CN201672918U - Disaster situation obtaining system - Google Patents

Disaster situation obtaining system Download PDF

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Publication number
CN201672918U
CN201672918U CN2010201940986U CN201020194098U CN201672918U CN 201672918 U CN201672918 U CN 201672918U CN 2010201940986 U CN2010201940986 U CN 2010201940986U CN 201020194098 U CN201020194098 U CN 201020194098U CN 201672918 U CN201672918 U CN 201672918U
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China
Prior art keywords
module
disaster
control
image
condition
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Expired - Fee Related
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CN2010201940986U
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Chinese (zh)
Inventor
徐志强
刘明星
杨建思
王胜利
姜旭东
郭军
吴忠良
王军
田宝峰
梁建宏
郑钰
余永光
廖力
李晓宇
刘莎
张东宁
韩炜
卜淑彦
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INSTITUTE OF GEOPHOSICS OF CHINA EARTHQUAKE ADMINISTRATION
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INSTITUTE OF GEOPHOSICS OF CHINA EARTHQUAKE ADMINISTRATION
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Priority to CN2010201940986U priority Critical patent/CN201672918U/en
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Publication of CN201672918U publication Critical patent/CN201672918U/en
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Abstract

The utility model relates to a disaster situation obtaining system capable of fast obtaining the disaster situations after the disaster occurs. The disaster situation obtaining system comprises an aerial photographing device, an image analysis device and a remote controller, wherein the remote controller sends out control information to the aerial photographing device in a wireless mode, the aerial photographing device collects ground disaster situation images according to the control information received from the remote controller, and transmits the collected disaster situation images to the image analysis device, and the image analysis device analyzes the disaster situation images received from the aerial photographing device. The disaster situation images in disaster areas are collected in real time through controlling an unmanned plane to fly on the disaster areas by using image collection equipment such as a video camera, a digital camera, a forward looking infrared instrument and the like carried by the unmanned plane, and are transmitted to the image analysis device on the ground in real time, and the image analysis device carries out real-time processing on the disaster situation images transmitted back by the unmanned plane for obtaining the disaster images of the disaster areas in the shortest time. The utility model breaks through unfavorable situations of disaster relief delay caused by in-time disaster situation obtaining incapability because of communication breaking in the disaster areas after heavy disasters such as earthquake and the like occur, and can provide firsthand information for fast organization of rescue and relief activities after the disaster and for post-disaster reconstruction work.

Description

A kind of the condition of a disaster is obtained system
Technical field
The utility model relates to the hazards control field, and a kind of specifically the condition of a disaster that can obtain the condition of a disaster after disaster takes place is fast obtained system.
Background technology
In all previous earthquake field in the past, obtaining and differentiating of shake back the condition of a disaster all is that the very important person goes investigation and collects to each corner in disaster area.And in fact after the earthquake, top priority is to make the decision-making of the disaster relief as early as possible, so that command scheduling rescue strength.And to accurately make disaster relief decision-making, still need quick and precisely to grasp the condition of a disaster.
8.1 grades of violent earthquakes take place at the south of the mountains, eastern the Kunlun edge in November 14 calendar year 2001, the earthquake region is on innerland, roof of the world Qinghai-Tibet Platean, and mean sea level is more than 4000 meters, because scene is uninhabited, current violent earthquake does not cause casualties, but has formed the structure deformed belt that reaches 430 kilometers.Though the satellite remote sensing images data is also arranged after the earthquake, is difficult to accurately differentiate in detail disaster-stricken situation from the sharpness of image and effect.On depopulated zone, plateau and Gobi desert, shake back the condition of a disaster obtain with geologic examination all be that the scientific investigation personnel drive or walking is prolonged seismic zone and carried out.Multichannel scientific expedition lasts the several months and just obtains earthquake region disaster figure.
Bachu-6.2 grades of earthquakes of Jiashi Ms (surface wave magnitude) in same 2003, the Ms6.1 level earthquake of Dongwuzhumuqin Banner, Inner Mongol in 2004, shake back the condition of a disaster is obtained and differentiated also all is after earthquake emergency team arrives earthquake field, make an on-the-spot survey and take to each corner in disaster area by the people, collect and obtain through gathering after disaster-stricken situation takes 3 days at the soonest, make the work of commanding and decision-making department very passive, it is particularly important to commanding and decision-making therefore to obtain the condition of a disaster fast.
The huge casualties of kilometer range up to a hundred that October in 2005, Pakistani Ms7.6 level on the 8th earthquake caused, the area, Kashmir that its massive forces are stationed, only army's injures and deaths just reach thousands of people, and road interruption, river diversion are caused in landslide everywhere, and are just difficult more for grasping the condition of a disaster.
Though adopt satellite remote sensing technology to take and to analyze the seismic region situation, the technology of obtaining of the readability of Aerial Photography, satellite data and time restriction and actual disaster scenarios it differ greatly, for the earthquake rescue, help limited.
The utility model content
Technical problem to be solved in the utility model provides a kind of the condition of a disaster and obtains system, when taking place can to obtain the disaster information in disaster area in a short period of time after the earthquake, to promote emergency management and rescue reaction velocity and comprehensive emergency capability.
The technical scheme that the utility model solves the problems of the technologies described above is as follows: a kind of the condition of a disaster is obtained system, comprises the device of taking photo by plane, image analysis apparatus and telechiric device; Described telechiric device sends control information by wireless mode to the device of taking photo by plane; The described device of taking photo by plane is gathered the condition of a disaster image on ground according to the control information that receives from telechiric device, and sends the condition of a disaster image of gathering to image analysis apparatus; Described image analysis apparatus is analyzed the condition of a disaster image that receives from the device of taking photo by plane.
The beneficial effects of the utility model are: can personnel or miscellaneous equipment can not in time enter or execute the task in unapproachable region, provide important the condition of a disaster image information for aspects such as emergency management and rescue decision-making and commanders rapidly and accurately, strengthen capability of fast response, promote emergency management and rescue reaction velocity and comprehensive emergency capability greatly.
On the basis of technique scheme, the utility model can also be done following improvement.
Further, the described device of taking photo by plane comprises unmanned plane and the image capture device that is arranged on the unmanned plane; Described telechiric device is controlled unmanned plane and image capture device, and described image capture device is gathered the condition of a disaster image and sent image analysis apparatus to by wireless mode.
Adopt the beneficial effect of above-mentioned further scheme to be, be not subjected to disaster area matter condition influence badly, can cause means of transportation to destroy in violent earthquake, and use under complicated geographical environment and the extreme climate hazardous condition.
Further, described unmanned plane comprise remote-control data receiver module, telemetry intelligence (TELINT) transmitter module, from model plane piece, unmanned aerial vehicle (UAV) control module and unmanned plane body; Described unmanned aerial vehicle (UAV) control module is carried out flight control from the control signal that telechiric device receives to the unmanned plane body according to the remote-control data receiver module; Be electrically connected with remote-control data receiver module, telemetry intelligence (TELINT) transmitter module and unmanned aerial vehicle (UAV) control module respectively from the model plane piece, described from model plane piece receiving satellite positioning signals and generate navigation information, and according to the control information that receives from the remote-control data receiver module, by the unmanned aerial vehicle (UAV) control module unmanned plane body is carried out automatic flight control, and navigation information is sent to image analysis apparatus by the telemetry intelligence (TELINT) transmitter module.
Adopt the beneficial effect of above-mentioned further scheme to be, realized the Long-distance Control of unmanned plane, and self-navigation flight, make that unmanned plane can be at the safe flight under any weather environment.
Further, describedly comprise GPS receiver module, navigation module, navigation modulation module and view data laminating module from the model plane piece; Described navigation module is electrically connected with GPS receiver module, remote-control data receiver module, view data laminating module, unmanned aerial vehicle (UAV) control module respectively, and is electrically connected with the telemetry intelligence (TELINT) transmitter module by navigation modulation module; Described view data laminating module is electrically connected with image capture device and telemetry intelligence (TELINT) transmitter module respectively; Described GPS receiver module receiving satellite positioning signals, and satellite positioning signal sent to the navigation module that is electrically connected with it; Described remote-control data receiver module receives the control information that telechiric device sends, and sends control information to be electrically connected with it navigation module; Described navigation module generates navigation information according to the satnav information that receives from the GPS receiver module, and according to navigation information and the control information that receives from the remote-control data receiver module, the unmanned aerial vehicle (UAV) control module sending controling instruction that Xiang Yuqi is electrically connected, the unmanned aerial vehicle (UAV) control module is carried out automatic flight control according to the steering order that receives from navigation module to the unmanned plane body; Described navigation module sends navigation information to the telemetry intelligence (TELINT) transmitter module through navigation modulation module, and navigation module directly sends navigation information to the view data laminating module; The telemetry intelligence (TELINT) transmitter module will send to image analysis apparatus wirelessly from the satellite positioning signal that navigation module receives; The locating information that the view data laminating module will receive from navigation module and bind from the condition of a disaster image that image capture device receives and to obtain the view data binding information, and sending the view data binding information to the telemetry intelligence (TELINT) transmitter module, the telemetry intelligence (TELINT) transmitter module will send to image analysis apparatus with wireless mode from the view data binding information that the view data laminating module receives.
Adopt the beneficial effect of above-mentioned further scheme to be, when realizing that navigation module is to unmanned plane location and navigation feature, the binding of the condition of a disaster image that unmanned plane location longitude and latitude coordinate and image capture device gather is provided, can in time understand the disaster scenarios it of concrete longitude and latitude position, bring great convenience for the later stage rescue work.
Further, described image capture device comprises colored CCD television camera and/or digital camera and/or forward looking infrared.
Adopt the beneficial effect of above-mentioned further scheme to be, overcome the problem that the technology of obtaining of readability, satellite data of Aerial Photography and time restriction and actual disaster scenarios it but differ greatly, the most real the most direct first-hand the condition of a disaster data is provided.
Further, the control signal that described unmanned aerial vehicle (UAV) control module receives from telechiric device according to the remote-control data receiver module is controlled colored CCD television camera, digital camera and forward looking infrared.
Further, described view data laminating module is bound colored CCD television camera and/or forward looking infrared shot image data with the locating information that receives from navigation module becomes the view data binding information.
Adopt the beneficial effect of above-mentioned further scheme to be, make image analysis apparatus understand the disaster scenarios it of unmanned plane present position at that time and this position at any time, and be convenient to image analysis apparatus the disaster image that receives is spliced processing.
Further, described telechiric device comprises host computer control device, telepilot, channel switching module and remote-control data sending module, and described channel switching module is electrically connected with host computer control device, telepilot and remote-control data sending module respectively; Host computer control device and telepilot transmit control signal by the chain road direction of being made up of channel switching module and the remote-control data sending module device of taking photo by plane respectively, and channel switching module is switched between host computer control device and telepilot.
Adopt the beneficial effect of above-mentioned further scheme to be, realized the Long-distance Control of unmanned plane.
Further, described image analysis apparatus comprises the condition of a disaster image receiver module and image processing system, described the condition of a disaster image receiver module receives the condition of a disaster image of the device transmission of taking photo by plane and sends to image processing system, and image processing system is handled the condition of a disaster image that receives.
Adopt the beneficial effect of above-mentioned further scheme to be, image analysis apparatus receives the condition of a disaster image by the condition of a disaster image receiver module, and analyze timely by image processing system, can effectively learn the disaster area the condition of a disaster rapidly, for effectively taking disaster relief measure to provide in time and reliable information.
In addition, the image of digital camera shooting can be stored in the movable flashing card.Because the image quality of digital camera utilizes the movable flashing card can store the disaster photo of a large amount of high definition significantly better than the colored CCD television camera, treat to carry out after unmanned plane returns further careful analysis.
Description of drawings
Fig. 1 obtains system chart for the utility model the condition of a disaster;
Fig. 2 obtains the device embodiments synoptic diagram of taking photo by plane in the system for the utility model the condition of a disaster;
Fig. 3 obtains image capture device embodiment synoptic diagram in the system for the utility model the condition of a disaster;
Fig. 4 is the utility model image analysis apparatus block diagram;
Fig. 5 obtains telechiric device block diagram in the system for the utility model the condition of a disaster;
Fig. 6 obtains computer control and image analysis system theory diagram in system's embodiment for the utility model the condition of a disaster;
Fig. 7 obtains computer control and image analysis system structural representation in system's embodiment for the utility model the condition of a disaster;
Fig. 8 compiles processing flow chart for the condition of a disaster video image.
In the accompanying drawing, the list of parts of each label representative is as follows:
1, the device of taking photo by plane, 2, image analysis apparatus, 3, telechiric device, 4, computer control and image analysis system, 101, unmanned plane, 102, image capture device, 201, the condition of a disaster image receiver module, 202, image processing system, 301, the host computer control device, 302, telepilot, 303, channel switching module, 304, the remote-control data sending module, 10101, the remote-control data receiver module, 10102, the telemetry intelligence (TELINT) transmitter module, 10103, from model plane piece, 10104, the unmanned aerial vehicle (UAV) control module, 10105, the unmanned plane body, 1010301, the GPS receiver module, 1010302, navigation module, 1010303, navigation modulation module, 1010304, the view data laminating module, 10201, the colored CCD television camera, 10202, digital camera, 10203, forward looking infrared, 20101, remote measurement receiving antenna assembly, 20102, the remote measurement receiving unit, 401, the PC104 computing machine, 402, video frequency collection card, 403, receive the modulation module, 404, image is recorded device, 405, image display, 406, the navigational parameter display module, 407, the keyboard and mouse assembly
Embodiment
Below in conjunction with accompanying drawing principle of the present utility model and feature are described, institute gives an actual example and only is used to explain the utility model, is not to be used to limit scope of the present utility model.
As shown in Figure 1, the utility model the condition of a disaster is obtained system, comprises the device 1 of taking photo by plane, image analysis apparatus 2 and telechiric device 3; Wherein, telechiric device 3 is controlled the device 1 of taking photo by plane by wireless mode and is carried out the image acquisition work of ground the condition of a disaster; The device 1 of taking photo by plane sends the condition of a disaster image of gathering to image analysis apparatus 2 by wireless mode; 2 pairs of image analysis apparatus are analyzed from the device 1 received the condition of a disaster image of taking photo by plane, to ensure the carrying out rapidly and efficiently of disaster relief work.
For realizing the purpose of obtaining the condition of a disaster image fast and safely, the device 1 of taking photo by plane of the present utility model adopts unmanned plane to carry image capture device, realizes the collection to the disaster area the condition of a disaster.
Fig. 2 is in the utility model, the embodiment synoptic diagram of the device 1 of taking photo by plane.As shown in Figure 2, the device 1 of taking photo by plane comprises unmanned plane 101 and is arranged at image capture device 102 on the unmanned plane; Telechiric device 3 is controlled unmanned plane 101 and image capture device 102 by wireless mode, utilize image capture device 102 to gather each regional the condition of a disaster image information, and send the condition of a disaster image information to image analysis apparatus 2 with wireless mode by unmanned plane 101, thereby realized the purpose of remote collection the condition of a disaster image, particularly after disaster takes place, the condition of a disaster complexity, when personnel can't in time enter, giving fast, grasp the condition of a disaster information provided the necessary technology means to organize disaster relief programs rapidly.
As shown in Figure 2, in the present embodiment, unmanned plane 101 mainly comprises remote-control data receiver module 10101, telemetry intelligence (TELINT) transmitter module 10102, from model plane piece 10103, unmanned aerial vehicle (UAV) control module 10104 and unmanned plane body 10105.Wherein, unmanned aerial vehicle (UAV) control module 10104 is arranged on the unmanned plane body 10105, and be connected with remote-control data receiver module 10101, the effect of remote-control data receiver module 10101 is to receive the control signal that telechiric device 3 sends over wireless mode, and unmanned aerial vehicle (UAV) control module 10104 can be carried out flight control from the wireless control signal that telechiric device 3 receives to unmanned plane body 10105 according to remote-control data receiver module 10101.
A main effect from model plane piece 10103 is that unmanned plane is braked flight control.It is electrically connected with remote-control data receiver module 10101, telemetry intelligence (TELINT) transmitter module 10102 and unmanned aerial vehicle (UAV) control module 10104 respectively, from model plane piece 10103 receiving satellite positioning signals and generate navigation information, and according to the control information that receives from remote-control data receiver module 10101, carry out automatic flight control by 10104 pairs of unmanned plane bodies of unmanned aerial vehicle (UAV) control module 10105, and navigation information is sent to image analysis apparatus 2 by telemetry intelligence (TELINT) transmitter module 10102.In the present embodiment, from the concrete structure of model plane piece 10103 as shown in Figure 2, comprise GPS receiver module 1010301, navigation module 1010302, navigation modulation module 1010303 and view data laminating module 1010304.Wherein, navigation module 1010302 is electrically connected with GPS receiver module 1010301, remote-control data receiver module 10101, view data laminating module 1010304 and unmanned aerial vehicle (UAV) control module 10104 respectively, and is electrically connected with telemetry intelligence (TELINT) transmitter module 10102 by navigation modulation module 1010303; View data laminating module 1010304 is electrically connected with image capture device 102 and telemetry intelligence (TELINT) transmitter module 10102 respectively.
The effect of GPS receiver module 1010301 is to receive satnav information, and sends satnav information to navigation module 1010302.The effect of remote-control data receiver module 10101 is to receive the control information that telechiric device 3 sends, and sends control information to be electrically connected with it navigation module 1010302.An effect of navigation module 1010302 is, generate navigation information according to the satnav information that receives from GPS receiver module 1010301, and according to navigation information and the control information that receives from remote-control data receiver module 10101, unmanned aerial vehicle (UAV) control module 10104 sending controling instructions that Xiang Yuqi is electrically connected, unmanned aerial vehicle (UAV) control module 10104 is carried out automatic flight control according to the steering order that receives from navigation module 1010302 to unmanned plane body 10105.In addition, navigation module 1010302 sends navigation information to telemetry intelligence (TELINT) transmitter module 10102 through navigation modulation module 1010303, and telemetry intelligence (TELINT) transmitter module 10102 will send to image analysis apparatus through the navigation information that navigation modulation module 1010303 receives wirelessly from navigation module 1010302; And, navigation module 1010302 also directly sends navigation information to view data laminating module 1010304, view data laminating module 1010304 will be bound from the locating information of navigation module 1010302 receptions with from the condition of a disaster image that image capture device 102 receives and obtain the view data binding information, and sending the view data binding information to telemetry intelligence (TELINT) transmitter module 10102, telemetry intelligence (TELINT) transmitter module 10102 will send to image analysis apparatus 2 with wireless mode from the view data binding information that view data laminating module 1010304 receives.Therefore another effect from model plane piece 10103 is that image and navigation data that image capture device 102 sends are bound, and by telemetry intelligence (TELINT) transmitter module 10102 binding information is sent to image analysis apparatus 2 with wireless mode.
As shown in Figure 3, image capture device 102 mainly comprises colored CCD television camera 10201, digital camera 10202 and forward looking infrared 10203 in the present embodiment; Colored CCD television camera 10201, digital camera 10202 and forward looking infrared 10203 all are electrically connected with unmanned aerial vehicle (UAV) control module 10104, telechiric device 3 can carry out control operation by colored CCD television camera 10201, digital camera 10202 and the forward looking infrared 10203 in remote-control data receiver module 10101 and 10104 pairs of image capture devices 102 of unmanned aerial vehicle (UAV) control module, simultaneously, the condition of a disaster image that colored CCD television camera 10201 forward looking infrareds 10203 are collected can send view data laminating module 1010304 to, to be for further processing and to transmit.Digital camera 10202 captured the condition of a disaster images are stored in the memory device such as SD (Secure Digital Memory Card, safe digital card) card that carries at random, treat to obtain after unmanned plane 101 returns the wherein the condition of a disaster image of record.
Fig. 4 obtains the logic diagram of image analysis apparatus 2 in the system for the utility model the condition of a disaster, in the image analysis apparatus 2, mainly comprise the condition of a disaster image receiver module 201 and image processing system 202, wherein the condition of a disaster image receiver module 201 receives the condition of a disaster image that the device 1 of taking photo by plane transmits by wireless mode, and the condition of a disaster image sent to image processing system 202, the condition of a disaster image that 202 pairs of image processing systems receive carries out analyzing and processing.
Fig. 5 obtains the logic diagram of telechiric device 3 in the system for the utility model the condition of a disaster, telechiric device 3 mainly comprises host computer control device 301, telepilot 302, channel switching module 303 and remote-control data sending module 304, channel switching module 303 respectively with host computer control device 301, telepilot 302 and remote-control data sending module 304 are electrically connected, host computer control device 301 and telepilot 302 transmit control signal by the chain road direction of being made up of channel switching module 303 and remote-control data sending module 304 device of taking photo by plane respectively, and channel switching module 303 can be switched between host computer control device 301 and telepilot 302.
On no matter the current computer system still is software from hardware, all have very strong functions, therefore can utilize same computer equipment to carry out the work of host computer control device 301 and image processing system 202 simultaneously.As shown in Figure 6, host computer control device 301 has been formed computer control and image analysis system 4 jointly with image processing system 202, thereby has realized simultaneously the function to the analyzing and processing of the control of the device 1 of taking photo by plane and the condition of a disaster image.
Fig. 7 is arranged at the computer control on ground and the structural representation of image analysis system 4 in the present embodiment.As shown in Figure 7, the condition of a disaster image receiver module 201 is electrically connected with image analysis system 4 with computer control, computer control is electrically connected with remote-control data sending module 304 through channel switching module 303 again with image analysis system 4, telepilot 302 is connected with channel switching module 303 simultaneously, channel switching module 303 can be switched between computer control and image analysis system 4 and telepilot 302, to realize the flexible control to the device 1 of taking photo by plane.
Computer control and image analysis system 4 comprise PC104 computing machine 401, video frequency collection card 402, receive modulation module 403, image is recorded device 404, image display 405, navigational parameter display module 406 and keyboard and mouse assembly 407.Wherein, PC104 is a kind of industrial-controlled general line that defines for embedded Control specially, PC104 comes down to a kind of IEEE-P996 of compact, its signal definition and PC/AT basically identical, but it is electric fully different with mechanical specification, it is embedded control system a kind of optimization, small-sized, nesting structural embedded control, in the present embodiment, PC104 computing machine 401 has been held a concurrent post the task of image processing system 202 and host computer control device 301 simultaneously as the core of computer control and image analysis system 4.
In the present embodiment, the condition of a disaster image receiver module 201 is made up of remote measurement receiving antenna assembly 20101 and remote measurement receiving unit 20102.Remote measurement receiving antenna assembly 20101 receives unmanned plane 101 and sends remote measurement receiving unit 20102 to navigation information and the condition of a disaster image that wireless mode sends, remote measurement receiving unit 20102 sends the condition of a disaster image to image and records device 404 and record and preserve, simultaneously remote measurement receiving unit 20102 is respectively with the navigation information of the condition of a disaster image and unmanned plane 101, sending to PC104 computing machine 401 through video frequency collection card 402 with reception modulation module 403 handles, PC104 computing machine 401 shows the condition of a disaster image that receives by image display 405, and shows by the navigation information of 406 pairs of unmanned planes 101 of navigational parameter display module.
Can carry out straighforward operation by channel switching module 303 and the 304 pairs of unmanned planes of remote-control data sending module 101 that are electrically connected with PC104 computing machine 401 according to the received the condition of a disaster image of PC104 computing machine 401 and the navigation information of unmanned plane 101.Keyboard and mouse assembly 407 is connected with PC104 computing machine 401, so that the PC104 computing machine is operated.
In the present embodiment, PC104 computing machine 401 can carry out real-time picture mosaic to the real-time video that receives, the dynamic image data is provided, and can the logarithmic code camera 10202 photos of taking carry out follow-up picture mosaic and handle, so that clear, complete disaster area panorama picture mosaic to be provided, and can carry out target-region locating according to the navigation information of unmanned plane 101.
During work, unmanned plane 101 carries image capture device 102 gathers ground image according to setting navigation channel or remote control course line, carry out communication transmission by the condition of a disaster image receiver module 201 and remote-control data sending module 304 with computer control that is arranged at ground and image analysis system 4 by unmanned plane 101, computer control and image analysis system 4 receives and the instant resulting image of splicing and showing in real time, obtains the condition of a disaster fast, follows the tracks of the condition of a disaster, detects purpose such as road thereby reach.
By the photo that the SD cassette tape of digital camera returns, handle through splicing, form regional the condition of a disaster distribution plan, quick grasp the condition of a disaster distributes and the purpose of assessment the condition of a disaster thereby reach.
PC104 built-in computer corresponding function software is formed ground control and flight path control system, realizes man-machine interaction, thereby finishes manipulation and control to aircraft.Fig. 8 compiles processing flow chart for the condition of a disaster video image, as shown in Figure 8, inputted video image is through carrying out image mosaic after the parameter settings such as splicing cutting edge setting, display mode setting, character recognition are provided with, can carry out the multiframe positioning function as required, and will splice result's preservation, can splice result's playback afterwards; In addition, fill order's frame alignment function as required also, thus realize that impact point geo-location, impact point coordinate show, distance is measured between impact point, the impact point orientation shows, multiple target point mark and spininess sectional drawing function.After receiving, video image also can carry out video playback and video recording operation.
The utility model is taken a flight test in simulated earthquake disaster area, seismographic station, Bai Jia village and is taken test, and the photo after splicing and digital camera obtain has in real time all reached good effect; The shooting of taking a flight test in seismic region, Beichuan county town is tested, and has obtained Beichuan shake back the condition of a disaster overview image, has all possessed the condition of a disaster discrimination function on whole structure and the sharpness; In Han Wang's shooting of taking a flight test to the extreme environment of peaceful circuit, unclear at whole geological state, flight path is with under the definite situation of map entirely, carry out blind the flying to of halfhour approximately no signal in the gully and returned more than totally 40 kilometer, obtained the ground overview image of flight circuit equally, verified system-wide combination property, and and rugged environment in obtain the ability of the condition of a disaster fast.
The above only is preferred embodiment of the present utility model, and is in order to restriction the utility model, not all within spirit of the present utility model and principle, any modification of being done, is equal to replacement, improvement etc., all should be included within the protection domain of the present utility model.

Claims (9)

1. a condition of a disaster is obtained system, it is characterized in that: comprise the device of taking photo by plane, image analysis apparatus and telechiric device; Described telechiric device sends control information by wireless mode to the device of taking photo by plane; The described device of taking photo by plane is gathered the condition of a disaster image on ground according to the control information that receives from telechiric device, and sends the condition of a disaster image of gathering to image analysis apparatus; Described image analysis apparatus is analyzed the condition of a disaster image that receives from the device of taking photo by plane.
2. the condition of a disaster according to claim 1 is obtained system, it is characterized in that: the described device of taking photo by plane comprises unmanned plane and the image capture device that is arranged on the unmanned plane; Described telechiric device is controlled unmanned plane and image capture device, and described image capture device is gathered the condition of a disaster image and sent image analysis apparatus to by wireless mode.
3. the condition of a disaster according to claim 2 is obtained system, it is characterized in that: described unmanned plane comprises remote-control data receiver module, telemetry intelligence (TELINT) transmitter module, from model plane piece, unmanned aerial vehicle (UAV) control module and unmanned plane body; Described unmanned aerial vehicle (UAV) control module is carried out flight control from the control signal that telechiric device receives to the unmanned plane body according to the remote-control data receiver module; Be electrically connected with remote-control data receiver module, telemetry intelligence (TELINT) transmitter module and unmanned aerial vehicle (UAV) control module respectively from the model plane piece, described from model plane piece receiving satellite positioning signals and generate navigation information, and according to the control information that receives from the remote-control data receiver module, by the unmanned aerial vehicle (UAV) control module unmanned plane body is carried out automatic flight control, and navigation information is sent to image analysis apparatus by the telemetry intelligence (TELINT) transmitter module.
4. the condition of a disaster according to claim 3 is obtained system, it is characterized in that: describedly comprise GPS receiver module, navigation module, navigation modulation module and view data laminating module from the model plane piece; Described navigation module is electrically connected with GPS receiver module, remote-control data receiver module, view data laminating module, unmanned aerial vehicle (UAV) control module respectively, and is electrically connected with the telemetry intelligence (TELINT) transmitter module by navigation modulation module; Described view data laminating module is electrically connected with image capture device and telemetry intelligence (TELINT) transmitter module respectively; Described GPS receiver module receiving satellite positioning signals, and satellite positioning signal sent to the navigation module that is electrically connected with it; Described remote-control data receiver module receives the control information that telechiric device sends, and sends control information to be electrically connected with it navigation module; Described navigation module generates navigation information according to the satnav information that receives from the GPS receiver module, and according to navigation information and the control information that receives from the remote-control data receiver module, the unmanned aerial vehicle (UAV) control module sending controling instruction that Xiang Yuqi is electrically connected, the unmanned aerial vehicle (UAV) control module is carried out automatic flight control according to the steering order that receives from navigation module to the unmanned plane body; Described navigation module sends navigation information to the telemetry intelligence (TELINT) transmitter module through navigation modulation module, and navigation module directly sends navigation information to the view data laminating module; The telemetry intelligence (TELINT) transmitter module will send to image analysis apparatus wirelessly from the satellite positioning signal that navigation module receives; The locating information that the view data laminating module will receive from navigation module and bind from the condition of a disaster image that image capture device receives and to obtain the view data binding information, and sending the view data binding information to the telemetry intelligence (TELINT) transmitter module, the telemetry intelligence (TELINT) transmitter module will send to image analysis apparatus with wireless mode from the view data binding information that the view data laminating module receives.
5. the condition of a disaster according to claim 4 is obtained system, it is characterized in that: described image capture device comprises colored CCD television camera and/or digital camera and/or forward looking infrared.
6. the condition of a disaster according to claim 5 is obtained system, it is characterized in that: the control signal that described unmanned aerial vehicle (UAV) control module receives from telechiric device according to the remote-control data receiver module, colored CCD television camera, digital camera and forward looking infrared are controlled.
7. the condition of a disaster according to claim 5 is obtained system, it is characterized in that: described view data laminating module is bound colored CCD television camera and/or forward looking infrared shot image data with the locating information that receives from navigation module become the view data binding information.
8. obtain system according to each described the condition of a disaster of claim 1 to 7, it is characterized in that: described telechiric device comprises host computer control device, telepilot, channel switching module and remote-control data sending module, and described channel switching module is electrically connected with host computer control device, telepilot and remote-control data sending module respectively; Host computer control device and telepilot transmit control signal by the chain road direction of being made up of channel switching module and the remote-control data sending module device of taking photo by plane respectively, and channel switching module is switched between host computer control device and telepilot.
9. obtain system according to each described the condition of a disaster of claim 1 to 7, it is characterized in that: described image analysis apparatus comprises the condition of a disaster image receiver module and image processing system, described the condition of a disaster image receiver module receives the condition of a disaster image of the device transmission of taking photo by plane and sends to image processing system, and image processing system is handled the condition of a disaster image that receives.
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CN102589524A (en) * 2011-01-13 2012-07-18 华北电网有限公司北京超高压公司 Power line patrolling method
CN102745335A (en) * 2012-06-01 2012-10-24 广州市红鹏直升机遥感科技有限公司 Aerial shooting holder controller of aircraft and control method thereof
CN104156901A (en) * 2014-08-01 2014-11-19 江苏恒创软件有限公司 People searching and basic material conveying method based on unmanned aerial vehicle in special environment
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CN104317288A (en) * 2014-10-22 2015-01-28 陕西亿美万泰科技有限公司 Unmanned aerial vehicle system for police multipurpose surveillance
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CN102589524A (en) * 2011-01-13 2012-07-18 华北电网有限公司北京超高压公司 Power line patrolling method
CN102589524B (en) * 2011-01-13 2014-01-08 国家电网公司 Power line patrolling method
CN102745335A (en) * 2012-06-01 2012-10-24 广州市红鹏直升机遥感科技有限公司 Aerial shooting holder controller of aircraft and control method thereof
CN104156901A (en) * 2014-08-01 2014-11-19 江苏恒创软件有限公司 People searching and basic material conveying method based on unmanned aerial vehicle in special environment
CN104299365A (en) * 2014-08-06 2015-01-21 江苏恒创软件有限公司 Method for monitoring mountain landslide and debris flow in mountainous areas based on unmanned aerial vehicle
CN104299365B (en) * 2014-08-06 2017-01-04 江苏恒创软件有限公司 Monitoring landslide, mountain area, the method for mud-rock flow of based on unmanned plane
CN104317288A (en) * 2014-10-22 2015-01-28 陕西亿美万泰科技有限公司 Unmanned aerial vehicle system for police multipurpose surveillance
CN104955167A (en) * 2015-04-24 2015-09-30 览意科技(上海)有限公司 Connection method and system between model plane and remote controller
CN104955167B (en) * 2015-04-24 2018-11-06 览意科技(上海)有限公司 A kind of connection method between the model of an airplane and remote controler with connect system
CN105416584A (en) * 2015-11-12 2016-03-23 广州杰赛科技股份有限公司 Post-disaster life tracking unmanned aerial vehicle system
CN110209187A (en) * 2018-02-28 2019-09-06 广东奥信实业有限公司 A kind of 360 ° of adjustable mini mute unmanned plane camera systems

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