KR100937051B1 - Three-dimensional image output system having a large number images for an object - Google Patents

Abstract

PURPOSE: A 3D map display system using a plurality of aerial photographing images is provided to immediately check a side image about a specific area that a user selects in a digital map, thereby obtaining side image information. CONSTITUTION: A data integration managing unit(400) comprises the following units. A data receiving module(410) receives photographing image data. An edition updating module(420) edits planar information to be identified. An input module(450) inputs a control signal. A GPS coordinate associating module(490) combines GPS coordinate systems based on the planar information.

Description

Three-dimensional image output system having a large number images for an object}

The present invention relates to a three-dimensional stereoscopic map display system using a plurality of aerial photographs.

Advances in photography and aviation have had a significant impact on photorealistic mapping. In other words, the plane can be taken in the vertical direction and the GPS coordinate information is applied to the photographed image to create a realistic numerical map.

However, since the digital map photographs the ground in the vertical direction in the aircraft, the digital map user has no choice but to check the plane of the feature. However, the user has no experience in seeing the feature of the feature of the feature, and only grasps the numerical map by associating the feature of the feature and the layout of the feature, so the image of the plane is photographed by the elderly with low spatial perception and cognitive ability. It was difficult to see and understand the baseline digital map and apply it to the actual terrain.

In addition, since the heights of the flat features are all seen to be the same, the users of the numerical map familiar with the area had a lot of inconvenience in understanding the numerical map without the altitude information.

Accordingly, the present invention has been made to solve the above problems, the user can check the plane image as well as the side image of a specific area through the digital map, it is easy to understand the surrounding area, through this It is a technical task to provide a three-dimensional stereoscopic map display system using a plurality of aerial photographs that can maximize the convenience of using a digital map.

The present invention to achieve the above technical problem,

First, second, and third cameras 121, 122, and 123; The reference base 111 for fixing the first camera 121 and the rotating bases 112 and 112 'for fixing the second and third cameras 122 and 123, respectively, and the reference base 111 are fixed to the center. The pair of pivoting tables 112 and 112 'is fixed to both ends so that the first, second, and third cameras 121, 122, and 123 are arranged in a row, and the reference table and the reference table. Screw 114, which is rotatably mounted on the base 111, and a trapezoid-shaped guide 115 formed side by side on the pivoting tables 112 and 112 ', respectively, so that the distance between one surface facing each other is gradually narrowed downward. , 115 'and a presser 116 formed at the center of the nut portion 116a through which the screw 114 is engaged, and both ends slidably engaged with the one surface of the guides 115 and 115'. One support frame 110; The appliance part 100 of the drive motor 130 which provides power for the rotation of the screw 114:

A screw counter 210 for counting the number of revolutions of the screw 114; The second and third cameras 122 and 123 of the second and third cameras 122 and 123 are provided through the moving distance of the pressing table 116 and the length L1 of the pressing table 116 according to the rotation speed of the screw 114 input from the screw counter 210. A photographing angle calculation module 220 programmed to calculate a photographing angle θ1 and installed in a computer; A GPS receiver 270 for detecting GPS coordinates; A GPS identification module 230 programmed to receive the GPS coordinates from the GPS receiver 270 and confirm the current position of the aircraft A and installed in the computer; Positioning module 240 is programmed to receive and confirm the altitude (H) of the aircraft (A) while communicating with the air measurement unit 300 is installed on the computer; Receiving the GPS and shooting angle (θ1) information of the shooting area from the GPS checking module 230 and the shooting angle calculation module 220, the corresponding shooting image data transmitted from the first, second, and third cameras 121, 122, and 123. The first, second, and third cameras 121, 122, and 123 are the same by calculating the altitude H checked by the positioning module 240 and the shooting angle θ1 checked by the shooting angle calculation module 220. A data classification module 250 that checks the moving distance D of the aircraft A to capture the point, and is programmed to store the captured image data based on the moving distance D and installed in the computer; Computational unit 200 of the data communication module 260 is programmed to receive the captured image data from the data classification module 250 to be transferred to the following data integration management unit 400 is installed on a computer:

Aircraft measurement unit 300 of the altitude measuring instrument 330 for measuring the altitude (H) of the aircraft (A), and transmits the altitude (H) measured by the positioning module 240: And

The data receiving module 410, which is programmed to receive the captured image data from the data communication module 260 and installed in the computer, separates the captured image data into side photographed image data and planar photographed image data, and receives new photographed image data. In case of updating the data stored in the side image image database 430 and the plane image image database 440, the editing update module 420 is installed to the computer is programmed to edit the settable information for each structure included in the image image for identification And a side photographing image database 430 and a planar photographing image database 440 which respectively store side photographing image data and planar photographing image data, and are programmed to be input to a control signal by a user's input device. Input module 450 and input module 450 The control module 470 is programmed to control the operation of the following search module 480, GPS coordinates connection module 490 and output module 460 according to the input control signal and installed on a computer, and the side image image database 430 And a search module 480 for searching the data of the planar photographing image database 440, and a GPS coordinate system on the photographed image of the photographed image data searched by the search module 480 based on the GPS coordinates included in each photographed image data. Synthesis and application is performed, but the GPS coordinate linkage module 490 installed in the computer is programmed to synthesize the GPS coordinate system based on the plane information set for each structure, and the GPS coordinates and the photographed image are synthesized and output through the output device. Data integration management unit 400 of the output module 460 is programmed to be installed on the computer:

It is a three-dimensional stereoscopic map display system using a plurality of aerial photography including a.

According to the present invention, the side image of the specific area selected by the user can be immediately confirmed on the digital map, and the collective image can be secured in one operation without having to perform a plurality of photographing operations in order to secure the side image information. Therefore, there is an effect of minimizing the occurrence of additional costs for producing a more effective and efficient digital map.

Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.

1 is a view schematically showing a photographing image applied to the present invention, Figures 2 and 3 is a view schematically showing the appearance of aerial photography based on the display system according to the present invention, with reference to this description do.

FIG. 1 (a) illustrates a plane photographing image of the first camera 121 installed in the aircraft A to photograph the ground in the vertical direction, and FIG. 1 (b) shows the aircraft (the photographed laterally toward the ground). A side photographed image of the second and third cameras 122 and 123 installed in A) is illustrated.

In order to photograph the specific building B, which is the photographing point of the first camera 121, with the second and third cameras 122 and 123, the aircraft A is vertically upward of the building B as shown in the drawing. In the first position S1, it must move to the second position S2 or the third position S3 that is laterally.

In addition, in order to arrange the first, second, and third positions S1, S2, and S3 in a line with respect to the building B, the first, second, and third cameras may be arranged in a direction parallel to the traveling direction of the aircraft A. Must be fixed to the support frame 110 so that 121, 122, 123 are disposed.

Here, the support frame 110 is to fix the first, second, third, cameras 121, 122, 123 to the aircraft A, the structure and operation details will be described in more detail below.

As can be seen in Figure 1 (b), the photographed image taken sideways shows the side of the feature including the building (B). In other words, it is possible to check the height of the feature, and furthermore, when the resolution is high, the appearance of the feature familiar to the user can be distinguished. Therefore, when the user cannot understand the terrain in the planar photographing image, the side photographing image of the same point can be output, so that the numerical map can be easily analyzed and utilized.

On the other hand, the side-shooting of the feature is taken even if the altitude and position (S1, S2, S3) of the aircraft A are the same, depending on the shooting angle (θ1) of the second and third cameras 122 and 123, but the other area is taken. Can be. Therefore, the display system according to the present invention can grasp the information on the area photographed by the second and third cameras 122 and 123 relative to the photographing angle θ1 of the second and third cameras 122 and 123. Should be

In addition, the aircraft A may not only travel in a straight line but also turn at a constant turning angle θ2 as shown in FIG. 3 to fly in a different direction, regardless of the turning angle θ2. The information about the area photographed by (122, 123) should also be known accurately.

To this end, the display system according to the present invention checks the current altitude H and the moving distance D of the aircraft A, and the photographing angles θ1 of the second and third cameras 122 and 123, thereby providing a constant altitude H. When the aircraft A operates the travel distance (D) calculated in), the second and third cameras 122 and 123 automatically control to photograph the ground. That is, if the current aircraft A altitude H and the shooting angles θ1 of the second and third cameras 122 and 123 are checked, the second and third cameras 122 and 123 may operate at the moment when the aircraft should operate. It can calculate from the moving distance D of (A).

Of course, the second and third cameras 122 and 123 perform continuous shooting (including video shooting) regardless of the moving distance D of the aircraft A, but the moving distance D when classifying the collected side photographing images. ), It may be classified by taking into consideration the altitude (H) and the shooting angle (θ1), and then linked with the planar photographed image of the same area.

The operation of the display system according to the present invention will be described in detail below with reference to a block diagram.

Figure 4 is an exploded perspective view showing a state of the support frame according to the present invention, Figure 5 is a front view showing the operation of the support frame according to the present invention, will be described with reference to this.

In the support frame 110 according to the present invention, the first, second and third cameras 121, 122, and 123 are rotatably fixed to the aircraft A, and the display system of the second and third cameras 122 and 123 is rotated. It is to be able to accurately grasp the operation state, the reference base 111 for fixing the first camera 121 floating, and the rotating table 112 for fixing the second and third cameras 122, 123 rotatably, respectively. 112 '), and the first, second, and third cameras 121, 122, and 123 are fixed in a row through the reference table 111 and the rotating tables 112 and 112', but the rotating tables 112 and 112 'are Guides (113, 113 ') rotatably fixed, screws (114) rotatably mounted on the reference table (111), and trapezoidal guides (10) mounted on each of the pivots (112, 112'). (115, 115 ') and the pressing table (116) which is slidably engaged with the guide (115, 115'), respectively, while moving up and down along the screw (114).

As shown, the first, second, and third cameras 121, 122, and 123 are suspended to photograph downward, and the performance may vary depending on the shooting purpose.

The second and third cameras 122 and 123 disposed at both ends of the edges of the first, second and third cameras 121, 122 and 123 installed in this way rotate to face each other. That is, when the photographing angle θ1 of the second camera 122 faces the first camera 121 at 30 degrees, the photographing angle θ1 of the second camera 122 faces the first camera 121 at the photographing angle −30 degrees of the third camera 123. To this end, the first and second cameras 121, 122, and 123 are connected to the reference base 111 and the pivoting bands 112 and 112 'in a row, the fixing bases 113 and 113', and the reference base 111. ) And a screw 114 and a guide 115, 115 ′ mounted on each of the rotating table 112 and 112 ′, and a pressing table 116 engaged with both ends of the guide 115 and 115 ′.

As shown in FIG. 5, the pressure bar 116 includes a nut portion 116a having a pitch that is engaged with the pitch of the screw 114, and the screw through the engagement of the screw 114 and the nut portion 116a. Along the 114 it is configured to move up and down. At this time, the screw 114 is rotated by the rotational force of the drive motor 130 via the reducer 140, and the lifting and lowering of the pressure table 116 will be determined according to the rotation direction.

On the other hand, when the drive motor 130 rotates in the direction of lowering the pressing table 116, the pressing table 116 moves downward along the screw 114 as shown in Figure 5 (b). At this time, one surface of the guide (115, 115 ') that both ends of the presser 116 is engaged with each other is formed to be inclined downward, so that the interval between the guide (115, 115') is narrowed. On the other hand, since the pressing bar 116 maintains its original length when lifting up and down, the guides 115 and 115 'are forced outward as the pressing bar 116 moves downward. Of course, this force is located at the bottom of the fixing pins (112a, 112a ') to space the guides (115, 115') apart from each other, and to pivotally secure the pivot (112, 112 ') and the fixing (113, 113'). The second and third cameras 122 and 123 rotate at the same photographing angle θ1 toward the first camera 121.

Unexplained withdrawal number '111a' refers to the 'fixing pin' for fixing the reference base 111 and the fixing base (113, 113).

Here, the photographing angles θ1 of the second and third cameras 122 and 123 are the intervals L2 and L2 'between the pressing table 116 and the fixing tables 113 and 113' relative to the length L1 of the pressing table 116. Can be calculated as In this case, the intervals L2 and L2 'may be calculated based on the rotation speed of the screw 114. For this purpose, the display system according to the present invention includes a screw counter 210 for counting the rotation speed of the screw 114; 6).

In more detail, through the pitch and the structure of the pitch, the movement distance of the pressing table 116 to linearly move by the rotation of the screw 114 can be set. In other words, when the screw 114 is rotated two times, the presser 116 may move 1 mm or more or less than 1 mm. As a result, when the screw counter 210 counts the number of revolutions of the screw 114, it is possible to calculate the moving distance of the pressure table 116 according to the set content, through which the gap (L2, L2 ') can be confirmed. have. In addition, the photographing angles θ1 of the second and third cameras 122 and 123 are calculated through the checked intervals L2 and L2 ', and the strings of the aircraft A are measured using the photographing angles θ1 calculated as described above. The movement distance D from the altitude H to the second and third positions S2 and S3 corresponding to the first position S1 may be checked.

FIG. 6 is a block diagram illustrating a configuration of a display system according to the present invention, and FIG. 7 schematically illustrates a numerical map image by the display system according to the present invention.

The display system according to the present invention includes a device unit 100 and a computer unit 200, the computer unit 200 is to operate in conjunction with the aviation measurement unit 300 installed in the aircraft (A).

The device unit 100 includes a support frame 110, cameras 121, 122, and 123 (hereinafter, 120), a driving motor 130, and a speed reducer 140.

Since the description of the device unit 100 has been described above, the description thereof is omitted here.

The computer unit 200 includes a screw counter 210 for counting the number of revolutions of the screw 114 and the second and third cameras 122 and 123 according to the number of revolutions of the screw 114 counted by the screw counter 210. Receiving GPS coordinates from the shooting angle calculation module 220 for calculating the shooting angle θ1, the GPS receiver 270 for detecting the GPS coordinates, and the GPS receiver 270 to check the current position of the aircraft A. The GPS identification module 230, and the positioning module 240 for confirming the current state of the aircraft (A) while communicating with the air measurement unit 300, and classifies the photographed image for the same area taken by the camera 120 And a data communication module 260 for storing the captured image data classified by the data classification module 250 to the integrated data management unit 400 located on the ground. At this time, the modules 220, 230, 240, 250, 260 constituting the computer unit 200 is a device composed of software programmed for the task and hardware (computer) applied to drive the software, each module Software and hardware (computer) of (220, 230, 240, 250, 260) can be applied to the known technology for the operation, through which those skilled in the art can easily implement the present invention in the detailed description.

On the other hand, the aviation measurement unit 300 installed for the operation of the aircraft (A) is a direction measuring instrument 310 for detecting the turning angle (θ2) of the aircraft (A), and the tilt sensor for detecting the horizontal state of the aircraft (A) And an altitude meter 330 for measuring the altitude of the aircraft A. The aviation measurement unit 300 is for reference to the shooting operation affected by the operating state of the aircraft (A), the information provided from the aviation measurement unit 300 is whether the utilization of the photographed image taken by the camera 120 And criteria for classification.

For reference, the information of the air measurement unit 300 is recorded as data, such as a black box of the aircraft (A), the positioning module 240 according to the present invention to check the corresponding data transmitted to the black box from the air measurement unit 300 Can be. In addition, the positioning module 240 may be set to check the data of the air measurement unit 300 delivered to the digital aeronautical instrument board, to confirm the corresponding data.

The operation of the display system according to the present invention will be described in sequence.

1. The photographer sets the photographing angle θ1 of the second and third cameras 122 and 123 before the photographing operation using the camera 120.

The setting of the photographing angle θ1 is performed by controlling the driving motor 130 of the operator. That is, when the operator operates the drive motor 130, the rotational force of the drive motor 130 is transmitted to the screw 114 through the reducer 140, and the rotation of the screw 114 moves the press table 116. In this case, the second and third cameras 122 and 123 are rotated.

On the other hand, the screw counter 210 counts the number of revolutions of the screw 114, according to the set angle photographing operation module 220 is the interval (L2, L2) between the pressing table 116 and the fixing table (113, 113 ') Calculate '). As described above, the length L1 of the pressing table 116 is a fixed value, and the intervals L2 and L2 'between the pressing table 116 and the fixing tables 113 and 113' are variable values, but the screw 114 is fixed. Since the variable value can be known by the number of revolutions, the photographing angle calculation module 220 can accurately calculate the photographing angles θ1 of the second and third cameras 122 and 123.

2. The positioning module 240 checks the flight measurement unit 300 from time to time while checking the operating state of the aircraft (A) in real time, and according to the confirmed operating state to determine whether to drive the camera 120 or the camera 120 ) Determines whether to use the captured image or classifies the captured image.

In the embodiment according to the present invention will be described that the camera 120 automatically executes a continuous shooting operation at a predetermined interval.

3. The camera 120 proceeds the shooting operation at a predetermined interval (including video recording), and the data classification module 250 is the shooting time, the shooting area GPS, aviation measurement unit 300 in the captured image data output Enter the information and the photographing angle (θ1) confirmed in.

4. Even when all aerial photographing work is completed or aerial photographing, the data classification module 250 proceeds to classify photographed image data for the same region.

As described above, in order to classify the photographed image data of the first camera 121 photographing the same region as the photographing region of the second and third cameras 122 and 123 photographing the side surface of the feature, the photographing angle θ1. The travel distance D of the aircraft A corresponding thereto is required.

Of course, since the aerial shooting is taken at an altitude H within the error range, the data classification module 250 uses the fixed altitude H and the shooting angles θ1 of the second and third cameras 122 and 123. The movement distance D of the aircraft A, which is the position of the second and third cameras 122 and 123, which may photograph the same region as the first camera 121, may be calculated.

As a result, the data classification module 250 captures images captured at intervals of the moving distance D among photographed images photographed by the first camera 121 and photographed images photographed by the second and third cameras 122 and 123. Images will be considered to photograph the same area and will be grouped together. For reference, the moving distance D for the captured image may be calculated through the GPS coordinates included in the captured image data.

Meanwhile, as shown in FIG. 3, the aircraft A travels in a direction parallel to the first, second, and third cameras 121, 122, and 123 arranged in a row, and the second position S2 from the first position S1. It may also move to a different turning position (θ2), may move from the first position (S1) to another second position (S2 '). In this case, if the building B photographed by the first camera 121 and the moving distance D which is a horizontal straight line distance of the operated aircraft A coincide, the second and third cameras 122 and 123 are the same. You can classify it as taking a picture of building (B).

In other words, it is possible to easily create a digital map that allows a user to check various aspects of a particular feature. In addition, even a single aerial shot is expected to secure economical production of digital maps with abundant information by securing various side photographs of the features located on the ground.

5. When the captured image data is classified, the data communication module 260 transmits the classified captured image data to the data integrated management unit 400.

Hereinafter, the integrated data management unit 400 will be described in detail with reference to FIG. 6.

Integrated data management unit 400 is a data receiving module 410 for receiving the photographed image data transmitted from the data communication module 260, and the photographed image data received by the data receiving module 410 side photographed image data and plane photographing When the new image data is received and the new image data is received, the corresponding data stored in the side image image database 430 and the plane image image database 440 are updated. The control update module 420, the side photographing image database 430 and the plane photographing image database 440 which store the side photographing image data and the planar photographing image data, respectively, and the control signal by the user's input device manipulation. In accordance with the input module 450 and the control signal input to the input module 450, the following search module 480 and GP A control module 470 for controlling operations of the S coordinate linking module 490 and the output module 460, and a search module 480 for searching data of the side photographing image database 430 and the planar photographing image database 440. And a GPS coordinate system synthesized and applied to the captured image of the captured image data retrieved by the search module 480 based on the GPS coordinates included in each captured image data, but synthesized the GPS coordinate system based on the plane information set for each structure. The coordinate linking module 490 and an output module 460 for outputting the completed digital map by combining the GPS coordinates and the photographed image through the output device. In this case, the modules 410, 420, 450, 460, 470, 480, and 490 constituting the data integration management unit 400 are software programmed for a corresponding task and hardware (computer) applied to drive the software. With the device configured, the software and hardware (computer) of each module 410, 420, 450, 460, 470, 480, 490 can be applied to the known technology for the corresponding operation, and thus those skilled in the art will see The invention can be easily carried out.

For reference, the input device may be a conventional keyboard or various buttons and the like, and the output device may be a conventional monitor or the like.

The data receiving module 410 may wirelessly receive photographed image data in real time from the data communication module 260 of the computer unit 200, and after receiving the photographed image, receives the photographed image data stored in a separate storage medium. You might get it.

The editing update module 420 manages data of the side photographing image database 430 and the planar photographing image database 440 storing the photographed image data, and the side of the photographed image data input through the data receiving module 410. When it is determined that the image data is different from the photographed image data stored in the photographed image database 430 and the planar photographed image database 440, the operation of updating the photographed image database 430 and the planar photographed image database 440 is performed.

In reality, since the digital map maker will use the aircraft A for aerial photography where the topographical change has occurred, the producer manipulates the editing update module 420 to produce the side photographing image database 430 and the planar photographing image database 440. Will be updated directly.

The updated side photographing image database 430 and the planar photographing image database 440 may provide a digital map of the terrain required by the user.

In more detail, when the user inputs the relevant information of the area P that the user wishes to operate the input module 450, the control module 470 operates the search module 480 to display the planar photographing image database. In operation 440, the GPS coordinate link module 490 synthesizes the corresponding GPS coordinate system to the found photographed image and outputs the synthesized GPS coordinate system through the output module 460. In this case, the GPS coordinate system will be synthesized based on the area P.

On the other hand, if the user wants to see the side view of the area (P), the search module 480 searches the side photographing image database 430, the GPS coordinate link module 490 is the area (P) in the retrieved photographed image The GPS coordinate system is synthesized and applied based on), and is output through the output module 460. At this time, the area (P) is set to the plane of any structure (building B). This applies to the principle that the plane must be visible even if the side view of the structure is visible, and the plane information is set for each of the structures included in the side photographing image and the plane photographing image, so that the GPS coordinate link module 490 displays the plane information. GPS coordinate system can be applied as a standard. Here, the plane information will include GPS coordinates.

As a result, the GPS coordinate system is accurately synthesized even in the plane image and the side image image having a large overall image difference, so that the user can always use the digital map by checking the accurate GPS coordinate regardless of image change.

1 is a view schematically showing a photographed image applied to the present invention,

2 and 3 is a view schematically showing the appearance of aerial photography based on the display system according to the present invention,

Figure 4 is an exploded perspective view showing a state of the support frame according to the present invention,

5 is a front view showing the operation of the support frame according to the present invention,

6 is a block diagram showing the configuration of a display system according to the present invention;

7 is a view schematically showing a digital map image by the display system according to the present invention.

Claims (1)

First, second, and third cameras 121, 122, and 123; The reference base 111 for fixing the first camera 121 and the rotating bases 112 and 112 'for fixing the second and third cameras 122 and 123, respectively, and the reference base 111 are fixed to the center. The pair of pivoting tables 112 and 112 'is fixed to both ends so that the first, second, and third cameras 121, 122, and 123 are arranged in a row, and the reference table and the reference table. Screw 114, which is rotatably mounted on the base 111, and a trapezoid-shaped guide 115 formed side by side on the pivoting tables 112 and 112 ', respectively, so that the distance between one surface facing each other is gradually narrowed downward. , 115 'and a presser 116 formed at the center of the nut portion 116a through which the screw 114 is engaged, and both ends slidably engaged with the one surface of the guides 115 and 115'. One support frame 110; The appliance part 100 of the drive motor 130 which provides power for the rotation of the screw 114: A screw counter 210 for counting the number of revolutions of the screw 114; The second and third cameras 122 and 123 of the second and third cameras 122 and 123 are provided through the moving distance of the pressing table 116 and the length L1 of the pressing table 116 according to the rotation speed of the screw 114 input from the screw counter 210. A photographing angle calculation module 220 programmed to calculate a photographing angle θ1 and installed in a computer; A GPS receiver 270 for detecting GPS coordinates; A GPS identification module 230 programmed to receive the GPS coordinates from the GPS receiver 270 and confirm the current position of the aircraft A and installed in the computer; Positioning module 240 is programmed to receive and confirm the altitude (H) of the aircraft (A) while communicating with the air measurement unit 300 is installed on the computer; Receiving the GPS and shooting angle (θ1) information of the shooting area from the GPS checking module 230 and the shooting angle calculation module 220, the corresponding shooting image data transmitted from the first, second, and third cameras 121, 122, and 123. The first, second, and third cameras 121, 122, and 123 are the same by calculating the altitude H checked by the positioning module 240 and the shooting angle θ1 checked by the shooting angle calculation module 220. A data classification module 250 that checks the moving distance D of the aircraft A to capture the point, and is programmed to store the captured image data based on the moving distance D and installed in the computer; Computational unit 200 of the data communication module 260 is programmed to receive the captured image data from the data classification module 250 to be transferred to the following data integration management unit 400 is installed on a computer: Aircraft measurement unit 300 of the altitude measuring instrument 330 for measuring the altitude (H) of the aircraft (A), and transmits the altitude (H) measured by the positioning module 240: And The data receiving module 410, which is programmed to receive the captured image data from the data communication module 260 and installed in the computer, separates the captured image data into side photographed image data and planar photographed image data, and receives new photographed image data. In case of updating the data stored in the side image image database 430 and the plane image image database 440, the editing update module 420 is installed to the computer is programmed to edit the settable information for each structure included in the image image for identification And a side photographing image database 430 and a planar photographing image database 440 which respectively store side photographing image data and planar photographing image data, and are programmed to be input to a control signal by a user's input device. Input module 450 and input module 450 The control module 470 is programmed to control the operation of the following search module 480, GPS coordinates connection module 490 and output module 460 according to the control signal is installed on a computer, and the side photographing image database 430 And a search module 480 for searching the data of the planar photographing image database 440, and a GPS coordinate system on the photographed image of the photographed image data searched by the search module 480 based on the GPS coordinates included in each photographed image data. Synthesis and application is performed, but the GPS coordinate linkage module 490 installed in the computer is programmed to synthesize the GPS coordinate system based on the plane information set for each structure, and the GPS coordinates and the photographed image are synthesized and output through the output device. Data integration management unit 400 of the output module 460 is programmed to be installed on the computer: Three-dimensional stereoscopic map display system using a plurality of aerial photographs, characterized in that it comprises a.

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