CN109087275A - Computer estimation method - Google Patents
Computer estimation method Download PDFInfo
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- CN109087275A CN109087275A CN201810233102.6A CN201810233102A CN109087275A CN 109087275 A CN109087275 A CN 109087275A CN 201810233102 A CN201810233102 A CN 201810233102A CN 109087275 A CN109087275 A CN 109087275A
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T7/00—Image analysis
- G06T7/0002—Inspection of images, e.g. flaw detection
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q50/00—Systems or methods specially adapted for specific business sectors, e.g. utilities or tourism
- G06Q50/10—Services
- G06Q50/26—Government or public services
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T7/00—Image analysis
- G06T7/90—Determination of colour characteristics
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B17/00—Monitoring; Testing
- H04B17/30—Monitoring; Testing of propagation channels
- H04B17/309—Measuring or estimating channel quality parameters
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/18502—Airborne stations
- H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service
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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
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T2207/00—Indexing scheme for image analysis or image enhancement
- G06T2207/30—Subject of image; Context of image processing
- G06T2207/30196—Human being; Person
Abstract
The present invention relates to a kind of computer estimation methods, this method includes providing a kind of rescue capacity calculation machine assessment system immediately, under the mode of the analysis of image overall brightness and adaptable image procossing, the subgraph for obtaining accurately human body to be succoured carries out bodily form analysis, to determine the corresponding human body weight of each subgraph, human body total load to be succoured is determined based on the multiple human body subgraph, to determine whether the aircraft can succour the judgement information of all personnel that meet with misfortune.
Description
Technical field
The present invention relates to computer field more particularly to a kind of computer estimation methods.
Background technique
With the appearance of microprocessor (CPU), begin to use microprocessor in computer, makes computer volume-diminished
, cost reduces.On the other hand, the rapid development of Software Industry improves the convenient degree of computer internal operation system, meter
Calculation machine external equipment also tends to be perfect.Computer theory and technical constantly improve promote microcomputer to penetrate into quickly entirely
In the various industries and department of society, and become the requirement of people's living and studying.Over 40 years, the volume of computer is continuous
Diminution, desktop computer, laptop, palm PC, tablet computer volume be gradually miniaturized, and provides convenient and fast clothes for people
Business.Therefore, future computer still can constantly tend to be miniaturized, and volume will be smaller and smaller.
Internet links together computer all over the world, thence into Internet era.Computer network
Human world is revolutionized, people are linked up by internet, exchange (OICQ, microblogging etc.), shared education resources (document
Access, long-distance education etc.), information consult shared (Baidu, Google) etc., the especially appearance of wireless network greatly improves
People use the convenience of network, and future computer will further develop in terms of networking.
Summary of the invention
The present invention provides a kind of computer estimation method, in the analysis of image overall brightness and adaptable image procossing
Under mode, the subgraph for obtaining accurately human body to be succoured carries out bodily form analysis, to determine the corresponding human body of each subgraph
Weight determines human body total load to be succoured based on the multiple human body subgraph, particular, it is important that also by aircraft bearing load
Threshold value subtracts whether target total load in human body total load to be succoured and cabin can be sought to obtain operation result with the determining aircraft
Rescue the judgement information of all personnel that meet with misfortune.
For this purpose, the present invention at least has the important inventive point of following two:
(1) target total load in the human body total load to be succoured and the cabin is subtracted based on aircraft bearing load threshold value
Operation result is accurately judged to aircraft and can succour completely need to be succoured human body, and notifies in time when that can not succour completely
Rear is rescued, to ensure that the validity and reliability of rescue action;
(2) in the analytical judgment of image overall brightness, the object pixel in image to be processed is selected using Lie groupoid
Point and the mechanism analyzed of ratio using the color component to target pixel points, to effectively prevent image entirety
The erroneous judgement of brightness, and the number of tiles cut to the high-definition image is determined based on the current comparison reference, together
When determine based on the degree of roughness of each images fragment itself and execute the dynamics of image smoothing to described image fragment, thus real
The picture smooth treatment based on image content itself is showed.
According to an aspect of the present invention, a kind of computer estimation method is provided, this method includes providing a kind of battalion immediately
Capacity calculation machine assessment system is rescued, under the mode of the analysis of image overall brightness and adaptable image procossing, is obtained accurate
The subgraph of human body to be succoured carries out bodily form analysis, to determine the corresponding human body weight of each subgraph, based on the multiple
Human body subgraph determines human body total load to be succoured, to determine whether the aircraft can succour the judgement letter of all personnel that meet with misfortune
Breath, the instant rescue capacity calculation machine assessment system include:
Camera out of my cabin, setting aboard, for shooting to scene outside aircraft cabin, are schemed out of my cabin immediately with obtaining
Picture exports the instant image out of my cabin;
Camera in cabin is arranged in aircraft cabin, for being shot the scene in cabin to obtain engine room inside
Image;
Curve pixel analysis equipment is connect with the camera out of my cabin, for receiving the instant image out of my cabin, with described
Immediately the center of the horizontal direction in image is classified as Y-axis out of my cabin, with the central row of the vertical direction in the instant image out of my cabin
For X-axis, Lie groupoid is depicted in image described based on the X-axis and the Y-axis out of my cabin immediately, and will it is described it is instant out of my cabin
Each pixel that Lie groupoid passes through in image obtains the red green of the multiple target pixel points as multiple target pixel points
Signal component value, black and white signal component value and champac signal component value, and following operation is done for each target pixel points: red green signal component value is removed
Target point is obtained divided by the results added of black and white signal component value with the result of black and white signal component value and champac signal component value
Ratio value, after being also used to for the ratio values of the multiple target pixel points being added divided by the quantity of the multiple target pixel points with
Obtain current comparison reference;
Fragment decision device is connect, for receiving respectively with the camera out of my cabin and the curve pixel analysis equipment
The current comparison reference and the instant image out of my cabin, are determined based on the current comparison reference to the instant cabin
The number of tiles that outer image is cut, wherein the current comparison reference is bigger, cuts to the instant image out of my cabin
The number of tiles arrived is fewer;
Fragment processing equipment is connect with the fragment decision device, for receiving the number of tiles, and based on described broken
Sheet data is to the fragment cutting process of image progress out of my cabin immediately, to obtain and export multiple images fragment;
Piece smoothing arrangement is morcelled, connect with the fragment processing equipment, for receiving described multiple images fragment, and is based on
The degree of roughness of each images fragment itself determines the dynamics that image smoothing is executed to described image fragment, and by multiple execution
The images fragment of complete picture smooth treatment is compound to morcel piece smoothed image to obtain;
Body detection device is connect with the piece smoothing arrangement of morcelling, and described morcels piece smoothed image, and base for receiving
It obtains and divides from described morcel in piece smoothed image in default human body upper limit gray threshold and default human body lower limit gray threshold
Multiple human body subgraphs out;
Load Analysis equipment, setting aboard, are connect with the camera out of my cabin and the body detection device respectively,
Bodily form analysis is carried out for receiving multiple human body subgraphs and instant image out of my cabin, and to each human body subgraph, with determination
Each corresponding human body weight of human body subgraph determines human body total load to be succoured based on the multiple human body subgraph.
Detailed description of the invention
Embodiment of the present invention is described below with reference to attached drawing, in which:
Fig. 1 is the structural block diagram according to the instant rescue capacity calculation machine assessment system shown in embodiment of the present invention.
Camera in cabin
Fig. 2 is according to camera in the cabin of the instant rescue capacity calculation machine assessment system shown in embodiment of the present invention
Structural schematic diagram.
Specific embodiment
Embodiment of the present invention is described in detail below with reference to accompanying drawings.
In order to help the sea personnel that meet with misfortune to be succoured as early as possible, various countries are directed to marine accident, are all provided with corresponding marine
Search and rescue center.
China Maritime Search & Rescue Center is found in 1989, is responsible for the organization of unity co-ordination of whole nation maritime search and rescue, daily
Work is undertaken by Safety Supervision Bureau of Ministry of Communications (existing CHINA MSA).It plays and ensures social stability, promote maritime traffic cause
Development, marine resources exploitation and comprehensive utilization to ocean, and then promote the economic development of country, improve the sound of government
The significant role of reputation and international image.The maritime search and rescue work that China Maritime Search & Rescue Center is responsible for, including marine emergency event
Early warning prevention, life salvage, environment relief and salvage of property, important navigable waters remove obstacles and the reception of piracy information with
Processing.
For the rescue of the marine personnel that meet with misfortune, various countries maritime search and rescue center, which generally uses, sends aircraft arrival accident sea area with charge free,
Personnel as much as possible, which are succoured, using aircraft flees from predicament.However, how in a short time the carrying capacity due to aircraft is limited,
Determine the maximum number that arriving airplane can be succoured, be current various countries' maritime search and rescue center need solution technical problem it
One.
In order to overcome above-mentioned deficiency, the present invention has built a kind of computer estimation method, and this method includes providing one kind i.e.
When succour capacity calculation machine assessment system, under the mode of the analysis of image overall brightness and adaptable image procossing, obtain quasi-
The subgraph of true human body to be succoured carries out bodily form analysis, to determine the corresponding human body weight of each subgraph, based on described
Multiple human body subgraphs determine human body total load to be succoured, to determine whether the aircraft can succour the judgement of all personnel that meet with misfortune
Information, the instant rescue capacity calculation machine assessment system can provide accurate rescue ability to arrive at the aircraft in sea area of meeting with misfortune
Judgment mechanism.
Fig. 1 is the structural block diagram according to the instant rescue capacity calculation machine assessment system shown in embodiment of the present invention,
The system comprises:
Flight driving body frame structure 1, is arranged aboard, for executing various flight operations;
Connector 2, setting is on flight driving body frame structure 1, for that will be connected to flight driving body frame structure by camera 3 out of my cabin
1, camera 3 it will be arranged aboard out of my cabin;
Camera 3 out of my cabin, setting aboard, for shooting to scene outside aircraft cabin, are schemed out of my cabin immediately with obtaining
Picture exports the instant image out of my cabin;
Camera in cabin, as shown in Fig. 2, being arranged in aircraft cabin, for being shot the scene in cabin to obtain
Obtain engine room inside image;
Curve pixel analysis equipment is connect with the camera out of my cabin, for receiving the instant image out of my cabin, with described
Immediately the center of the horizontal direction in image is classified as Y-axis out of my cabin, with the central row of the vertical direction in the instant image out of my cabin
For X-axis, Lie groupoid is depicted in image described based on the X-axis and the Y-axis out of my cabin immediately, and will it is described it is instant out of my cabin
Each pixel that Lie groupoid passes through in image obtains the red green of the multiple target pixel points as multiple target pixel points
Signal component value, black and white signal component value and champac signal component value, and following operation is done for each target pixel points: red green signal component value is removed
Target point is obtained divided by the results added of black and white signal component value with the result of black and white signal component value and champac signal component value
Ratio value, after being also used to for the ratio values of the multiple target pixel points being added divided by the quantity of the multiple target pixel points with
Obtain current comparison reference;
Fragment decision device is connect, for receiving respectively with the camera out of my cabin and the curve pixel analysis equipment
The current comparison reference and the instant image out of my cabin, are determined based on the current comparison reference to the instant cabin
The number of tiles that outer image is cut, wherein the current comparison reference is bigger, cuts to the instant image out of my cabin
The number of tiles arrived is fewer;
Fragment processing equipment is connect with the fragment decision device, for receiving the number of tiles, and based on described broken
Sheet data is to the fragment cutting process of image progress out of my cabin immediately, to obtain and export multiple images fragment;
Piece smoothing arrangement is morcelled, connect with the fragment processing equipment, for receiving described multiple images fragment, and is based on
The degree of roughness of each images fragment itself determines the dynamics that image smoothing is executed to described image fragment, and by multiple execution
The images fragment of complete picture smooth treatment is compound to morcel piece smoothed image to obtain;
Body detection device is connect with the piece smoothing arrangement of morcelling, and described morcels piece smoothed image, and base for receiving
It obtains and divides from described morcel in piece smoothed image in default human body upper limit gray threshold and default human body lower limit gray threshold
Multiple human body subgraphs out;
Load Analysis equipment, setting aboard, are connect with the camera out of my cabin and the body detection device respectively,
Bodily form analysis is carried out for receiving multiple human body subgraphs and instant image out of my cabin, and to each human body subgraph, with determination
Each corresponding human body weight of human body subgraph determines human body total load to be succoured based on the multiple human body subgraph;
Weight detection equipment in cabin is arranged in aircraft cabin, connect with camera in the cabin, for receiving the machine
Cabin internal image, and all kinds of targets in the engine room inside image are identified, and the type of the target based on identification and
Quantity determines target total load in cabin;
Load evaluation equipment is arranged in aircraft cabin, examines respectively with weight in the load Analysis equipment and the cabin
Measurement equipment connection, for receiving target total load in the human body total load to be succoured and the cabin, and by aircraft bearing load
Threshold value subtracts in the human body total load to be succoured and the cabin that target total load is to obtain operation result, when the operation result
When more than or equal to preset difference value threshold value, complete rescue signal is issued.
Then, continue to carry out further the specific structure of instant rescue capacity calculation machine assessment system of the invention
It is bright.
In the instant rescue capacity calculation machine assessment system:
In the load evaluation equipment, when the operation result is less than preset difference value threshold value, issued section rescue letter
Number.
In the instant rescue capacity calculation machine assessment system, further includes:
Wireless communication interface is connect with the load Analysis equipment and the load evaluation equipment respectively;
Wherein, the wireless communication interface is used for when receiving the part rescue signal, is schemed described out of my cabin immediately
Picture and the part rescue signal send jointly to the sea rescue platform of distal end.
In the instant rescue capacity calculation machine assessment system:
In the wireless communication interface, including multiple wireless transmission units, it further include signal strength measurement unit and biography
Defeated switch unit;
Wherein, the signal strength measurement unit is connect with the multiple wireless transmission unit respectively;
Wherein, the transmission switch unit is connect with the signal strength measurement unit, also respectively with it is the multiple wireless
Transmission unit connection.
In the instant rescue capacity calculation machine assessment system:
The signal strength measurement unit is used to measure the transmission that signal in the multiple wireless transmission unit sends channel
Intensity;
Wherein, the transmission that signal in the multiple wireless transmission unit is sent channel by the signal strength measurement unit is strong
Strongest wireless transmission unit is spent as object transmission unit.
In the instant rescue capacity calculation machine assessment system:
The transmission switch unit is switched to the object transmission unit to realize the wireless transmission of data.
In the instant rescue capacity calculation machine assessment system:
The red green signal component value of the target pixel points indicates the numberical range from red to green;
And the champac signal component value of the target pixel points is from yellow to the numberical range of blue.
And in the instant rescue capacity calculation machine assessment system:
In the curve pixel analysis equipment, when the current comparison reference is less than or equal to pre-set limit, issue
The exceeded signal of brightness;
And in the curve pixel analysis equipment, when the current comparison reference is greater than pre-set limit, issue
The low mark signal of brightness.
In addition, the multiple wireless transmission unit includes GPRS transmission unit in the wireless communication interface.
GPRS is the abbreviation of general packet radio service technology (General Packet Radio Service), he is
A kind of available mobile data services of gsm mobile telephone user.GPRS can say be GSM continuity.GPRS is with previous continuously in frequency
The mode of road transmission is different, is to be transmitted with package (Packet) formula, therefore the expense that user is born is with its transmission money
Material list position calculates, and not uses its entire channel, theoretically inexpensively.The transmission rate of GPRS can be promoted to 56 even
114Kbps。
GPRS is often described as " 2.5G ", that is to say, that this technology is located at the second generation (2G) and the third generation (3G) is mobile
Between mechanics of communication.He is by providing the data transmitting of middling speed using not used TDMA channel in GSM network.GPRS is broken through
GSM net can only provide the mode of thinking of circuit switching, only by increasing corresponding functional entity and to existing base station system
Part transformation is carried out to realize packet switch, the investment of this transformation is comparatively and little, but obtained user data rate
Considerable.Moreover, connection and transmission all can because no longer needing intermediary's converter required for existing wireless application
It is more convenient to be easy.In this way, user can both connect to the internet, the interactive communications such as video conference are participated in, and in the same video signal net
The user of (VRN) on network, it might even be possible to dial up on the telephone without passing through, and continue and be connected to the network.
For the communication mode of GPRS packet switch in the communication mode of packet switch, data are divided into the packet of certain length
(grouping) has a packets headers before each packet (address mark therein indicates the grouping is sent to where).Data transmission it
Before do not need to allocate channel in advance, establish connection.But when each data packet reaches, according to the information in datagram header
(such as destination address) temporarily finds an available channel resource and sends the datagram.In this transmission mode, number
According to the side's of sending and receiving cochannel between there is no fixed occupancy relationship, channel resource can be regarded as being total to by all users
Enjoy use.Since data service all shows a kind of paroxysmal business characteristic in most cases, to channel width
Changes in demand is larger, therefore will preferably utilize channel resource using packet mode progress data transmission.Such as one into
The user of row WWW browsing, most of the time are in browse state, and really only account for very little ratio for the time of data transmission.
In this case according to the mode of fixed busy channel, it will cause the biggish wasting of resources.
Using instant rescue capacity calculation machine assessment system of the invention, for aircraft rescue worker quantity in the prior art
It is difficult to the technical issues of assessing with ability, by high-precision Image Acquisition and image procossing, acquisition accurately meets with misfortune personnel's
Information on load, and based on target total load and the information on load for the personnel that meet with misfortune in aircraft bearing load threshold value, cabin, accurate judgement
Aircraft can be succoured completely and need to be succoured human body out, to solve above-mentioned technical problem.
It is understood that although the present invention has been disclosed in the preferred embodiments as above, above-described embodiment not to
Limit the present invention.For any person skilled in the art, without departing from the scope of the technical proposal of the invention,
Many possible changes and modifications all are made to technical solution of the present invention using the technology contents of the disclosure above, or are revised as
With the equivalent embodiment of variation.Therefore, anything that does not depart from the technical scheme of the invention are right according to the technical essence of the invention
Any simple modifications, equivalents, and modifications made for any of the above embodiments still fall within the range of technical solution of the present invention protection
It is interior.
Claims (8)
1. a kind of computer estimation method, this method includes providing a kind of rescue capacity calculation machine assessment system immediately, in image
Under the mode of overall brightness analysis and adaptable image procossing, the subgraph for obtaining accurately human body to be succoured carries out the bodily form point
Analysis determines that human body to be succoured always is born based on the multiple human body subgraph to determine the corresponding human body weight of each subgraph
Lotus, to determine whether the aircraft can succour the judgement information of all personnel that meet with misfortune, the instant rescue capacity calculation machine assessment
System includes:
Camera out of my cabin, setting are aboard, defeated to obtain immediately image out of my cabin for shooting to scene outside aircraft cabin
The instant image out of my cabin out;
Camera in cabin is arranged in aircraft cabin, for being shot to the scene in cabin to obtain engine room inside image;
Curve pixel analysis equipment is connect with the camera out of my cabin, for receiving the instant image out of my cabin, with described instant
The center of the horizontal direction in image is classified as Y-axis out of my cabin, with the center behavior X of the vertical direction in the instant image out of my cabin
Axis is depicted Lie groupoid in the instant image out of my cabin based on the X-axis and the Y-axis, and is schemed described out of my cabin immediately
Each pixel that Lie groupoid passes through as in as multiple target pixel points, obtain the multiple target pixel points it is red it is green at
Score value, black and white signal component value and champac signal component value, and do following operation for each target pixel points: by red green signal component value divided by
The result and champac signal component value of black and white signal component value obtain the ratio of target point divided by the results added of black and white signal component value
Example value, divided by the quantity of the multiple target pixel points to obtain after being also used to for the ratio value of the multiple target pixel points being added
Obtain current comparison reference;
Fragment decision device is connect with the camera out of my cabin and the curve pixel analysis equipment respectively, described for receiving
Current comparison reference and the instant image out of my cabin are schemed based on the current comparison reference determination to described out of my cabin immediately
The number of tiles obtained as cutting, wherein the current comparison reference is bigger, cuts to the instant image out of my cabin
Number of tiles is fewer;
Fragment processing equipment is connect with the fragment decision device, for receiving the number of tiles, and is based on the fragment number
Fragment cutting process is carried out according to the instant image out of my cabin, to obtain and export multiple images fragment;
Piece smoothing arrangement is morcelled, is connect with the fragment processing equipment, for receiving described multiple images fragment, and based on each
The degree of roughness of a images fragment itself determines the dynamics that image smoothing is executed to described image fragment, and has executed figure for multiple
Piece smoothed image is morcelled as the images fragment of smoothing processing is compound to obtain;
Body detection device is connect with the piece smoothing arrangement of morcelling, for receive it is described morcel piece smoothed image, and based on pre-
If human body upper limit gray threshold and default human body lower limit gray threshold from it is described morcel obtain and be partitioned into piece smoothed image it is more
A human body subgraph;
Load Analysis equipment, setting aboard, connect with the camera out of my cabin and the body detection device respectively, are used for
Multiple human body subgraphs and instant image out of my cabin are received, and bodily form analysis is carried out to each human body subgraph, it is each with determination
The corresponding human body weight of a human body subgraph determines human body total load to be succoured based on the multiple human body subgraph;
Weight detection equipment in cabin is arranged in aircraft cabin, connect with camera in the cabin, for receiving in the cabin
Portion's image, and all kinds of targets in the engine room inside image are identified, and the type and quantity of the target based on identification
Determine target total load in cabin;
Load evaluation equipment is arranged in aircraft cabin, sets respectively with weight detecting in the load Analysis equipment and the cabin
Standby connection, for receiving target total load in the human body total load to be succoured and the cabin, and by aircraft bearing load threshold value
Target total load is in human body total load to be succoured described in subtracting and the cabin to obtain operation result, when the operation result is greater than
When equal to preset difference value threshold value, complete rescue signal is issued.
2. the method as described in claim 1, it is characterised in that:
In the load evaluation equipment, when the operation result is less than preset difference value threshold value, issued section rescue signal.
3. method according to claim 2, which is characterized in that the system also includes:
Wireless communication interface is connect with the load Analysis equipment and the load evaluation equipment respectively;
Wherein, the wireless communication interface is used for when receiving the part rescue signal, will the instant image out of my cabin with
And the part rescue signal sends jointly to the sea rescue platform of distal end.
4. method as claimed in claim 3, it is characterised in that:
In the wireless communication interface, including multiple wireless transmission units, it further include that signal strength measurement unit and transmission are cut
Change unit;
Wherein, the signal strength measurement unit is connect with the multiple wireless transmission unit respectively;
Wherein, the transmission switch unit is connect with the signal strength measurement unit, also respectively with the multiple wireless transmission
Unit connection.
5. method as claimed in claim 4, it is characterised in that:
The signal strength measurement unit is used to measure the transmission intensity that signal in the multiple wireless transmission unit sends channel;
Wherein, signal in the multiple wireless transmission unit is sent the transmission intensity of channel most by the signal strength measurement unit
Strong wireless transmission unit is as object transmission unit.
6. method as claimed in claim 5, it is characterised in that:
The transmission switch unit is switched to the object transmission unit to realize the wireless transmission of data.
7. method as claimed in claim 6, it is characterised in that:
The red green signal component value of the target pixel points indicates the numberical range from red to green;
And the champac signal component value of the target pixel points is from yellow to the numberical range of blue.
8. method as claimed in claim 1, it is characterised in that:
In the curve pixel analysis equipment, when the current comparison reference is less than or equal to pre-set limit, brightness is issued
Exceeded signal;
And in the curve pixel analysis equipment, when the current comparison reference is greater than pre-set limit, brightness is issued
Low mark signal.
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CN109700464A (en) * | 2018-12-29 | 2019-05-03 | 朱新玲 | Medical number source delivery system |
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