KR102341610B1 - Image Processing System - Google Patents

Abstract

The present invention provides an image processing system for processing video images captured based on a GPS. The image processing system comprises: an image storage module (3100'); an image reception module (3200') for wirelessly receiving a video image taken; a coordinate synthesis module (3300') for synthesizing GPS coordinates with the received video image; and an image correction module for extracting differences by comparing the video image edited at the same magnification with an existing video image stored in advance. The coordinate synthesis module (3300') includes: a shape setting module (3310') for editing a video image received through the image reception module (3200') to match a shape and a standard; a reference point setting module (3320') for setting a reference point of the video image cut by the shape setting module (3310'); a comparison point setting module (3330') for setting a comparison point that can be relatively compared with the reference point set by the reference point setting module (3320'); and a coordinate checking module (3340') for checking actual GPS coordinates of the reference point and synthesizing the GPS coordinates with the video image based thereon. The video image received by the image reception module (3200') is obtained by a camera installed in a photographing unit, and the photographing unit includes a predetermined flight device (D). According to the present invention, it is possible to provide an image processing system that integrates and manages image information collected through a drone in real time by correcting changes in the image information immediately when a change part is detected.

Description

An image processing system that processes captured image images based on GPS

The present invention relates to an image processing system, and more particularly, when a changed part is detected in comparison with a collected image image and an existing image image, it integrates and manages real-time collected information through a drone that can correct it immediately. It relates to an image processing system that processes video images taken based on GPS including spatial image drawing update that can manage and operate the corresponding photographing means more effectively and accurately.

A technology is being developed to integrate and manage real-time collected information through drones that can correct image information data collected in real time through multiple photographing units with existing image information data, and then correct it immediately when a changed part is detected. However, in the photography-related part, which is the core of this technology, there is a large inefficiency in operation and management in providing the flying camera that is the means of the filming, and there are various deficiencies that can cause a large expenditure in stability, reliability and cost. There are problems that exist.

Republic of Korea Patent Registration No. 10-1006977

The problem to be solved by the present invention is to compare the image information data collected in real time through a plurality of shooting units with the existing image information data and then integrate and manage real-time collected information through a drone that can correct it immediately when a changed part is detected. It is to provide an image processing system for processing video images taken based on GPS.

In addition, in operating such a system, it is to provide an image processing system for processing a captured image image based on a GPS having a photographing means and various configurations that can guarantee the effective operation and reliability of the photographing means for photographing.

In addition, it is to provide an image processing system for processing a captured image image based on a GPS capable of imparting structural stability including earthquake resistance of elements related to photographing means and structural stability and durability.

In addition, through accurate check management in the operation of the photographing means, the video shot based on the GPS that can accurately and reliably manage the flight, the number of normal flights, return, non-return, and operation of the plurality of photographing means through accurate check management An image processing system for processing images is provided.

The problems of the present invention are not limited to the problems mentioned above, and other problems not mentioned will be clearly understood by those skilled in the art from the following description.

The present invention provides an image processing system for processing a captured image image based on an integrated management GPS, comprising: an image storage module (3100'); an image receiving module 3200' for wirelessly receiving the photographed image image; a coordinate synthesizing module 3300' for synthesizing GPS coordinates with the received video image; and an image correction module for extracting differences by comparing the edited image at the same magnification with the previously stored image image, wherein the coordinate synthesizing module 3300 ′ is received through the image receiving module 3200 ′. a shape setting module 3310' for editing a video image to match a shape and a standard; a reference point setting module (3320') for setting a reference point of the image image cut by the shape setting module (3310'); a comparison point setting module 3330' that sets a comparative point that can be relatively compared with the reference point set by the reference point setting module 3320'; and a coordinate confirmation module (3340') for confirming the actual GPS coordinates of the reference point and synthesizing the GPS coordinates with the video image based thereon; Including, the image image received by the image receiving module (3200') is obtained by a camera installed in the photographing unit, the photographing unit is a video image taken based on the GPS including a predetermined flight device (D) An image processing system for processing is provided.

The image processing system for processing the image image taken based on the GPS,

It includes a control unit in which the flight device (D) is operated, and the control unit includes a plurality of flying devices (D) and a mounting device (1000) on which a plurality of the flying devices (D) are mounted, the Mounting device 1000 includes a central guide module 1100 , a first structure 1200 provided on one side of the guide module 1100 , and a second structure 1300 provided on the other side of the guide module 1100 . ), the uppermost first mounting panel part 1210 horizontally installed from the first structure 1200 to the guide module 1100, and the guide module 1100 from the first structure 1200 horizontally installed A first mounting panel module including a second mounting panel part 1220 in the middle, and a third mounting panel part 1230 at the lowermost end horizontally installed from the first structure 1200 to the guide module 1100 and , a fourth mounting panel part 1310 at the uppermost level installed horizontally from the second structure 1300 to the guide module 1100, and the lowermost end horizontally installed from the second structure 1300 to the guide module 1100 A second mounting panel module including a fifth mounting panel unit 1320 of the, the first mounting panel unit 1210 to the fifth mounting panel unit 1320 are a plurality of the flying device (D) on the upper surface When is seated, it is possible to provide an image processing system for processing a captured image image based on a GPS provided with a battery supply unit (B) for supplying batteries for each of the flight devices (D).

The guide module 1100 includes an upper panel unit 1110 in which the first mounting panel unit 1210 to a fifth mounting panel unit 1320 are installed, and a lower driving unit driven by interlocking the upper panel unit 1110 with the upper panel unit 1110 . It includes a panel part 1120, wherein the lower driving panel part 1120 is provided at the end of the first support panel part 1121 that moves forward and backward to one side, and the first support panel part 1121, and moves upward and downward. A first actuator 1122 in which a first structure 1200 is installed to drive the first structure 1200, a second support panel part 1123 that moves forward and backward to the other side, and the second support panel part ( 1123), the second structure 1300 is installed at the upper portion and the second actuator 1124 for driving the second structure 1300 is provided at the end of the GPS to process the photographed image image An image processing system may be provided.

According to the present invention as described above, there are one or more of the following effects.

The present invention is based on GPS, which integrates and manages real-time collected information through a drone that can immediately correct when a changed part is detected after comparing the image information data collected in real time through a plurality of photographing units with the existing image information data. It is possible to provide an image processing system for processing a photographed video image.

In addition, in operating such a system, it is possible to provide an image processing system for processing a photographed image based on a GPS having a photographing means and various configurations that can guarantee the effective operation and reliability of the photographing means for photographing. .

In addition, it is possible to provide an image processing system for processing a photographed image image based on a GPS capable of imparting structural stability including earthquake resistance of elements related to photographing means, structural stability and durability.

In addition, through accurate check management in the operation of the photographing means, it is possible to provide an image processing system that processes the captured video images based on the GPS, which can accurately and reliably manage the flight and return of a plurality of photographing means. can

1 is a view showing the overall configuration of an image processing system for processing a captured image image based on a GPS that integrates and manages real-time collection information through a drone according to an embodiment of the present invention.
2 is a diagram showing the configuration of a coordinate synthesis module according to an embodiment of the present invention.
3 is an exemplary diagram schematically illustrating a video image captured by a photographing unit according to an embodiment of the present invention.
4 is a diagram showing the configuration of an image correction module according to an embodiment of the present invention.
5 is an exemplary diagram schematically illustrating a process of reducing and editing a video image using a magnification editing module according to an embodiment of the present invention.
6 is a view showing the overall appearance of the photographing unit according to an embodiment of the present invention.
Figure 7 is a view showing the overall appearance of the buffer according to an embodiment of the present invention.
8 is a view showing the overall appearance of the rotation detachable unit according to an embodiment of the present invention.
9 is a view showing a view from above of the rotation detachable unit according to an embodiment of the present invention.
10 is a cross-sectional view showing an internal state of the rotation control unit according to an embodiment of the present invention.
11 is a longitudinal cross-sectional view showing a state of a fixing bracket according to an embodiment of the present invention.
12 is a view showing a view from the bottom of the fixing bracket according to an embodiment of the present invention.
13 is a view showing an exploded state of each configuration of the windshield according to an embodiment of the present invention.
14 is a cross-sectional view illustrating an operation of the windshield according to an embodiment of the present invention.
and
15 to 16 are views showing the main configuration according to another embodiment of the present invention.

Hereinafter, based on the accompanying drawings, the present invention will be described in detail so that those of ordinary skill in the art can easily carry out the present invention. However, the present invention may be embodied in several different forms and is not limited to the embodiments described herein. In order to clearly explain the present invention, parts irrelevant to the description are omitted, and the same reference numerals are assigned to the same or similar components throughout the specification. In addition, the terms or words used in the present specification and claims should not be construed as being limited to their ordinary or dictionary meanings, and the inventor must properly understand the concept of the term in order to best describe his invention. Based on the principle that it can be defined, it should be interpreted as meaning and concept consistent with the technical idea of the present invention.

1 is a diagram showing the overall configuration of an image processing system for processing a captured image image based on a GPS that integrates and manages real-time collected information through a drone according to an embodiment of the present invention. As shown, the image processing system for processing the captured video image based on the GPS according to the present invention includes a base station 2000', a photographing unit 1000', and a processing unit 3000'. The base station 2000', the photographing unit 1000', and the processing unit 3000' can communicate through a network. The base station 2000' receives a position value from an artificial satellite, calculates each other, outputs a GPS correction value, and wirelessly transmits the output GPS correction value. Specifically, the base station 2000' is a GPS receiver that receives a location value from an artificial satellite by disposing a GPS antenna 2110'.

(2100'), a base control unit 2300' and DGPS (Differential GPS') antenna 2210' that mutually calculates the current position value received from the GPS receiver and a specified absolute value to output a GPS correction value and a DGPS transmitter 2200' for receiving the GPS correction values from the controller and transmitting them wirelessly.

The base station 2000' transmits the GPS correction value (position value') calculated through the base controller 2300' to the DGPS transmitter 2200', and a DGPS antenna 2210' connected to the DGPS transmitter 2200'. ) through the wireless transmission to the photographing unit 1000' to be described later. The photographing unit 1000' communicates wirelessly with the base station 2000', calculates the GPS correction value received from the base station 2000', calculates the coordinates of the measurement point, and captures the area according to the coordinates. The processing unit 3000' is installed in a remote location, receives the video image captured by the photographing unit 1000', extracts a difference from the previously stored video image, and generates an edited image. The processing unit 3000' includes an image storage module 3100', an image receiving module 3200', a coordinate synthesis module 3300', a magnification editing module 3400', and an image correction module 3500'. . Details of the processing unit 3000' will be described below. FIG. 2 is a diagram showing the configuration of a coordinate synthesis module according to an embodiment of the present invention, and FIG. 3 is an exemplary diagram schematically illustrating a video image captured by a photographing unit according to an embodiment of the present invention.

The image storage module 3100' stores an existing image image in advance, and the image receiving module 3200' wirelessly receives the captured image image from the photographing unit 1000'. That is, an image of the image before the terrain change occurs is stored in the image storage module 3100', and the image receiving module 3200' may receive the image image taken after the terrain change occurs. The coordinate synthesizing module 3300' synthesizes GPS coordinates with the video image captured by the photographing unit 1000'. the coordinate synthesis module

3300' includes a shape setting module 3310', a reference point setting module 3320', a comparison point setting module 3330', and a coordinate confirmation module 3340'.

The shape setting module 3310' limits the range by editing the video image received from the video receiving module 3200', and synthesizes the video image captured by the photographing unit 1000' with other video images. to conform to its form and specifications. For example, as shown in FIG. 3 , the image image received by the image receiving module 3200' is cut into a rectangular image, and the horizontal and vertical lengths of the rectangular image are set to meet the standard. The reference point setting module 3320' holds the center of the video image P1' cut by the shape setting module 3310' as the reference point C'. At this time, it is preferable that the corresponding point of the image image P1' taken as the reference point C' is not changed according to the topographical features.

The comparison point setting module 3330' sets an arbitrary point relatively comparable to the reference point C' as the comparison point R'. This comparison point R' becomes a comparison value for determining the sameness between the real geography, which is the object of the video image P1', and the video image P1'. The setting of the comparison point R' has no special restrictions, so it can be variously selected within the range of the video image P1' around the reference point C'. The coordinate confirmation module 3340' checks the actual GPS coordinates of the reference point C', and prepares for synthesizing the GPS coordinates centered on the reference point C' in the video image P1' based on this. At this time, since the standard of the GPS coordinates must match the standard of the video image P1', check the GPS coordinates of the comparison point (R') to determine the 'real distance' between the reference point (C') and the comparison point (R') and the image Check the 'image distance' between the reference point C' and the comparison point R' on the image P1', respectively. The coordinate check module 3340' calculates the ratio of the 'real distance' and the 'image distance' checked in this way, and reduces or enlarges the GPS coordinates according to the scale. The coordinate check module 3340' synthesizes the reduced or enlarged GPS coordinates in the video image P1', and provides the GPS coordinates in the entire video image P1' in addition to the reference point C' and the comparison point R'. to be applied. 4 is a diagram showing the configuration of an image correction module according to an embodiment of the present invention, and FIG. 5 schematically shows a process of reducing and editing a video image using the magnification editing module according to an embodiment of the present invention. It is one example diagram.

5 (a') is a video image (P1') photographed through a photographing unit and a video image (P1'') obtained by editing the magnification of the video image (P1'), and FIG. 5 (b') is a previously stored image. The video image P2' of As shown, the magnification editing module 3400' edits the video image P1' to which the GPS coordinates are input at the same magnification as the previously stored video image P2', and the video image P1' itself is reduced or enlarged so that it can be accurately compared with the existing video image (P2'). The magnification editing module 3400' compares the video images P1, P1', P2' with the corresponding reference point C' of the video images P1, P1', P2' to match the magnifications of the video images P1, P1', P2' having various magnifications. Check the distance D' between the points R', and adjust the magnifications of the video images P1, P1', and P2' so that these distances D' match. In this case, the selected reference point C' and the comparison point R' may be the same point in the newly captured video image P1' and the previously stored video image P2'.

The image correction module 3500' reads a video image P1'' edited at the same magnification with a pre-stored existing video image P2', and a processed image module 3510', a comparison detection module 3520' and an edited image module 3530'. The processed image module 3510' extracts a layer from the image image received through the image receiving module 3200' and processed through the coordinate synthesis module 3300' and the magnification editing module 3400' to create a processed image file. create In other words, the processed image module 3510' extracts the layers of buildings, roads, altitudes, fences, and inland water systems necessary for correction, and warps them to have a resolution that can be decoded. to create The comparison detection module 3520' detects a difference by comparing the existing image image stored in the image storage module 3100' with the processed image. The comparison detection module 3520' compares the generated processed image with the existing video image, detects differences in position and shape, and classifies each processed image as an object to be read or an object to be read. For example, if a number of buildings are newly added (different in shape) in the upper right corner based on the crossroads near the reference point C' as in (a') of FIG. 5, the processed image can be classified as a reading object. .

The edited image module 3530' analyzes the processed image classified as an object to be read by the comparison detection module 3520' and, when it is read that there is a change in the feature, converts the extracted layer of the processed image to the existing image image. A new edit overlaid on top creates and saves an image file. In this way, by comparing the received video image with the pre-stored video image, the video image with differences can be replaced with the latest video image. It is possible to quickly provide the changed video image according to the

6 is a view showing an overall appearance of a photographing unit according to an embodiment of the present invention. As shown, the photographing unit 1000' includes a photographing body 1010' disposed in the center, four wing portions 1020' extending from the side of the photographing body, and four propellers coupled to the wing end, respectively ( 1030') by default. As the propeller 1030' operates, the photographing unit 1000' may rise or fall, and may move to a desired point. Although not shown, a control unit, a communication unit, and the like are built-in inside the photographing body 1010 ′ to communicate with the base station 2000 ′ and the processing unit 3000 ′. Specifically, the propeller 1030' is disposed in the center and coupled to surround the central part 1031' connected to the rotating motor (not shown) and the outside of the central part to receive rotational force from the central part, and the rotating blade 1034' to the outside. ) includes a wing rotating part 1032' to which it is coupled.

The blade rotating part 1032' is formed in a ring shape, and a plurality of 'T'-shaped melting parts 1033' protrude from the inside of the blade rotating part 1032'. A groove is formed in the central portion 1031' in a shape corresponding to the 'T'-shaped melting part 1033' to be inserted. It is transmitted to the rotating part 1032'. At this time, it is preferable that the melting part 1033' is made of a material having a relatively lower melting point than the central part 1031' and the blade rotating part 1032'. That is, when foreign substances are caught in the propeller 1030' and the propeller does not rotate properly and heat is generated due to overcurrent, the melting part 1033' having a low melting point is first melted and broken. can be separated. The melting part 1033' may be made of a polypropylene' material, and the central part 1031' and the wing rotating part 1032' may be made of a polyamide' material. The polypropylene material has a melting point of about 160°C, which is about 80°C lower than that of the polyamide material.

Accordingly, the expensive rotary motor is not damaged by heat and the user can reuse the propeller 1030' again by replacing only the blade rotating part 1032' and the rotating blade 1034' part. On the other hand, the fixing bracket 1300' is coupled to the lower portion of the photographing body 1010', and the rotary detachable part 1200' is inserted so as to be detachably attached to the lower part of the fixed bracket, and the buffer part 1100' is provided on the lower surface of the rotary detachable part. ) is coupled, and the camera 1400' is coupled to the lower surface of the buffer unit. A windshield 1500', which will be described later, is coupled to a lower portion of the wing portion 1020'. 7 is a view showing the overall appearance of the buffer according to an embodiment of the present invention. As shown, the camera 1400' is mounted on the bottom surface of the photographing body 1010' via a fixing bracket 1300', a rotation detachable part 1200' and a buffer part 1100', in a vertical direction. It is used to acquire a video image by photographing a geographical feature. In the present invention, the camera 1400' is used to photograph an area in which a terrain change occurs.

Specifically, the buffer part 1100' is a buffer top plate 1110' coupled to the lower surface of the rotation detachable part 1200', a buffer bottom plate 1130' that is spaced apart from each other at a predetermined interval in the lower portion of the buffer top plate, and It is mounted between the buffer upper plate and the lower buffer plate includes a buffer elastic portion (1120') that provides an elastic restoring force in the vertical direction. A camera 1400' is coupled to the lower surface of the buffer lower plate 1130'. In the illustrated embodiment, the buffer upper plate 1110' and the buffer lower plate 1130' are formed in the shape of a square panel, but are not limited thereto, and may be formed in various shapes, and the buffer elastic part 1120') It is also formed in the form of a coil spring, but is not limited thereto.

The cushioning elastic unit 1120 ′ provides an elastic restoring force in the vertical direction to attenuate shock or vibration applied to the camera 1400 ′ from the photographing unit, thereby improving the accuracy of the camera. In addition, at the four corners of the buffer upper plate 1110 ', four upper plate extension parts 1111' forming a 'U'-shaped groove protrude downward and extend toward the bottom, and at the four corners of the lower buffer plate 1130', there are 'U' 'Four lower plate extensions 1131 ' forming a shape groove protrude upward.

That is, the upper plate extension 1111 ′ and the lower plate extension 1131 ′ are formed to protrude to face each other like teeth, and the upper plate extension 1111 ′ is disposed relatively inside the lower plate extension 1131 ′. A predetermined space is formed in a portion where the upper plate extension 1111 ′ and the lower plate extension 1131 ′ face each other. The left and right elastic parts 1140' are inserted into the predetermined space formed by the upper plate extension part 1111' and the lower plate extension part 1131'. The left and right elastic part 1140' has one side in contact with the 'U'-shaped groove of the upper plate extension part 1111' and the other side is in contact with the 'U'-shaped groove of the lower plate extension part 1131' to contact the buffer top plate 1110. ') and the buffer lower plate 1130' to provide an elastic restoring force in the front, back, left, and right directions. In other words, in the lower buffer plate 1130 ′ and the camera 1400 ′ coupled to the lower portion thereof, the vertical vibration is attenuated by the buffer elastic unit 1120 ′, and the left and right elastic units 1140 ′ in the front, rear, left and right directions. vibration is damped.

Two upper plate extensions 1111' disposed on one side of the buffer top plate 1110' among the four upper plate extension parts 1111', the other side of the buffer top plate 1110' among the four upper plate extension parts 1111' The remaining two upper plate extensions 1111 ′ disposed on the . The upper plate support 1112' and the buffer lower plate 1130' are connected through the raised part 1150', and as the heightened part 1150' is adjusted, the buffer upper plate 1110' and the buffer lower plate 1130') The distance between them may be variable. That is, the user can increase the height in consideration of the flying speed of the drone, the weight of each part, and tighten or loosen the part 1150 ′, and thus the separation distance between the buffer top plate 1110 ′ and the buffer bottom plate 1130 ′ is variable. Thus, the stiffness of the cushioning elastic part 1120 ′ can be adjusted.

At this time, the interval between the lower surface of the buffer upper plate 1110' and the uppermost end of the lower plate extension 1131' is preferably adjusted to be relatively narrower than the length of the left and right elastic parts 1140', and accordingly, the left and right elastic parts ( 1140') is prevented. Figure 8 is a view showing the overall appearance of the rotary detachable unit according to an embodiment of the present invention, Figure 9 is a view showing a view from the top of the rotary detachable unit according to an embodiment of the present invention.

As shown, the rotational detachable unit 1200' is coupled to the upper portion of the buffer unit 1100' and is coupled to the detachable body 1210' and the detachable body part made of a hard material, and is detachable made of an elastic material. and a fastening part 1220'. The detachable body part 1210' is made of a hard material having sufficient rigidity to support the buffer part 1100' coupled to the lower part, such as metal, wood, etc., and the detachable fastening part 1220' has elasticity such as silicon. Made of flexible material. In the present invention, the detachable body part 1210' and the detachable fastening part 1220' are made of different materials, so that the camera 1400' can be stored separately when not in use, and can be attached and used when in use. have. The detachable body portion 1210 'is a detachable lower plate 1211' coupled to the upper portion of the buffer upper plate 1110', a detachable rotating shaft 1212 ' extending from the center of the detachable lower plate toward the upper part, and a detachable rotating shaft at the upper end of the It is mounted and includes a rotation control unit 1230' for controlling the rotation of the detachable rotation shaft.

As described above, since the detachable body 1210 ′ is rotatable based on the detachable rotation shaft 1212 ′, the viewing angle of the camera 1400 ′ can be freely adjusted. Such rotation may be performed manually by a user, or may be automatically performed using a known configuration such as a motor or a gear. The detachable and fastening part 1220' is a detachable upper plate 1221' coupled to the upper part of the detachable lower plate 1211', is formed in a hemispherical shape on the upper part of the detachable upper plate, and is a detachable and elastic part disposed to surround the detachable rotation shaft 1212'. (1222 '), a detachable external force portion (1223 ') formed on both sides of the detachable telescopic part and capable of applying an external force so that the taktaktak telescopic part can be retracted or unfolded, a rotation guide part (1224') formed to protrude from the side of the detachable external force part, and It includes a detachable perforation part 1225' that is perforated in the form of a ten (十') shape on the upper portion of the detachable extension part.

The user may hold the detachable external force unit 1223' and apply force to allow the detachable external force unit 1223' to come into the detachable/extending unit 1222', and at this time, the protruding rotation guide unit 1224' is also detachable. The detachable body part 1210' can be separated from the fixing bracket 1300' to be described later as it enters the stretchable part 1222'.

When inserting the detachable body part 1210' into the fixing bracket 1300', reverse the above process to apply a force so that the rotation guide part 1224' enters the detachable/extensible part 1222' inside the fixing bracket. Inserted into (1300'), the detachable external force portion 1223' is placed so that the rotation guide portion 1224' can protrude. 10 is a cross-sectional view illustrating an internal state of a rotation control unit according to an embodiment of the present invention. As shown, the rotation control unit 1230' is coupled to the upper end of the detachable rotation shaft 1212', the rotation control body 1231' with an empty interior, and a first spring 1232 coupled to the inner left end of the rotation control body. '), a first slider 1233' coupled to the end of the first spring, a first sphere 1234' coupled to the end of the first slider and exposed to the outside of the rotation control body or accommodated inside the rotation control body , a second spring 1236 ′ coupled to the inner right end of the rotation control body, a second slider 1237 ′ coupled to an end of the second spring, and an end of the second slider and exposed to the outside of the rotation control body or rotated and a second sphere 1238' that can be housed inside the control body.

Since the first spring 1232' provides an elastic force for pushing the first slider 1233' to the right, the first sphere 1234' is partially outside the rotation control body 1231' unless an external force is applied. Or all exposed. Similarly, since the second spring 1236' provides an elastic force for pushing the second slider 1237' to the left, the second sphere 1238' moves to the outside of the rotation control body 1231' unless an external force is applied. Some or all of them are exposed. On the other hand, an electromagnet 1235' which is magnetized when a current flows is mounted on one side of the first slider 1233', and a second slider 1237' facing one side of the first slider 1233' On one side of the magnetic body 1239' is mounted. When a current flows through the electromagnet 1235', the first slider 1233' and the second slider 1237' are contacted and fixed, so the first sphere 1234' and the second sphere 1238' are the rotation control body ( 1231') and may be fixed in a state exposed to the outside.

In other words, normally the first sphere 1234' and the second sphere 1238' are accommodated inside or outside the rotation control body 1231' by the first spring 1232' and the second spring 1236'. The exposed state can be moved freely, but when a current flows in the electromagnet 1235', the electromagnet 1235' and the magnetic material 1239' are fixed in the attached state, so the first slider 1233' and the second slider ( 1237 ′ is hardened like a single rod, and accordingly, the first sphere 1234 ′ and the second sphere 1238 ′ can be fixed in a state exposed to the outside. 11 is a longitudinal cross-sectional view showing the state of the fixing bracket according to an embodiment of the present invention, Figure 12 is a view showing the state of the fixing bracket according to an embodiment of the present invention viewed from below. As shown, the fixing bracket 1300' is coupled to the lower portion of the photographing body 1010' and an insertion space 1311' so that the detachable and fastening part 1220' of the rotational detachable part 1200' can be inserted. It is disposed on the upper end of the formed fixed body (1310') and the inner insertion space of the fixed body and includes a rotation receiving unit (1320') in which the rotation control unit 1230' is rotatably accommodated. That is, the fixing bracket 1300' is coupled to the lower surface of the photographing body 1010', and the rotational detachable part 1200' is detachably and rotatably fastened to this fixing bracket 1300', and the rotational detachable part ( The buffer unit 1100' is coupled to the lower portion of the 1200', and the camera 1400' is coupled to the lower portion of the buffer unit 1100'.

A guide groove 1312' is recessed along the periphery of the central portion of the insertion space 1311'. The above-mentioned rotation guide part 1224' is accommodated in the guide groove 1312', and accordingly, the detachable body part 1210' can rotate in a constant orbit without being separated from the fixing bracket 1300'. On the other hand, a plurality of locking grooves 1321' are recessed along the circumference of the inner surface of the rotation accommodating part 1320'. The first sphere 1234 ′ and the second sphere 1238 ′ are accommodated in the locking groove 1321 ′ to have a certain fixing force. In other words, as the detachable body part 1210' rotates, the detachable rotation shaft 1212' is rotated, and the rotation control unit 1230' at its upper end also rotates, the first sphere 1234' and the second sphere ( When 1238') is accommodated in the locking groove 1321', it temporarily has a little fixing force, and the first sphere 1234' and the second sphere 1238' pass through the locking groove 1321' and then again When accommodated in the other locking groove 1321 ', it is possible to clearly recognize whether the rotation is rotated by forming a sense of theft with a 'click' feeling.

If the viewing angle adjustment of the camera 1400' is completed and it is no longer necessary to rotate the detachable body unit 1210', a current flows through the electromagnet unit 1235' to the first slider 1233' and the second slider. 1237' is made to be as hard as a single rod, and accordingly, the first sphere 1234' and the second sphere 1238' are fixed in the state accommodated in the engaging groove 1321', so the detachable body part 1210' will no longer rotate. Although not shown, the electromagnet unit 1235 ′ is electrically connected to a general control unit of the photographing unit, a battery, and the like, and may operate so that current flows or does not flow according to circumstances. In addition, rotation of the camera 1400 ′ and the detachable body 1210 ′ may also be performed automatically using a known configuration such as a motor or a gear.

13 is a view showing an exploded state of each configuration of the windshield according to an embodiment of the present invention, Figure 14 is a cross-sectional view illustrating an operation of the windshield according to an embodiment of the present invention. 6, the windshield 1500' is coupled to the lower portion of the wing portion 1020'. When the photographing unit 1000' is seated on the ground, the windshield 1500' allows each part including the photographing body 1010' to be safely seated on the ground, and when the photographing unit 1000' operates, the windshield (1500') is disposed around the camera (1400') serves to prevent excessive wind injection into the camera (1400'). Specifically, the windshield part 1500' is installed to be movable up and down in the wind case 1530', which has an empty interior and an entry hole 1531' at the bottom, and the wind case to protrude to the outside or be accommodated inside. The lower wind body 1510' that can be, a plurality of locking jaws 1511' that are formed to protrude from the top of the front surface of the lower wind body, are disposed in front of the lower wind body and are installed to be movable up and down to protrude to the outside or inside It includes a plurality of rails 1521' that are recessed in the rear surface of the upper wind body 1520' and the upper wind body that can be accommodated in the upper wind body and accommodate a plurality of locking jaws 1511'.

An end of the lower wind body 1510 ′ is connected to a wind rotation motor 1540 ′ and can be rotated upward or downward, and a plurality of locking jaws 1511 ′ are accommodated in a plurality of rails 1521 ′. It can slide up and down. As shown, a plurality of locking jaws 1511' are formed in a 'T' shape and do not separate from the rail 1521'. When the body 1510' is further moved downward, the upper wind body 1520' is moved downward along with the lower wind body 1510' while the locking jaw 1511' is caught on the rail 1521'. Conversely, when the lower wind body 1510' is further moved toward the upper part in a state where the locking jaw 1511' of the lower wind body 1510' is located at the uppermost end of the rail 1521', the upper wind body 1520' is The lower wind body 1510' is accommodated in an overlapping state.

The present invention divides the lower wind body 1510 ′ and the upper wind body 1520 ′ in this way, and according to the downward movement of the lower wind body 1510 ′, the upper wind body 1520 ′ can also be moved downward. It occupies a small area and at the same time maximizes the effect of preventing wind ingress.

In addition, the present invention can freely adjust the extent to which the lower wind body 1510' and the upper wind body 1520' are unfolded in consideration of the speed of the wind and the like. On the other hand, in the lower wind body 1510', a plurality of vent holes 1512' are arranged to be spaced apart in the transverse direction, and a plurality of air grooves 1513' are disposed spaced apart between the plurality of vent holes 1512'. do. The plurality of vent holes 1512' are formed in a longitudinally long oval shape, and some wind passes through the lower wind body 1510' to allow natural flow to the rear, so that when a strong wind occurs, the lower wind body 1510 ') is broken or excessive vibration is generated and has an effect of preventing transmission to the Tron body 3100' and the camera 1400'. The plurality of air grooves 1513 ′ are formed in a 'V' shape with a low central portion and high both ends, and four air grooves 1513 ′ spaced apart in the longitudinal direction form a set. The plurality of air grooves 1513 ′ guide the wind that collides with the lower wind body 1510 ′ in the direction of the vent holes 1512 ′ to flow.

15 to 16 are views showing the main configuration according to another embodiment of the present invention. 15 to 16 based on the above content, in the image processing system for processing a captured image image based on the integrated management GPS, an image storage module (3100'); an image receiving module 3200' for wirelessly receiving the photographed image image; a coordinate synthesizing module 3300' for synthesizing GPS coordinates with the received video image; and an image correction module for extracting differences by comparing the edited video image at the same magnification with the pre-stored existing video image.

Here, the coordinate synthesizing module 3300' includes: a shape setting module 3310' for editing the video image received through the image receiving module 3200' to match the shape and standard; a reference point setting module (3320') for setting a reference point of the image image cut by the shape setting module (3310'); a comparison point setting module 3330' that sets a comparative point that can be relatively compared with the reference point set by the reference point setting module 3320'; and a coordinate confirmation module (3340') for confirming the actual GPS coordinates of the reference point and synthesizing the GPS coordinates with the video image based thereon; includes

In addition, the image image received by the image receiving module (3200') is acquired by a camera installed in the photographing unit, the photographing unit is to include a predetermined flight device (D), and is photographed based on the integrated management GPS The image processing system for processing an image image includes a control unit in which the flight device (D) is operated, and the control unit is a plurality of flying devices (D) and the flying device (D) is mounted in a plurality A mounting device 1000 is included, wherein the mounting device 1000 includes a central guide module 1100 , a first structure 1200 provided on one side of the guide module 1100 , and the guide module 1100 . A second structure 1300 provided on the other side of the, the uppermost first mounting panel 1210 installed horizontally from the first structure 1200 to the guide module 1100, and the first structure 1200 The middle second mounting panel part 1220 installed horizontally from the guide module 1100, and the lowermost third mounting panel part 1230 installed horizontally from the first structure 1200 to the guide module 1100 ) including a first mounting panel module, a fourth mounting panel part 1310 at the top that is horizontally installed from the second structure 1300 to the guide module 1100, and the second structure 1300 from the The guide module 1100 includes a second mounting panel module including a fifth mounting panel unit 1320 at the bottom horizontally installed.

On the other hand, the first mounting panel unit 1210 to the fifth mounting panel unit 1320, when a plurality of the flying device (D) is seated on the upper surface, for supplying batteries for each to the flying device (D) A battery supply unit (B) is provided, and the guide module 1100 includes an upper panel unit 1110 in which the first mounting panel unit 1210 to the fifth mounting panel unit 1320 are installed, and the upper panel unit. 1110 includes a lower driving panel unit 1120 driven in association with each other, wherein the lower driving panel unit 1120 includes a first supporting panel unit 1121 that moves forward and backward to one side, and the first supporting panel unit A first driving body 1122 provided at the end of 1121 and having the first structure 1200 installed thereon to drive the first structure 1200, and a second support panel part that moves forward and backward to the other side ( 1123), and a second actuator 1124 provided at the end of the second support panel unit 1123 and having the second structure 1300 installed thereon to drive the second structure 1300 is provided. .

Here, the first actuator 1122 and the second actuator 1124 operate in a first height adjustment mode in which the first actuator 1122 and the second actuator 1124 are raised and lowered, respectively. And, the upper panel portion 1110 of the guide module 1100 is operated in a second height adjustment mode that elevates and lowers in response to the first height adjustment mode, and the second height is displayed on the flight device (D). Prevents from being impacted or falling according to the adjustment mode. The first structure 1200 applies an axial rotation force to the first mounting panel unit 1210 to the third mounting panel unit 1230, and the first mounting panel unit 1210 to the third mounting panel unit 1210. The panel unit 1230 is operated in the first fixing mode to be fixed on the upper panel unit 1110 by a rotational pressing force.

In addition, the second structure 1300 applies an axial rotation force to the fourth mounting panel unit 1310 to the fifth mounting panel unit 1320 , and the fourth mounting panel unit 1310 to the fifth mounting panel unit 1310 . The panel unit 1320 is operated in a second fixed mode in a fixed mode in which the panel unit 1320 is fixed on the upper panel unit 1110 by a rotational pressing force, and the first mounting panel unit 1210 to the third mounting panel unit 1230 are operated. ), a first magnetic coupling unit (M1) is provided at a position corresponding to the flight device (D), respectively, and the flying device (D) on the fourth mounting panel unit 1310 to the fifth mounting panel unit 1320 ), a second magnetic coupling portion (M2) is provided at a position corresponding to each.

The first magnetic coupling unit (M1) to the second magnetic coupling unit (M2) are fixed during the operation of the first fixed mode and the second fixed mode, so that the flight device (D) is in the first fixed mode and The second fixed mode operation operates in a magnetic force generating mode in which magnetic force is generated to prevent mutual collision or fall. In addition, the mounting device 1000, the lowermost main frame 1400 on which the lower driving panel unit 1120 is installed, is located on one side of the main frame 1400, and the first driving body ( 1122) is installed, and a first contact body 1411 in contact with a side portion of the first actuator 1122 is provided to fix the first actuator 1122 with the first contact body 1411. A movable body 1410 and a second contact body located on the other upper side of the main frame 1400 and having the second actuator 1124 installed thereon, and in contact with the side surface of the second actuator 1124 ( 1421) is provided, and a second movable body 1420 for fixing the second actuator 1124 with the second contact body 1421 is provided.

Here, the first contact body 1411 and the second contact body 1421 press and fix the first actuator 1122 and the second actuator 1124 through horizontal rotation, respectively, and One movable body 1410 is provided with a first sub contact body 1412 in contact with the first driving body 1122 on the opposite side opposite to the first contact body 1411, the first sub contact body ( 1412 is slidably pressurized to fix the first actuator 1122 on the first movable body 1410 by pressing it toward the first contact body 1411 . The second movable body 1420 is provided with a second sub-contact body 1422 in contact with the second driving body 1124 on the opposite side of the second contact body 1421 , the second sub-contact The sieve 1422 is slidably moved to press and fix the second actuator 1124 on the second movable body 1420 toward the second contact body 1421 .

The first movable body 1410 is formed when the first contact body 1411 and the first sub contact body 1412 are installed on the left and right sides of the first actuator 1122 , the first actuator 1122 . ) is provided with a pair of third sub-contacts 1413 positioned on the front and rear surfaces, and the third sub-contacts 1413 are pressed close to each other with the first actuator 1122 interposed therebetween. induced The second movable body 1420 is formed when the second contact body 1421 and the second sub contact body 1422 are installed to the left and right of the second actuator 1124 , the second actuator 1124 . ) is provided with a pair of fourth sub-contacts 1423 positioned on the front and rear surfaces, and the fourth sub-contacts 1423 are pressed close to each other with the second actuator 1124 interposed therebetween. is moving The main frame 1400 includes a 1-1 movable column 1431 installed on the main frame 1400 upper portion so as to be positioned below the first supporting panel unit 1121, and the 1-1 movable column. (1431) and adjacent 1-2 movable pillars (1433) are provided.

The 1-1 movable pillar 1431 is provided with a 1-1 binding hole 1432 for binding to surround the outer circumferential surface of the first support panel unit 1121, and the 1-2 movable pillar 1433 is provided. ) is provided with a 1-2 binding sphere 1434 for binding to surround the outer peripheral surface of the first support panel portion 1121.

The 1-1 movable pillar 1431 and the 1-2 movable pillar 1433 are moved upward or downward on the main frame 1400 to support and reinforce the first support panel unit 1121 between the top and bottom. and the 2-1 th movable pole 1441 installed on the upper part of the main frame 1400 so as to be positioned under the second supporting panel part 1123, and the 2-1 th movable pole 1441 on the upper part A 2-2 movable pillar 1443 is provided.

The 2-1 movable pillar 1441 is provided with a 2-1 binding hole 1442 for binding to surround the outer circumferential surface of the second support panel unit 1123, and the 2-2 movable pillar 1443 is provided. is provided with a 2-2 binding sphere 1444 for binding to surround the outer circumferential surface of the second support panel 1123, the 2-1 movable pillar 1441 and the 2-2 movable pillar 1443 ) is moved upward or downward on the main frame 1400 to support and reinforce the second support panel unit 1123 between the top and bottom.

Here, the upper panel part 1110 is provided with a first sortie detection module (S1) for detecting the sortie of the flying device (D), and the first structure 1200 has the sortie of the flying device (D). A second sortie detection module (S2) for detecting is provided, and the second structure (1300) is provided with a third sortie detection module (S3) for detecting the sortie of the flying device (D), the first output detection Module (S1) to the third sortie detection module (S3) checks the sortie of the normal number by detecting the sortie to the front and rear of the flying device (D). The driving method of the physical components described above is based on a motor, an actuator, etc., and the forward and backward movement and rotation movement are made, and the shape and size of each component can be variously selected and provided according to the installation site and materials to be implemented. . In addition, it goes without saying that the basic principle of cooling can be applied in the same or applied manner based on various existing methods. Although the present invention has been described with reference to the embodiment shown in the drawings, which is merely exemplary, it will be understood by those skilled in the art that various modifications and equivalent other embodiments are possible therefrom. Accordingly, the true technical protection scope of the present invention should be determined by the technical spirit of the appended claims.

1000': Recording unit 1010': Recording body
1020': Wing 1030 ': Propeller
1031': central part 1032': wing rotation part

Claims (2)

The processing unit 3000' of the image processing system, which includes a photographing unit 1000', a base station 2000', and a processing unit 3000', communicates through a network, and processes the captured image image based on the GPS.
an image storage module 3100' in which an existing image image is stored in advance;
an image receiving module 3200' for wirelessly receiving the image taken from the photographing unit 1000';
a coordinate synthesis module (3300') for synthesizing GPS coordinates with the video image received by the image receiving module (3200');
a magnification editing module (3400') for editing an image image synthesized with GPS coordinates by the coordinate synthesizing module (3300') at the same magnification as a previously stored image image; and
Comprising an image correction module (3500') for extracting a difference by comparing the image image edited at the same magnification by the magnification editing module (3400') with an existing image image stored in advance,
The coordinate synthesis module 3300' is
a shape setting module 3310' for editing the video image received through the video receiving module 3200' to match the shape and standard;
a reference point setting module 3320' for setting a reference point of the image image cut by the shape setting module 3310';
a comparison point setting module 3330' for setting a comparison point that can be relatively compared with the reference point set by the reference point setting module 3320'; and
a coordinate confirmation module 3340' for confirming the actual GPS coordinates of the reference point and synthesizing the GPS coordinates with the video image based thereon; including,
The image correction module 3500 is
a processed image module for generating a processed image file by extracting a layer from the image image received through the image receiving module (3200') and processed through the coordinate synthesis module (3300') and the magnification editing module (3400');
a comparison detection module for detecting a difference by comparing an existing image image stored in the image storage module 3100' with a processed image; and
an edited image module for generating a new edited image file by arranging the processed image classified as an object to be read by the comparison detection module on an existing video image; includes,
The image image received by the image receiving module (3200') is obtained by a camera installed in the photographing unit (1000'),
In the image processing system for processing the image image taken based on the photographing unit 1000' is a GPS processing the image image taken based on the GPS including a predetermined flight device (D),
The image processing system for processing the image image taken based on the GPS,
Further comprising a control unit in which the flight device (D) is operated,
The control unit is
A plurality of flying devices (D) and a mounting device (1000) on which a plurality of the flying devices (D) are mounted,
The mounting device 1000 is
A guide module 1100 in the center, a first structure 1200 provided on one side of the guide module 1100, a second structure 1300 provided on the other side of the guide module 1100, and the first The uppermost first mounting panel part 1210 installed horizontally from the structure 1200 to the guide module 1100, and the second mounting panel part installed horizontally from the first structure 1200 to the guide module 1100 (1220), and a first mounting panel module including a third mounting panel part 1230 of the lowermost level installed horizontally from the first structure 1200 to the guide module 1100,
The uppermost fourth mounting panel part 1310 is horizontally installed from the second structure 1300 to the guide module 1100, and the second structure 1300 to the guide module 1100 is installed horizontally. Including a second mounting panel module including a fifth mounting panel unit 1320,
The first mounting panel unit 1210 to the fifth mounting panel unit 1320 are,
When a plurality of the flying devices (D) are seated on the upper surface, an image processing system for processing an image image taken based on a GPS having a battery supply unit (B) for supplying batteries for each of the flying devices (D) .
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