CN108496365A - Processing method, processing unit and the aircraft of image - Google Patents
Processing method, processing unit and the aircraft of image Download PDFInfo
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- CN108496365A CN108496365A CN201780005386.7A CN201780005386A CN108496365A CN 108496365 A CN108496365 A CN 108496365A CN 201780005386 A CN201780005386 A CN 201780005386A CN 108496365 A CN108496365 A CN 108496365A
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- 238000003672 processing method Methods 0.000 title claims abstract description 36
- 238000003384 imaging method Methods 0.000 claims abstract description 42
- 238000012544 monitoring process Methods 0.000 claims description 29
- 238000000034 method Methods 0.000 claims description 15
- 230000015572 biosynthetic process Effects 0.000 claims description 9
- 238000003786 synthesis reaction Methods 0.000 claims description 9
- 238000010586 diagram Methods 0.000 description 19
- 230000006870 function Effects 0.000 description 9
- 238000004891 communication Methods 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 230000005540 biological transmission Effects 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 241000208340 Araliaceae Species 0.000 description 2
- 235000005035 Panax pseudoginseng ssp. pseudoginseng Nutrition 0.000 description 2
- 235000003140 Panax quinquefolius Nutrition 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 235000008434 ginseng Nutrition 0.000 description 2
- 238000009825 accumulation Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 210000003733 optic disk Anatomy 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000001902 propagating effect Effects 0.000 description 1
Classifications
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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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N21/00—Selective content distribution, e.g. interactive television or video on demand [VOD]
- H04N21/40—Client devices specifically adapted for the reception of or interaction with content, e.g. set-top-box [STB]; Operations thereof
- H04N21/43—Processing of content or additional data, e.g. demultiplexing additional data from a digital video stream; Elementary client operations, e.g. monitoring of home network or synchronising decoder's clock; Client middleware
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/60—Control of cameras or camera modules
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/60—Control of cameras or camera modules
- H04N23/66—Remote control of cameras or camera parts, e.g. by remote control devices
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/80—Camera processing pipelines; Components thereof
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/95—Computational photography systems, e.g. light-field imaging systems
-
- 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
-
- 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)
- Multimedia (AREA)
- Signal Processing (AREA)
- Computing Systems (AREA)
- Theoretical Computer Science (AREA)
- Studio Devices (AREA)
- Image Processing (AREA)
Abstract
The invention discloses a kind of processing methods of image, are used for aircraft (100), imaging device (10) is provided on aircraft (100).Processing method includes step：(S22) control imaging device (10) is imaged to obtain image；And the system time of the aircraft (100) of (S24) when being imaged imaging device (10) is synthesized in image.The invention also discloses a kind of processing units of image (20) and a kind of aircraft (100).
Description
Technical field
The present invention relates to consumer electronics technology, more particularly to a kind of processing method of image, processing unit and aircraft.
Background technology
In the related art, it is usually that postmenstruation processing adds timestamp that aircraft, which is formed by video, still, such
Mode of operation is easy to cause that video corresponding time is inaccurate, and the confidence level of time showing reduces in video.
Invention content
The embodiment of the present invention provides a kind of processing method of image, processing unit and aircraft.
The present invention provides a kind of processing method of image, is used for aircraft, is provided with imaging device on the aircraft, institute
Processing method is stated to include the following steps：
The imaging device imaging is controlled to obtain image；With
The system time of the aircraft when imaging device is imaged is synthesized in described image.
The present invention provides a kind of processing unit of image, is used for aircraft, is provided with imaging device on the aircraft, institute
Stating processing unit includes：
Control module, the control module is for controlling the imaging device imaging to obtain image；With
First processing module, the first processing module are for aircraft when being imaged the imaging device
The system time is synthesized in described image.
The aircraft of embodiment of the present invention includes imaging device and the processing unit.
When imaging device is imaged by processing method, processing unit and the aircraft of the image of embodiment of the present invention in real time
The system time of aircraft be synthesized in image, to ensure the accuracy and confidence level of time showing in image.
The additional aspect and advantage of embodiments of the present invention will be set forth in part in the description, partly will be from following
Description in become apparent, or the practice of embodiment through the invention is recognized.
Description of the drawings
The above-mentioned and/or additional aspect and advantage of the present invention is from combining in description of the following accompanying drawings to embodiment by change
It obtains obviously and is readily appreciated that, wherein：
Fig. 1 is the flow diagram of the processing method of the image of embodiment of the present invention；
Fig. 2 is the high-level schematic functional block diagram of the aircraft of embodiment of the present invention；
Fig. 3 is another flow diagram of the processing method of the image of embodiment of the present invention；
Fig. 4 is the high-level schematic functional block diagram of the first processing module of embodiment of the present invention；
Fig. 5 is another flow diagram of the processing method of the image of embodiment of the present invention；
Fig. 6 is another high-level schematic functional block diagram of the first processing module of embodiment of the present invention；
Fig. 7 is another flow diagram of the processing method of the image of embodiment of the present invention；
Fig. 8 is another high-level schematic functional block diagram of the aircraft of embodiment of the present invention；
Fig. 9 is another high-level schematic functional block diagram of the first processing module of embodiment of the present invention；
Figure 10 is another flow diagram of the processing method of the image of embodiment of the present invention；
Figure 11 is the high-level schematic functional block diagram of the processing unit of embodiment of the present invention；
Figure 12 is another flow diagram of the processing method of the image of embodiment of the present invention；
Figure 13 is the schematic diagram of the aircraft and terminal communication of embodiment of the present invention；
Figure 14 is another high-level schematic functional block diagram of the processing unit of embodiment of the present invention；
Figure 15 is another flow diagram of the processing method of the image of embodiment of the present invention；
Figure 16 is the schematic diagram of the image transmitting of embodiment of the present invention；
Figure 17 is another high-level schematic functional block diagram of the processing unit of embodiment of the present invention；
Figure 18 is another flow diagram of the processing method of the image of embodiment of the present invention；
Figure 19 is another schematic diagram of the image transmitting of embodiment of the present invention.
Main element symbol illustrates：
Aircraft 100, imaging device 10, processing unit 20, control module 22, the processing of first processing module 24, first are single
Member 242, second processing unit 244, third processing unit 246, processing subelement 2462, fourth processing unit 248, second processing
Module 26, third processing module 28, fourth processing module 29, positioning device 30, remote controler 500, transit terminal 600, high in the clouds clothes
Business device 700, terminal 800, display 80, monitoring client 900.
Specific implementation mode
Embodiments of the present invention are described below in detail, the example of the embodiment is shown in the accompanying drawings, wherein from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining the present invention, and is not considered as limiting the invention.
In the description of the present invention, it is to be understood that, term " first ", " second " are used for description purposes only, and cannot
It is interpreted as indicating or implies relative importance or implicitly indicate the quantity of indicated technical characteristic.Define as a result, " the
One ", the feature of " second " can explicitly or implicitly include one or more feature.In description of the invention
In, the meaning of " plurality " is two or more, unless otherwise specifically defined.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be to be electrically connected or can be in communication with each other to be mechanical connection；It can be directly connected, it can also be by between intermediary
It connects connected, can be the interaction relationship of the connection or two elements inside two elements.For the ordinary skill of this field
For personnel, the specific meanings of the above terms in the present invention can be understood according to specific conditions.
Following disclosure provides many different embodiments or example is used for realizing the different structure of the present invention.In order to
Simplify disclosure of the invention, hereinafter the component of specific examples and setting are described.Certainly, they are merely examples, and
And it is not intended to limit the present invention.In addition, the present invention can in different examples repeat reference numerals and/or reference letter,
This repetition is for purposes of simplicity and clarity, itself not indicate between discussed various embodiments and/or setting
Relationship.In addition, the present invention provides various specific techniques and material example, but those of ordinary skill in the art can be with
Recognize the application of other techniques and/or the use of other materials.
Embodiments of the present invention are described below in detail, the example of the embodiment is shown in the accompanying drawings, wherein from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining the present invention, and is not considered as limiting the invention.
Also referring to Fig. 1 and Fig. 2, the processing method of the image of embodiment of the present invention can be used for aircraft 100.Fly
Imaging device 10 is provided on row device 100.The processing method of image includes the following steps：
S22：The imaging of imaging device 10 is controlled to obtain image；With
S24：The system time of aircraft 100 when imaging device 10 is imaged is synthesized in image.
Referring to Fig. 2, the processing unit 20 of image can be used for aircraft 100.Imaging is provided on aircraft 100
Device 10.Processing unit 20 includes control module 22 and first processing module 24.Control module 22 is for controlling imaging device 10
Imaging is to obtain image.The system time synthesis of aircraft 100 when first processing module 24 is used to imaging device 10 being imaged
Into image.
In other words, the processing method of embodiment of the present invention can be real by the processing unit 20 of embodiment of the present invention
It is existing, wherein step S22 can be realized that step S24 can be realized by first processing module 24 by control module 22.
In some embodiments, the processing unit 20 of embodiment of the present invention can be applied to embodiment of the present invention
Aircraft 100, in other words the aircraft 100 of embodiment of the present invention include the processing unit 20 of embodiment of the present invention.In addition,
The aircraft 100 of embodiment of the present invention further includes imaging device 10, and imaging device 10 and processing unit 20 are electrically connected.
Processing method, processing unit 20 and the aircraft 100 of the image of embodiment of the present invention are in real time by imaging device
The system time of aircraft 100 when 10 imaging is synthesized in image, to ensure in image the accuracy of time showing and credible
Degree.
It is appreciated that when imaging device 10 is imaged, there are corresponding imaging time, i.e., corresponding aircraft per frame image
100 system time will be synthesized to per the corresponding imaging time of frame image in image, it can be ensured that can accurately and rapidly obtain
Imaging time per frame image, need to know the occasion of accurate image imaging time certain, such as live streaming, prison in real time
When control or exploration, image that the processing method of embodiment of the present invention, processing unit 20 and aircraft 100 obtain at
As the time has higher accuracy and confidence level.
In some embodiments, aircraft 100 includes unmanned vehicle.
Referring to Fig. 3, in some embodiments, step S24 includes the following steps：
S242：Convert system time to character string；With
S244：Image is handled so that character string to be written in image.
Referring to Fig. 4, in some embodiments, first processing module 24 includes at first processing units 242 and second
Manage unit 244.First processing units 242 are used to convert system time to character string.Second processing unit 244 is schemed for handling
As character string to be written in image.
In other words, step S242 can be realized by first processing units 242, and step S244 can be by second processing unit
244 realize.
In this way, can closely be combined together image and corresponding system time, occur when the later stage being avoided to synthesize
Error and prevent data to be tampered.
Specifically, the system time of every frame image is converted to character string by processing unit 20, then character string is write direct
The corresponding image data of image, for example in image pixel, corresponding system time is synthesized in image when to which image being imaged.
Referring to Fig. 5, in some embodiments, step S24 includes the following steps：
S246：System time is updated to obtain updated system time；With
S248：Updated system time is synthesized in image.
Referring to Fig. 6, in some embodiments, first processing module 24 include third processing unit 246 and the everywhere
Manage unit 248.Third processing unit 246 is for updating system time to obtain updated system time.Fourth processing unit
248 for updated system time to be synthesized in image.
In other words, step S246 can be realized that step S248 can be by fourth processing unit by third processing unit 246
248 realize.
In this way, can be obtained as system time, so that it is guaranteed that the standard of system time more accurate, the more authoritative time
True property and confidence level.
It is appreciated that the system time of aircraft 100 is as time goes by, it is understood that there may be large error, in order to protect
The accuracy for demonstrate,proving system time, needs to be updated system time, to reduce error, improves the confidence level of system time.
Also referring to Fig. 7 and Fig. 8, in some embodiments, aircraft 100 includes positioning device 30.Step S246
Include the following steps：
S2462：The time of the acquisition of positioning device 30 is handled as updated system time.
Also referring to Fig. 8 and Fig. 9, in some embodiments, aircraft 100 includes positioning device 30.Third processing
Unit 246 includes processing subelement 2462.Processing subelement 2462 is used to handle the time of the acquisition of positioning device 30 as update
System time afterwards.
In other words, step S2462 can be realized by processing subelement 2462.
In this way, can be updated to system time by the time that positioning device 30 obtains, to improve system time
Accuracy and confidence level.
It is appreciated that the timer inside aircraft 100 is since there is certain errors, error is smaller in a short time,
System time is more accurate, can be used normally, but passes through the accumulation of time, and error, which becomes conference, causes the time inaccurate, institute
To need to obtain more correct time using as system time by positioning device 30, such as GPS positioning device.GPS is fixed
Position device can send the request for obtaining the time to the satellite communicated with GPS positioning device, and receive the time conduct of satellite transmission
Updated system time.
Referring to Fig. 10, in some embodiments, processing method includes the following steps：
S26：There is the image of system time to encode synthesis.
1 is please referred to Fig.1, in some embodiments, processing unit 20 includes Second processing module 26.Second processing module
26 for having the image of system time to encode synthesis.
In other words, step S26 can be realized by Second processing module 26.
In this way, the efficiency of transmission of image can be improved.
It is appreciated that in image transmitting process, generally all image will not be directly transmitted, but it is advanced to image
Row coding is to generate smaller image file, to improve the efficiency of transmission of image.Also image can be carried out in an encoding process
Encryption ensures the safety of image data transmission.
Also referring to Figure 12 and Figure 13, in some embodiments, aircraft 100 is communicated with terminal 800.Terminal 800
Including display 80 and terminal time, display 80 is used to show the image that synthesis has system time.Processing method includes following
Step：
S28：Comparison terminal time and system time are to obtain delay time.
Also referring to Figure 13 and Figure 14, in some embodiments, aircraft 100 is communicated with terminal 800, terminal 800
Including display 80 and terminal time, display 80 is used to show that synthesis to have the image of system time, and processing unit 20 includes the
Three processing modules 28.Third processing module 28 is for comparison terminal time and system time to obtain delay time.
In other words, step S28 can be realized by third processing module 28.
In this way, the time difference of system time and terminal time can be obtained.
Specifically, by comparing the time difference of system time and terminal time, delay time can be obtained using as long-range
The slowed-down video of monitoring, to accurately grasp the time of monitoring.
In some embodiments, terminal 800 includes terminal handler, and terminal handler is for the comparison terminal time and is
The time unite to obtain delay time, i.e., step S28 can be realized by terminal handler, not do any restrictions herein.
Further, delay time may be displayed on display 80.
In some embodiments, when showing image, system time is also simultaneously displayed in image.In one example,
The format of the system time of display is：When year-month-day：Point：Second.
Also referring to Figure 15 and Figure 16, in some embodiments, aircraft 100 is communicated with remote controler 500, remote controler
500 communicate with monitoring client 900.Processing method includes the following steps：
S29：Image is passed sequentially through into aircraft 100 and remote controler 500 is sent to monitoring client 900.
Also referring to Figure 16 and Figure 17, in some embodiments, aircraft 100 is communicated with remote controler 500, remote controler
500 communicate with monitoring client 900.Processing unit 20 includes fourth process processing module 29.Fourth processing module 29 is used for image
It passes sequentially through aircraft 100 and remote controler 500 is sent to monitoring client 900.
In other words, step S29 can be realized by fourth processing module 29.
In this way, aircraft 100 can directly send images to monitoring client 900 by remote controler 500.
In some embodiments, monitoring client 900 and 500 direct communication of remote controler, aircraft 100 (such as unmanned flight
Device) it is usually to carry out direct communication with remote controler 500, therefore aircraft 100 can send images to prison by remote controler 500
End 900 is controlled, monitoring client 900 can be obtained every frame image system time corresponding with per frame image by being decoded to image.
In one example, monitoring client 900 is client, that is, monitors the display end of 100 local environment of aircraft.
Also referring to Figure 18 and Figure 19, in some embodiments, remote controler 500 passes through transit terminal 600 and high in the clouds
Server 700 is communicated with monitoring client 900.Processing method includes the following steps：
S31：Image is passed sequentially through into remote controler 500, transit terminal 600 and cloud server 700 and is sent to monitoring client
900。
Referring to Figure 17 and Figure 19, in some embodiments, remote controler 500 passes through transit terminal 600 and high in the clouds
Server 700 is communicated with monitoring client 900.Fourth processing module 29 is additionally operable to image passing sequentially through remote controler 500, transit terminal
600 and cloud server 700 be sent to monitoring client 900.
In other words, step S31 can also be realized by fourth processing module 29.
In this way, aircraft 100 can be sent image by remote controler 500, transit terminal 600 and cloud server 700
To monitoring client 900.
In some embodiments, monitoring client 900 is in remote monitoring, can not be with 500 direct communication of remote controler, and flies
Device 100 is usually to carry out direct communication with remote controler 500, therefore remote controler 500 can pass through (such as the base station of transit terminal 600
Or intelligent terminal, intelligent terminal include mobile phone, tablet computer etc.) and cloud server will from the image of aircraft 100 send
To monitoring client 900, i.e., image is according to 600 → cloud server of aircraft 100 → remote controler, 500 → transit terminal 700 → monitoring
The process transmission at end 900, monitoring client 900 can be obtained every frame image system corresponding with per frame image by being decoded to image
It unites the time.
In the description of this specification, reference term " embodiment ", " some embodiments ", " schematically implementation
What the description of mode ", " example ", " specific example " or " some examples " etc. meant to describe in conjunction with the embodiment or example
Particular features, structures, materials, or characteristics are contained at least one embodiment or example of the present invention.In this specification
In, schematic expression of the above terms are not necessarily referring to identical embodiment or example.Moreover, the specific spy of description
Sign, structure, material or feature can be combined in any suitable manner in any one or more embodiments or example.
Any process described otherwise above or method description are construed as in flow chart or herein, and expression includes
Module, segment or the portion of the code of one or more executable instructions for the step of executing specific logical function or process
Point, and the range of the preferred embodiment of the present invention includes other execution, wherein can not press shown or discuss suitable
Sequence, include according to involved function by it is basic simultaneously in the way of or in the opposite order, to execute function, this should be of the invention
Embodiment person of ordinary skill in the field understood.
Expression or logic and/or step described otherwise above herein in flow charts, for example, being considered use
In the order list for the executable instruction for executing logic function, can specifically execute in any computer-readable medium, for
Instruction execution system, device or equipment (system of such as computer based system including processor or other can be held from instruction
The instruction fetch of row system, device or equipment and the system executed instruction) it uses, or combine these instruction execution systems, device or set
It is standby and use.For the purpose of this specification, " computer-readable medium " can any can be included, store, communicating, propagating or passing
Defeated program is for instruction execution system, device or equipment or the dress used in conjunction with these instruction execution systems, device or equipment
It sets.The more specific example (non-exhaustive list) of computer-readable medium includes following：Electricity with one or more wiring
Interconnecting piece (electronic device), portable computer diskette box (magnetic device), random access memory (RAM), read-only memory
(ROM), erasable edit read-only storage (EPROM or flash memory), fiber device and portable optic disk is read-only deposits
Reservoir (CDROM).In addition, computer-readable medium can even is that the paper that can print described program on it or other are suitable
Medium, because can be for example by carrying out optical scanner to paper or other media, then into edlin, interpretation or when necessary with it
His suitable method is handled electronically to obtain described program, is then stored in computer storage.
It should be appreciated that each section of the present invention can be executed with hardware, software, firmware or combination thereof.Above-mentioned
In embodiment, software that multiple steps or method can in memory and by suitable instruction execution system be executed with storage
Or firmware executes.It, and in another embodiment, can be under well known in the art for example, if executed with hardware
Any one of row technology or their combination execute：With the logic gates for executing logic function to data-signal
Discrete logic, with suitable combinational logic gate circuit application-specific integrated circuit, programmable gate array (PGA), scene
Programmable gate array (FPGA) etc..
Those skilled in the art are appreciated that execute all or part of step that above-mentioned implementation carries
It is that relevant hardware can be instructed to complete by program, the program can be stored in a kind of computer readable storage medium
In, which includes the steps that one or a combination set of embodiment of the method when being executed.
In addition, each functional unit in each embodiment of the present invention can be integrated in a processing module, it can also
That each unit physically exists alone, can also two or more units be integrated in a module.Above-mentioned integrated mould
The form that hardware had both may be used in block executes, and can also be executed in the form of software function module.The integrated module is such as
Fruit is executed in the form of software function module and when sold or used as an independent product, can also be stored in a computer
In read/write memory medium.
Storage medium mentioned above can be read-only memory, disk or CD etc..Although having been shown and retouching above
The embodiment of the present invention is stated, it is to be understood that above-described embodiment is exemplary, and should not be understood as the limit to the present invention
System, those skilled in the art can be changed above-described embodiment, change, replace and become within the scope of the invention
Type.
Claims (17)
1. a kind of processing method of image is used for aircraft, is provided with imaging device on the aircraft, which is characterized in that institute
Processing method is stated to include the following steps：
The imaging device imaging is controlled to obtain image；With
The system time of the aircraft when imaging device is imaged is synthesized in described image.
2. processing method as described in claim 1, which is characterized in that flight when being imaged the imaging device
The system time of device is synthesized to the step in described image and includes the following steps：
Convert the system time to character string；With
Described image is handled so that the character string to be written in described image.
3. processing method as described in claim 1, which is characterized in that flight when being imaged the imaging device
The system time of device is synthesized to the step in described image and includes the following steps：
The system time is updated to obtain the updated system time；With
The updated system time is synthesized in described image.
4. processing method as claimed in claim 3, which is characterized in that the aircraft includes positioning device, the update institute
The step of system time is to obtain the updated system time is stated to include the following steps：
The time of the positioning device acquisition is handled as the updated system time.
5. processing method as described in claim 1, which is characterized in that the treating method comprises following steps：
There is the described image of the system time to encode synthesis.
6. processing method as described in claim 1, which is characterized in that the aircraft is communicated with terminal, and the terminal includes
Display and terminal time, the display are used to show the described image that synthesis has the system time, the processing method
Include the following steps：
Compare the terminal time and the system time to obtain delay time.
7. processing method as described in claim 1, which is characterized in that the aircraft is communicated with remote controler, the remote controler
It is communicated with monitoring client, the treating method comprises following steps：
Described image is passed sequentially through into the aircraft and the remote controler is sent to the monitoring client.
8. processing method as claimed in claim 7, which is characterized in that the remote controler passes through transit terminal and cloud server
It is communicated with the monitoring client, the treating method comprises following steps：
Described image is passed sequentially through into the remote controler, the transit terminal and the cloud server and is sent to the monitoring
End.
9. a kind of processing unit of image is used for aircraft, is provided with imaging device on the aircraft, which is characterized in that institute
Stating processing unit includes：
Control module, the control module is for controlling the imaging device imaging to obtain image；With
First processing module, when the first processing module is used for the system of aircraft when being imaged the imaging device
Between be synthesized in described image.
10. processing unit as claimed in claim 9, which is characterized in that the first processing module includes：
First processing units, the first processing units are used to convert the system time to character string；With
Second processing unit, the second processing unit is for handling described image so that described image is written in the character string
In.
11. processing unit as claimed in claim 9, which is characterized in that the first processing module includes：
Third processing unit, the third processing unit is for when updating the system time to obtain the updated system
Between；With
Fourth processing unit, the fourth processing unit is for the updated system time to be synthesized in described image.
12. processing unit as claimed in claim 11, which is characterized in that the aircraft includes positioning device, the third
Processing unit includes：
Subelement is handled, the processing subelement is used to handle the time of the positioning device acquisition as the updated system
It unites the time.
13. processing unit as claimed in claim 9, which is characterized in that the processing unit includes：
Second processing module, the Second processing module are used to have the described image of the system time to encode synthesis.
14. processing unit as claimed in claim 9, which is characterized in that the aircraft is communicated with terminal, and the terminal includes
Display and terminal time, the display are used to show the described image that synthesis has the system time, the processing unit
Including：
Third processing module, the third processing module is for the terminal time and the system time to be postponed
Time.
15. processing unit as claimed in claim 9, which is characterized in that the aircraft is communicated with remote controler, the remote controler
It is communicated with monitoring client, the processing unit includes：
Fourth processing module, the fourth processing module are used to described image passing sequentially through the aircraft and the remote controler
It is sent to the monitoring client.
16. processing unit as claimed in claim 15, which is characterized in that the remote controler passes through transit terminal and cloud service
Device is communicated with the monitoring client, the fourth processing module be additionally operable to by described image pass sequentially through the remote controler, it is described in
Turn terminal and the cloud server is sent to the monitoring client.
17. a kind of aircraft, which is characterized in that including：
Imaging device；With
Processing unit as described in claim 9-16 any one.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2017/074817 WO2018152783A1 (en) | 2017-02-24 | 2017-02-24 | Image processing method and device, and aircraft |
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| CN112399081A (en) * | 2020-11-03 | 2021-02-23 | 深圳市中博科创信息技术有限公司 | Method and system for integrally transmitting image data and control data |
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