CN106603979A - Unmanned aerial vehicle image data real-time processing system and processing method based on electromechanics - Google Patents
Unmanned aerial vehicle image data real-time processing system and processing method based on electromechanics Download PDFInfo
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- CN106603979A CN106603979A CN201611152436.8A CN201611152436A CN106603979A CN 106603979 A CN106603979 A CN 106603979A CN 201611152436 A CN201611152436 A CN 201611152436A CN 106603979 A CN106603979 A CN 106603979A
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Closed-Circuit Television Systems (AREA)
- Image Processing (AREA)
Abstract
The invention discloses an unmanned aerial vehicle image data real-time processing system based on electromechanics in the electromechanical field. The system comprises a vehicle body, the top of the vehicle body is provided with a canard, the left sidewall and the right sidewall of the vehicle body are respectively provided with a fixed wing, the bottom of the vehicle body is provided with a rear wing, the bottom of the outer wall of the vehicle body is provided with two sets of empennages, the top of the outer wall of the vehicle body is provided with a streamer camera, the bottom of the streamer camera is provided with a main duct, an inner cavity of the main duct is provided with a motor, the outer wall of a power output terminal of the motor is uniformly provided with blades, the bottom of the blades is provided with a positioning device, the electrical output of the streamer camera is connected with a signal emission subsystem, and the electrical output of the signal emission subsystem is connected with a central processor. The flight device is a duct-type fixed-wing gas-electric hybrid power flight device, the flight duration time of the flight device is longer, long-time shooting of the ground is performed, and real-time image processing is realized.
Description
Technical field
The present invention relates to field of electromechanical technology, specially a kind of based on electromechanical unmanned plane image data real time processing system
And processing method.
Background technology
The image for obtaining ground target in real time by flight instruments is an importance in flight instruments operational exertion.
Flight instruments has to obtain the image of ground target in real time, to have the advantages that real-time is good, workable, when being applied to
Preliminary reconnaissance, real time reconnaissance, injure assessment etc. use.From the point of view of image processing point, flight instruments obtains in real time ground
The image of target is mainly used for interpretation analysis and localization process is most important.But flight instruments flying distance is not far, continuation of the journey
Time is not long, it is difficult to long-time shooting image.In view of problem mentioned above, a kind of unmanned plane based on electromechanics of present invention design
Image data real time processing system and processing method, it is mentioned above to solve the problems, such as.
The content of the invention
It is an object of the invention to provide a kind of based on electromechanical unmanned plane image data real time processing system and process side
Method, to solve above-mentioned background technology in propose flight instruments flying distance is not far, cruising time is not long, it is difficult to long-time shoots
The problem of image.
For achieving the above object, the present invention provides following technical scheme：A kind of unmanned plane image data reality based on electromechanics
When processing system, including fuselage is provided with front wing at the top of the fuselage, the left and right sides wall of the fuselage is provided with fixation
The wing, the bottom of the fuselage is provided with rear wing, and the outer wall bottom of the fuselage is provided with two groups of empennages, the outer wall top of the fuselage
Portion is provided with streamer camera, and the bottom of the streamer camera is provided with main duct, and the inner chamber of the main duct is provided with motor,
The outer wall of the motor power outfan is evenly arranged with blade, and the bottom of the blade is provided with position finder, the streamer
Camera electrically exports connection signal transmitting subsystem, and the signal transmitting subsystem electrically exports connection central processing unit, described
Respectively electrically output connects image processing subsystem, display subsystem and wireless telecommunications subsystem to central processing unit.
Preferably, the outer wall of two groups of fixed-wings, front wing and rear wings is provided with little duct.
Preferably, signal transmitting subsystem includes image acquisition units, the electrical company of output of described image collecting unit
Signal transmited processor is connect, the signal transmited processor is electrically input into respectively Connection Time data acquisition unit and position data
Electrically input connects position finder, the signal for collecting unit, the time data collecting unit and placement data acquisition unit
Respectively electrically output connects frame memory element and frame extraction unit to transmited processor, and the frame extraction unit electrically exports connection frame
Processing unit, the frame processing unit electrically exports connection high-frequency signal adjustment unit, and the high-frequency signal adjustment unit is electrical
Output connection signal transmitter unit.
Preferably, described image processing subsystem includes view data receiving unit, described image data receipt unit electricity
Property output connection image data processing unit, described image data processing unit electrically exports connection image processor, the figure
As processor, respectively electrically output connects image data memory cell, image flame detection unit, contour edge detector unit and edge
Breakpoint joint unit.
Preferably, the display subsystem includes signal receiving unit, and the signal receiving unit electrically exports connection letter
Number processing unit, the signal processing unit electrically exports connection signal pattern converting unit, the signal pattern converting unit
Electrically output connects video-stream processor, and respectively electrical output connection figure picture shows memory element and drives list the video-stream processor
Unit, the driver element electrically exports connection display.
Preferably, the wireless telecommunications subsystem includes radio receiving unit, the electrical company of output of the radio receiving unit
Wireless signal acquiring unit is connect, the wireless signal acquiring unit electrically exports connection wireless signal processing unit, described wireless
Signal processing unit electrically exports connecting communication processor, and the Communication processor electrically exports respectively connecting communication information Store
Unit, communication signal transmitter unit and input block, the input block electrically exports connection ground control terminal.
Electromechanical unmanned plane image data real-time processing method step should be based on as follows：
S1：Streamer camera is acquired by image acquisition units to ground image, and position finder is gathered by time data
Unit and placement data acquisition unit obtain the time data and position data of flight instruments, and signal transmited processor adopts image
The data of collection unit, time data collecting unit and placement data acquisition unit three collection are carried out by frame extraction unit to it
Packing framing, is processed the Frame after packing by frame processing unit, and high-frequency signal adjustment unit modulates Frame
To on high-frequency signal, and wireless transmit is carried out by signal transmitter unit, signal transmited processor by frame memory element will beat
Frame after bag is stored；
S2：View data receiving unit is received the view data that signal transmitter unit is launched, by view data
Processing unit is processed it, then by image processor respectively to image flame detection unit, contour edge detector unit and
Edge breakpoint joint unit carries out detection process, and image processor is deposited by image data memory cell to view data
Storage；
S3：Signal receiving unit is received the signal that signal transmitter unit is launched, then by signal processing unit
Signal to receiving is processed, and the signal after process is carried out view data conversion, display processing by signal pattern converting unit
Device is respectively increased driver element and display and the image after conversion is shown, video-stream processor shows that storage is single by image
Unit stores to view data；
S4：Radio receiving unit receives the data of signal transmitter unit transmitting and carries out wireless receiving, is adopted by wireless signal
Collection unit and wireless signal processing unit are acquired and process to the wireless signal for transmitting, and Communication processor is respectively by input
Unit and ground control terminal control input unit simultaneously carry out input control by Communication processor to it, and Communication processor passes through
Communication signal is controlled signal transmission to flight instruments by communication signal transmitter unit, and last Communication processor is by communicating letter
Breath memory element is stored communication information.
Compared with prior art, the invention has the beneficial effects as follows：This kind is located in real time based on electromechanical unmanned plane image data
Reason system and processing method, including the signal transmitting subsystem and image processing subsystem, display of earth station of flight instruments
System and wireless telecommunications subsystem, there is provided light stream camera obtains ground image and sends an image to earth station, ground station reception
Image and in real time place, image shows and remote input control, the flight instruments flying for culvert type fixed-wing oil electric mixed dynamic
Luggage is put, it is ensured that flight instruments flight cruising time is longer, and long-time shooting is carried out to ground and figure is carried out in real time
As processing.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is present system theory diagram；
Fig. 3 is that signal of the present invention launches subsystem theory diagram；
Fig. 4 is image processing subsystem theory diagram of the present invention；
Fig. 5 is display subsystem theory diagram of the present invention；
Fig. 6 is wireless telecommunications subsystem theory diagram of the present invention；
Fig. 7 is workflow diagram of the present invention.
In figure：1 fuselage, 2 front wings, 3 fixed-wings, 4 rear wings, 5 empennages, 6 position finders, 7 main ducts, 8 motor, 9 blades, 10
Streamer camera, 11 signals transmitting subsystem, 12 central processing units, 13 image processing subsystems, 14 display subsystems, 15 channel radios
News subsystem, 16 time data collecting units, 17 placement data acquisition units, 18 signal transmited processors, 19 image acquisition lists
Unit, 20 frame memory element, 21 frame extraction units, 22 frame processing units, 23 high-frequency signal adjustment units, 24 signal transmitter units,
25 view data receiving units, 26 image data processing units, 27 image processors, 28 image data memory cell, 29 images
Correcting unit, 30 contour edge detector units, 31 edge breakpoint joint units, 32 signal receiving units, 33 signal processing units,
34 signal pattern converting units, 35 video-stream processors, 36 images show memory element, 37 driver elements, 38 display, 39 wireless
Receiving unit, 40 wireless signal acquiring units, 41 wireless signal processing units, 42 Communication processors, the storage of 43 communication informations are single
Unit, 44 communication signal transmitter units, 45 input blocks, 46 ground control terminals.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than the embodiment of whole.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1-7 are referred to, the present invention provides a kind of technical scheme：By the front wing 2, rear wing 4 and the empennage that arrange on fuselage 1
5, to increase flight stability, motor 8 provides power, and motor 8 provides the energy by battery, and battery is rechargeable battery,
The blade 9 of main duct 7 has anti-twisted power guide functions, the rotating torque produced when rotating to the blade 9 for balancing main duct 7,
Produce the thrust that moves ahead, it is ensured that flight instruments flight cruising time is longer, and long-time is carried out to ground and shoot simultaneously in real time
Carry out image procossing, so as to solve above-mentioned background technology in propose flight instruments flying distance is not far, cruising time is not long,
The problem of long-time shooting image is difficult to, a kind of specific unmanned plane image data real time processing system based on electromechanics, including
Fuselage 1, the top of fuselage 1 is provided with front wing 2, and the left and right sides wall of fuselage 1 is provided with fixed-wing 3, and the bottom of fuselage 1 is arranged
There is a rear wing 4, the outer wall bottom of fuselage 1 is provided with two groups of empennages 5, front wing 2, rear wing 4 and empennage 5, to increase flight stability,
The outer wall top of fuselage 1 is provided with streamer camera 10, and streamer camera 10 is used for the intake of image on a surface target, streamer camera 10
Bottom be provided with main duct 7, the inner chamber of main duct 7 is provided with motor 8, and the outer wall of the clutch end of motor 8 uniformly sets
Blade 9 is equipped with, the blade 9 of main duct 7 has anti-twisted power guide functions, produces when rotating to the blade 9 for balancing main duct 7
Rotating torque, produces the thrust that moves ahead, it is ensured that flight instruments flight cruising time is longer, and the bottom of blade 9 is provided with position finder
6, for accurately being positioned to the region to be shot of streamer camera 10, the electrically output connection signal transmitting of streamer camera 10
Subsystem 11, electrically output connects central processing unit 12 to signal transmitting subsystem 11, and respectively electrically output connects central processing unit 12
Connect image processing subsystem 13, display subsystem 14 and wireless telecommunications subsystem 15.
Wherein, the outer wall of two groups of fixed-wings 3, front wing 2 and rear wings 4 is provided with little duct, and signal transmitting subsystem 11 is wrapped
Image acquisition units 19 are included, electrically output connects signal transmited processor 18, signal transmited processor 18 to image acquisition units 19
Connection Time data acquisition unit 16 and placement data acquisition unit 17, time data collecting unit 16 and position are electrically input into respectively
Put the electrical input connection position finder 6 of data acquisition unit 17, signal transmited processor 18 is by light stream camera 10 and the institute of position finder 6
The view data of collection, time data and position data are received and processed, and signal transmited processor 18 is electrically defeated respectively
Go out to connect frame memory element 20 and frame extraction unit 21, frame memory element 20 is stored the Frame after packing, frame is extracted
Unit 21 carries out packing framing to it, and electrically output connects frame processing unit 22 to frame extraction unit 21, to the Frame after packing
Processed, electrically output connects high-frequency signal adjustment unit 23 to frame processing unit 22, and high-frequency signal adjustment unit 23 is electrically defeated
Go out to connect signal transmitter unit 24, high-frequency signal adjustment unit 23 modulates Frame on high-frequency signal, and sends out by signal
Penetrating unit 24 carries out wireless transmit, and image processing subsystem 13 includes view data receiving unit 25, view data receiving unit
25 electrically export connection image data processing unit 26, and image data processing unit 26 electrically exports connection image processor 27,
Image processor 27 is launched signal transmitter unit 24 by view data receiving unit 25 and image data processing unit 26
View data is received and processed, and image processor 27 is respectively to image flame detection unit 29, the and of contour edge detector unit 30
Edge breakpoint joint unit 31 carries out detection process, and image data memory cell 28 is stored to view data, shows subsystem
System 14 includes signal receiving unit 32, and electrically output connects signal processing unit 33, signal processing unit to signal receiving unit 32
33 electrically export connection signal pattern converting unit 34, and signal pattern converting unit 34 electrically exports connection video-stream processor 35,
Video-stream processor 35 is sent out signal respectively by signal receiving unit 32, signal processing unit 33 and signal pattern converting unit 34
The signal for penetrating the transmitting of unit 24 is received, processed and image conversion, and respectively electrically output connection figure picture shows video-stream processor 35
Show memory element 36 and driver element 37, electrically output connects display 38 to driver element 37, after 38 pairs of conversions of display
Image shown that wireless telecommunications subsystem 15 includes radio receiving unit 39, the electrically output connection of radio receiving unit 39
Wireless signal acquiring unit 40, electrically output connects wireless signal processing unit 41, wireless signal to wireless signal acquiring unit 40
Processing unit 41 electrically exports connecting communication processor 42, and Communication processor 42 is adopted by radio receiving unit 39, wireless signal
Collection unit 40 and wireless signal processing unit 41 carry out wireless collection and process to the data that signal transmitter unit 24 is launched, and communicate
Processor 42 electrically exports respectively connecting communication information memory cell 43, communication signal transmitter unit 44 and input block 45, defeated
Enter the electrically output connection ground control terminal 46 of unit 45, ground control terminal 46 is by input block 45 to Communication processor 42
Input control is carried out, communication signal is controlled letter by Communication processor 42 by communication signal transmitter unit 44 to flight instruments
Number transmission, realizes remote control to unmanned plane, and communication information memory element 43 is entered communication information by Communication processor 42
Row storage.
A kind of unmanned plane image data real time processing system based on electromechanics, should be based on electromechanical unmanned plane image data reality
When process method step it is as follows：
S1：Streamer camera 10 is acquired by image acquisition units 19 to ground image, and position finder 6 passes through time data
Collecting unit 16 and placement data acquisition unit 17 obtain the time data and position data of flight instruments, signal transmited processor
18 data for gathering image acquisition units 19, time data collecting unit 16 and the three of placement data acquisition unit 17 pass through frame
Extraction unit 21 carries out packing framing to it, and the Frame after 22 pairs of packings of frame processing unit is processed, high-frequency signal
Adjustment unit 23 modulates Frame on high-frequency signal, and carries out wireless transmit, signal transmitting by signal transmitter unit 24
Processor 18 is stored the Frame after packing by frame memory element 20；
S2：View data receiving unit 25 is received the view data that signal transmitter unit 24 is launched, by image
Data processing unit 26 is processed it, then by image processor 27 respectively to image flame detection unit 29, contour edge
Detector unit 30 and edge breakpoint joint unit 31 carry out detection process, and image processor 27 passes through image data memory cell 28
View data is stored；
S3：Signal receiving unit 32 is received the signal that signal transmitter unit 24 is launched, then by signal processing
The signal of 33 pairs of receptions of unit is processed, and the signal after process is carried out view data conversion by signal pattern converting unit 34,
Video-stream processor 35 is respectively increased the image after the 38 pairs of conversions of driver element 37 and display and shows that video-stream processor 35 leads to
Cross image and show that memory element 36 is stored to view data；
S4：Radio receiving unit 39 receives the data of the transmitting of signal transmitter unit 24 and carries out wireless receiving, by wireless communication
The wireless signals of 41 pairs of transmission of number collecting unit 40 and wireless signal processing unit are acquired and process, 42 points of Communication processor
Input block 45 and the control input unit 45 of ground control terminal 46 and it Tong Guo be input into by Communication processor 42
Communication signal is controlled signal transmission by control, Communication processor 42 by communication signal transmitter unit 44 to flight instruments,
Last Communication processor 42 is stored communication information by communication information memory element 43.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding can carry out various changes, modification, replacement to these embodiments without departing from the principles and spirit of the present invention
And modification, the scope of the present invention be defined by the appended.
Claims (7)
1. a kind of unmanned plane image data real time processing system based on electromechanics, including fuselage (1), it is characterised in that：The machine
Front wing (2) is provided with the top of body (1), the left and right sides wall of the fuselage (1) is provided with fixed-wing (3), the fuselage (1)
Bottom be provided with rear wing (4), the outer wall bottom of the fuselage (1) is provided with two groups of empennages (5), the outer wall of the fuselage (1)
Top is provided with streamer camera (10), and the bottom of the streamer camera (10) is provided with main duct (7), the main duct (7)
Inner chamber is provided with motor (8), and the outer wall of motor (8) clutch end is evenly arranged with blade (9), the blade
(9) bottom is provided with position finder (6), and the streamer camera (10) electrically output connection signal transmitting subsystem (11) is described
Signal transmitting subsystem (11) electrically output connection central processing unit (12), respectively electrically output connects the central processing unit (12)
Connect image processing subsystem (13), display subsystem (14) and wireless telecommunications subsystem (15).
2. according to claim 1 a kind of based on electromechanical unmanned plane image data real time processing system, it is characterised in that：
The outer wall of two groups of fixed-wings (3), front wing (2) and rear wing (4) is provided with little duct.
3. according to claim 1 a kind of based on electromechanical unmanned plane image data real time processing system, it is characterised in that：
Signal transmitting subsystem (11) includes image acquisition units (19), and described image collecting unit (19) electrically believe by output connection
Number transmited processor (18), the signal transmited processor (18) respectively electrically input Connection Time data acquisition unit (16) and
Placement data acquisition unit (17), the time data collecting unit (16) and placement data acquisition unit (17) are electrically input into
Connection position finder (6), respectively electrically output connection frame memory element (20) and frame extract single to the signal transmited processor (18)
First (21), the frame extraction unit (21) electrically output connection frame processing unit (22), the frame processing unit (22) is electrically defeated
Go out to connect high-frequency signal adjustment unit (23), electrically output connects signal transmitter unit to the high-frequency signal adjustment unit (23)
(24)。
4. according to claim 1 a kind of based on electromechanical unmanned plane image data real time processing system, it is characterised in that：
Described image processing subsystem (13) includes view data receiving unit (25), and described image data receipt unit (25) is electrically defeated
Go out to connect image data processing unit (26), electrically output connects image processor to described image data processing unit (26)
(27), described image processor (27) respectively electrically output connection image data memory cell (28), image flame detection unit (29),
Contour edge detector unit (30) and edge breakpoint joint unit (31).
5. according to claim 1 a kind of based on electromechanical unmanned plane image data real time processing system, it is characterised in that：
The display subsystem (14) includes signal receiving unit (32), and the signal receiving unit (32) is electrically at output connection signal
Reason unit (33), the signal processing unit (33) electrically output connection signal pattern converting unit (34), the signal pattern
Electrical output connection video-stream processor (35) of converting unit (34), the video-stream processor (35) electrically exports respectively connection figure picture
Show memory element (36) and driver element (37), the driver element (37) electrically output connection display (38).
6. according to claim 1 a kind of based on electromechanical unmanned plane image data real time processing system, it is characterised in that：
The wireless telecommunications subsystem (15) includes radio receiving unit (39), and electrically output connects nothing to the radio receiving unit (39)
Line signal gathering unit (40), the wireless signal acquiring unit (40) electrically output connection wireless signal processing unit (41),
The wireless signal processing unit (41) electrically output connecting communication processor (42), the Communication processor (42) is electrical respectively
Output connecting communication information memory cell (43), communication signal transmitter unit (44) and input block (45), the input block
(45) electrically output connection ground control terminal (46).
7. a kind of based on electromechanical unmanned plane image data real-time processing method, it is characterised in that：Electromechanical unmanned plane should be based on
Image data real-time processing method step is as follows：
S1：Streamer camera (10) is acquired by image acquisition units (19) to ground image, and position finder (6) is by time number
The time data and position data of flight instruments, signal transmitting are obtained according to collecting unit (16) and placement data acquisition unit (17)
Processor (18) adopts image acquisition units (19), time data collecting unit (16) and placement data acquisition unit (17) three
The data of collection carry out packing framing by frame extraction unit (21) to it, the Frame after frame processing unit (22) is to packing
Processed, high-frequency signal adjustment unit (23) modulates Frame on high-frequency signal, and by signal transmitter unit (24)
Wireless transmit is carried out, signal transmited processor (18) is stored the Frame after packing by frame memory element (20)；
S2：View data receiving unit (25) is received the view data that signal transmitter unit (24) is launched, by image
Data processing unit (26) is processed it, then by image processor (27) respectively to image flame detection unit (29), wheel
Wide edge detection unit (30) and edge breakpoint joint unit (31) carry out detection process, and image processor (27) is by picture number
View data is stored according to memory element (28)；
S3：Signal receiving unit (32) is received the signal that signal transmitter unit (24) is launched, then by signal processing
Unit (33) is processed the signal for receiving, and the signal after process is carried out view data and turned by signal pattern converting unit (34)
Change, video-stream processor (35) is respectively increased driver element (37) and display (38) shows to the image after conversion, show
Processor (35) shows that memory element (36) is stored to view data by image；
S4：Radio receiving unit (39) receives the data of signal transmitter unit (24) transmitting and carries out wireless receiving, by wireless communication
Number collecting unit (40) and wireless signal processing unit (41) are acquired and process, Communication processor to the wireless signal for transmitting
(42) respectively by input block (45) and ground control terminal (46) control input unit (45) and by Communication processor
(42) input control is carried out to it, Communication processor (42) is by communication signal transmitter unit (44) by communication signal to flight dress
Put and be controlled signal transmission, last Communication processor (42) is deposited communication information by communication information memory element (43)
Storage.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611152436.8A CN106603979A (en) | 2016-12-14 | 2016-12-14 | Unmanned aerial vehicle image data real-time processing system and processing method based on electromechanics |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201611152436.8A CN106603979A (en) | 2016-12-14 | 2016-12-14 | Unmanned aerial vehicle image data real-time processing system and processing method based on electromechanics |
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| CN106603979A true CN106603979A (en) | 2017-04-26 |
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Cited By (1)
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| CN108521558A (en) * | 2018-04-10 | 2018-09-11 | 深圳慧源创新科技有限公司 | Unmanned plane figure transmission method, system, unmanned plane and unmanned plane client |
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| CN205203383U (en) * | 2015-12-17 | 2016-05-04 | 北京猎鹰无人机科技有限公司 | Unmanned aerial vehicle image data real -time processing system |
| CN205418106U (en) * | 2015-12-17 | 2016-08-03 | 北京猎鹰无人机科技有限公司 | Duct formula stationary vane oil -electricity hybrid vehicle unmanned aerial vehicle |
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| CN105480418A (en) * | 2015-12-17 | 2016-04-13 | 北京猎鹰无人机科技有限公司 | Ducted fixed-wing oil-electric hybrid unmanned aircraft |
| CN205203383U (en) * | 2015-12-17 | 2016-05-04 | 北京猎鹰无人机科技有限公司 | Unmanned aerial vehicle image data real -time processing system |
| CN205418106U (en) * | 2015-12-17 | 2016-08-03 | 北京猎鹰无人机科技有限公司 | Duct formula stationary vane oil -electricity hybrid vehicle unmanned aerial vehicle |
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| CN108521558A (en) * | 2018-04-10 | 2018-09-11 | 深圳慧源创新科技有限公司 | Unmanned plane figure transmission method, system, unmanned plane and unmanned plane client |
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Application publication date: 20170426 |