may, for instance, be desirable to provide direct communication between object processors 24 and mainframe computer 18 to reduce the necessary bandwidth of data link 26 by using a separate bus to transmit the updated viewpoint parameters and to allow appropriate action by the mainframe computer in the case of any overload conditions which might occur in the object processors. Similar communication may be provided between the subframe processors 28 and mainframe computer 18.
The number of object processors 24, will, of course, depend on the required scene content of a given application. Similarly, the required resolution and available hardware will determine the number of subframe processors and pixels for a particular system.
The above described preferred embodiment may also be adapted for use with a variety of known techniques for enhancing the simulation of the desired image plane. For instance, shadow computation techniques may be implemented in the subframe processors in conjunction with an illumination vector (e.g., sunlight or moonlight) supplied by the mainframe computer. Color may be implemented by computing individual red, green, and blue intensity levels adaptable to standard color video display equipment.
With regard to the described antialiasing and texturing techniques, various modifications and adaptations of these techniques will suggest themselves to those skilled in the art. For example, the antialising technique may be adapted to pixels near boundary curve sections which cannot be approximated as a single linear segment by simply considering multiple segments, computing weighting factors for each, then appropriately normalizing the individual segment weighting factors. Similar treatment may be applied to pixels intersecting by two or more boundary curves separating regions of three or more different colors or intensities, or for small surfaces on the order of one or two pixel width dimensions. Another advantage to the texture function employed by the present system is that it provides greater scene content without introducing aliasing problems. Since the texturing function is based on sine waves, it is relatively easy to eliminate those frequency components in each texture pattern which are higher than one half the sample frequency in the image plane.
It would be further appreciated that the object modeling of the present invention greatly simplifies object visibility determination. Once the proper image plane curves--accounting for intraobject surface visibility--are computed by the object processors, the interobject visibility is easily determined by the subframe processors based on the viewpoint parameters. Also, by ranking the objects in order of interobject visibility, and determining intensity levels for highest order objects before proceeding to second and third rank objects behind translucent first rank objects, the results of any overload will not be as distracting.
Another modification which is easily accommodated by the present system is a multiple level of detail model data base. Thus a group of objects, such as trees, may be represented by a single object for viewpoint parameters indicating a long range. As the range decreases, a bounding plane may be inserted between the high level of detail model (the individual trees) and the single object model, and moved back as the range decreases further. The high level of detail object closest to the bounding plane could be made translucent to merge into the low level of detail model.
Besides such scene control techniques, those skilled in the art will doubtless arrive at numerous modeling methods using quadric surfaces as disclosed herein. To a great extent, object modeling is as much an artistic as a scientific procedure, but the parameters used in the present CIG system offer great potential for automated modeling process, as well as being more descriptive than abstract in nature. As pointed out, texture parameters may be derived by Fourier analysis of actual objects (clouds, water, sand, trees, etc.). Statistical analysis should also prove useful in reducing major terrain features to quadric surface models. For instance, digitizing low pass filtering of the Defense Mapping Agency (DMA) elevation data for a desired model region can be used to isolate major terrain features, which may then be scaled and fit to appropriately shaped quadric surfaces. Once the geographic region of which the visual images are to be simulated has been modeled in gross with respect to elevation data, DMA cultural data may be used to generate further quadric surfaces, bounding planes and texture parameters corresponding to solid surface objects typically found in the region. DMA cultural data includes such information as percent tree and roof cover; location of buildings, bridges and other surface features; and predominant height and surface material of such features. By constructing a library of detailed generic features and referring to the DMA cultural data, then, appropriate features can be added to the major terrain features to complete the scene model.
It will be noted that the techniques and system of the present invention may be easily adapted to accommodate moving models and dynamic features such as smoke, dust clouds or tree foliage. As noted above, moving models may be implemented by changing the associated objects' location and orientation parameters as the model moves through the scene. With regard to dynamic models varying of the texture parameters for each models' associated objects may be done in a predetermined manner to simulate the desired motion or agitation of the associated texture patterns, e.g., drifting smoke or wind-blown tree foliage. Preferably, control of moving and dynamic models is by the mainframe computer. Thus, the desired motion may be implemented by simply reassigning an updated object list to the same object processor, the updated list including the appropriately altered orientation, location or texture parameters.
Although a stated object of the present invention is the provision of a system capable of producing dynamic images in real time, it will be appreciated that the various modeling and surface rendering techniques described herein may be applied to static image generation and off-line dynamic image generations as well. For off-line systems, the parallel architecture discussed above is not necessary. In fact, with no stipulation that the system work in real time, all object projection calculations and pixel generation could be performed sequentially by the mainframe computer.
TABLE C (Appendix A) shows a documented source code listing (FORTRAN and assembly language) designed to enable a Data General Eclipse S250 computer to perform the functions of mainframe 18, object processors 24, and subframe processors 28 (FIG. 1) in an off-line system. Prior to execution of the image generation program, object lists and other inputs are prepared in ASCII format and loaded into a magnetic disc bulk memory device. The object lists are stored in a SCENE file. Texture parameters for up to 28 texture patterns are stored in file TEXT, keyed to directory parameters in the SCENE file. A third input file, EYEPTS, stores a desired series of viewpoint parameters including an updated set of parameters for each frame of imagery to be generated. The viewpoint parameters may be generated prior to execution of the offline image generation program, or may be supplied from a keyboard or other interactive input device during program execution.
As will be noted from the documentation included in TABLE C, the SCENE file contains, in addition to object lists, inputs related to a light vector, ambience, ground plane texture and color, and sky texture and color. Thus, the first three words in the SCENE file are x, y and z coordinates indicating the direction of illumination (sunlight or moonlight). The next SCENE entry indicates the intensity of ambient light, and falls within a range from 0 (no ambience) to 1 (all objects white). The fifth and sixth SCENE words are, respectively, a surface sampling factor and a hyperboloid surface translucence factor, normally set to 0.5 and 0.05 respectively. The surface sampling factor is used to position intensity sample points within the surface image for computing surface shading. Using a smaller value for the hyperboloid translucence factor proportionally reduces the translucence limit for all hyperboloid surfaces.
The next twelve words in the SCENE file relate to color and texture of the ground plane and sky. Specifically, word seven is a factor used to weight the ground plane texture, and words 8-10 are the red, green and blue color intensities for the ground plane. Words 11 and 12 are not used. Word 13 is a sky texture fractional weight, similar to the ground plane texture weight. Word 14 is an arbitrarily chosen distance to a sky plane from the ground plane, the sky plane being an artifice for modeling sky color and cloud texture. Words 15-17 are the red, green and blue intensities from the sky plane. Word 18 is used to input a sky intensity or luminosity, since no ambient or reflected light will be emitted from the sky plane. Like the ambience, scene scaling and hyperboloid translucence input the ground and sky texture weighting inputs are scaled from 0 (no texture) to 1 (full texture). All color inputs are scaled from 0 to 255. Following the sky plane parameters, (i.e., beginning at SCENE word 19), is an input indicating the number of objects in the scene model.
The actual object lists begin at SCENE word 20. The first word in each object list is the texture pattern number, identifying one of the up to 28 sets of texture function parameters in the TEXT file. Following the texture pattern number are the percent texture weight (0-1), the translucence limit (0-1), and the red, green and blue color components (0-255) for the object. The next inputs in each list are object shape parameters, prefixed by an entry indicating the number of bounding planes. Four parameters follow the number of bounding planes and describe the quadric surface shape and size with respect to the object axes (i.e., without regard to the object's orientation or location within the scene). To simplify the modeling of a hyperboloid, its object axes are defined with respect to a base plane intersecting the lower sheet, rather than with respect to the lower sheet vertex. (The base plane may or may not also be a bounding plane). For both ellipsoids and hyperboloids, then, the two SCENE words following the number of bounding planes for the object are linear measurements along the object's x and y axes from the object origin to the quadric surface. Two further words relate to the object's z axis. For ellipsoids, the first is the linear measure from the origin to the surface, and the second z entry is always 0. For hyperboloids, the first entry is the measure from the vertex of the bounding cone to the lower sheet vertex, and the second z entry is the distance from the object origin to the bounding cone vertex. The "sharpness" of the hyperboloid is thus determined by the third hyperboloid parameter (set to 0 for a cone), and its height by the fourth parameter (non-zero only for hyperboloids).
Following the quadric shape parameters is an x displacement entry which allows objects to be moved along the reference scene x axis. For stationary objects, the x displacement input would be set equal to zero.
Six SCENE words relate the orientation and location of the object axes within the scene. Specifically, the roll, pitch and yaw of the object axes in degrees with respect to the reference axes comprise the object orientation parameters, and are followed by the x, y and z displacement location parameters.
Seven SCENE words for each associated bounding plane follow the object's quadric surface information. The first SCENE word for each plane identifies the type of plane--�1 for an exposed, potentially visible surface; �2 for a limiting surface (i.e., one which eliminates a hyperboloid sheet without actually intersecting the hyperboloid); and �3 for a hidden surface (e.g., the base plane of a mountain peak). The sign of the first parameter for each bounding plane identifies the inequality relation ○R for that plane--negative for ≦, positive for ≧.
The six parameters following the plane type are used to describe the position of the plane with respect to the reference system x-y ground plane, and describe the roll, pitch, and yaw (in degrees) and x, y, and z displacement necessary to move the bounding plane to its desired orientation location (from the ground plane position). It will be appreciated that only three of the available variables are ever necessary to position a plane; however, since the plane is positioned with respect to the ground plane rather than the object axes, the use of redundant ground plane positioning inputs simplifies object modeling.
The TEXT file, as indicated, includes parameters defining up to 28 texture patterns in accordance with the texture function described earlier. Each of the patterns may thus be referenced in the object lists in the SCENE file by an integer from 1 to 28. The parameters for the first pattern begin at TEXT word 7, and are followed in order by the parameters for the successively numbered patterns.
The first TEXT word for each pattern indicates the number of sine wave terms in the x and y directions, and is an integer from 1 to 7. The same number of spatial frequencies are used in both directions--that is, m and n from the texture function equation above are identical for a given texture pattern. The second TEXT entry for each pattern is an offset factor, normally having a value in a range from 0 to 5. The offset factor affects the mixture contrast--a lower value gives a higher contrast but results in clipping when the texture function yields a negative value.
The third, fourth and fifth TEXT words for each texture pattern relate to the translucence limit described earlier. The first translucence parameter establishes the base threshold for which complete translucence results when the texture function returns a lower value. The second parameter designates a range above the base threshold for which a variable translucence limit is to be computed; thus, setting the first and second translucence parameters to a common value results in a constant translucence limit for all objects textured by the associated texture pattern. The third translucence parameter relates to the variable translucence range and indicates a weight for the variable translucence limit. All of the translucence parameters have a normal range between 0 and 1.
Following the translucence parameters for each texture pattern in the TEXT file are the weighting factors Cx (up to seven, as indicated above), in turn followed by a like number of spatial frequencies wx. The weights will have a normal range of 0-1, while the range of the spatial frequencies will depend on the desired texture and the magnitude of spatial units used. If fewer than seven frequencies are used, 0 inputs should be used for the unused weights and frequencies. Only the x coordinate weights and frequencies are actually specified as inputs, the y weights and frequencies and the various phase shift factors being derived from the x weights and frequencies in accordance with four additional inputs following the x frequencies for each pattern.
Specifically, the first TEXT word following each pattern's x frequencies is a factor by which each x frequency is multiplied to obtain an associated y dependent x coordinate phase shift frequency (φx). The next entry is used directly as the phase shift weighting factor (J and K) for all x, y and z dependent phase shift frequencies. Following the phase shift weighting factor input is a factor by which each x frequency is multiplied to yield an associated y frequency. The resulting y frequencies, in turn, are used to generate x dependent y coordinate phase shift frequencies using the same input (i.e., the first TEXT word following the x frequencies) used to generate the x phase shift frequencies. Finally, the fourth input following the x frequencies is used to derive a single common z dependent phase shift frequency (for all ψx 's and ψy 's) by dividing by the first x frequency.
Two further inputs control the x and y offsets for the scene coordinate arguments to the texture function, and may be used to move the patterns parallel to the ground plane. It will be noted that the ninth texture pattern moves 200 spatial units in the x direction for every frame, in accordance with the statement four lines from the end of subroutine BPM1 in TABLE C.
The first four entries in the TEXT file are texture dynamics parameters which allow a designated one of the frequencies of a designated one of the texture patterns to be varied so as to simulate agitation of the texture pattern. The first TEXT word designates the affected frequency, and is set to an integer from 11 (for the first frequency) to 17 (for the seventh frequency). The second TEXT word identifies the texture pattern to be agitated (1-28). The third word dictates the weight of a dynamic offset factor to be added to the affected frequency, and will normally have a range similar to the affect frequency. The fourth texture dynamics parameter is a time period, in frames, for the repeated dynamic perturbation.
Those skilled in the art will appreciate that by entering an integer between 18 and 24 (for TEXT word 1), an agitation in the designated texture pattern (TEXT word 2) will be manifested as a periodic change in the magnitude rather than the spatial frequency of the pattern. Similarly, inputting a 1-10 will agitate the base translucence threshold (1), the variable translucence range (2), the weight of variable translucence (3), the x and y offsets (4, 5), the texture contrast (6), the phase shift magnitude (7), the z dependent phase shift frequency (8), the x to y frequency ratio (9); or the x-y phase shift frequency ratio (10). In each case, the third TEXT input (weighting factor) must be adjusted to an appropriate range.
The fifth entry in the TEXT file indicates the number of texture patterns. The sixth word is an antialias cutoff frequency input used to weight the Nyquist period for the projected patterns and having a range from 0 (all texture frequencies suppressed) to 1 (only frequencies greater than the Nyquist frequency suppressed).
Three input words precede the actual viewpoint parameters in the EYEPTS file. The first is the number of frames or viewpoints to be processed. The second EYEPTS entry is the distance from the focal point to the image plane (f), and the third entry is a zoom factor, normally set to one, which may be set to 2, 4 or 8 to proportionally magnify the image plane.
Following the zoom factor input are the viewpoint parameters, in six words for each viewpoint corresponding to roll, pitch, and yaw (in degrees) of the observer line of sight from the y reference axis and image plane h and v axes from the x and z reference axes and x, y and z displacement of the observer focal point from the reference origin. It will be noted that all six inputs are necessary, since not only the focal point and line of sight must be positioned, but the image plane rotation (pitch) must be specified as well.
Most of the subroutines and functions utilized by the program of TABLE C but not listed therein are standard system routines familiar to those skilled in computer programming. TABLE D (Appendix B) lists examples of file rewind, byte pack and unpack, read, bit operations, screen clear, video disc driver, and other routines which may be used with the program of TABLE C. All of the listings of TABLES C and D are compatible with a Data General Eclipse S250 and a Genisco GCT 3000 digital frame buffer, which may in turn be interfaced with any standard magnetic video disc drive to record the generated images on standard video tape.
Those skilled in the art will appreciate that interfacing a given computer with a particular digital frame buffer generally requires the development of special software. Hence the system routines of TABLE D are not applicable to other frame buffers in general.
In view of the various modifications which may be made in the present inventive system, the scope of the invention is to be interpreted only by the appended claims. ##SPC1##
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|U.S. Classification
|345/420, 345/427, 345/421, 348/123, 345/643, 345/582, 434/43
|International Classification
|Cooperative Classification
|European Classification
|Jun 27, 1983
Owner name: GRUMMAN AEROSPACE CORPORATION BETHPAGE,NY A CORP.
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNORS:BERLIN, EDWIN P. JR.;GARDNER, GEOFFREY Y.;GELMAN, ROBERT M.;AND OTHERS;REEL/FRAME:004149/0490;SIGNING DATES FROM 19830615 TO 19830622
|Aug 14, 1990
|Certificate of correction
|Nov 2, 1990
|Fee payment
Year of fee payment: 4
|Nov 14, 1994
|Fee payment
Year of fee payment: 8
|Jan 19, 1999
|Maintenance fee reminder mailed
|Jun 27, 1999
|Lapse for failure to pay maintenance fees
|Sep 21, 1999
|Expired due to failure to pay maintenance fee
Effective date: 19990630