CN106598037A - UAV identity recognition system based on electronic information UAV control - Google Patents
UAV identity recognition system based on electronic information UAV control Download PDFInfo
- Publication number
- CN106598037A CN106598037A CN201611144110.0A CN201611144110A CN106598037A CN 106598037 A CN106598037 A CN 106598037A CN 201611144110 A CN201611144110 A CN 201611144110A CN 106598037 A CN106598037 A CN 106598037A
- Authority
- CN
- China
- Prior art keywords
- remote sensing
- information
- signal
- uav
- satellite
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000003860 storage Methods 0.000 claims abstract description 30
- 230000005540 biological transmission Effects 0.000 claims abstract description 18
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 8
- 238000012545 processing Methods 0.000 claims abstract description 8
- 230000002452 interceptive effect Effects 0.000 claims description 9
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 3
- 238000012546 transfer Methods 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012552 review Methods 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Selective Calling Equipment (AREA)
Abstract
The invention discloses a UAV identity recognition system based on electronic information UAV control in the technical field of electronic information. The UAV identity recognition system comprises: a remote sensing aircraft, a satellite, a terrestrial signal transmitting and receiving base station and a remote sensing manipulator. The remote sensing aircraft comprises a wireless transceiver unit, a signal amplifier, a filter, a central processing unit, an identity information storage unit, a positioning subsystem, a flight control subsystem and an alarm feedback subsystem. The wireless transceiver unit is used for receiving and transmitting signals and communicating with satellite information, wherein radio wave transmission is used as an information transmission and reception mode. The signal amplifier increases the signal receiving capability of the wireless transceiver unit. The UAV identity recognition system based on electronic information UAV control outputs identity information to the terrestrial signal transmitting and receiving base station, can timely control the location information, and can more conveniently track the remote sensing aircraft.
Description
Technical field
The present invention relates to electronic information technical field, specially a kind of to be based on the unmanned fuselage of electronic information unmanned aerial vehicle (UAV) control
Part identifying system.
Background technology
With the development of electronic technology, unmanned plane has significantly prominent in Remote, cruising time and flight quality
Broken, which is very universal to be applied to Aerial photography, demonstration flight, takes precautions against natural calamities and recover and the field such as scientific investigation, even if but nothing
It is man-machine to bring conveniently to us, but existing many unmanned planes cannot realize that third party reviews and recognizes unmanned identity
Ability, it is as unmanned plane being capable of remote control so that some illegal molecules manufacture some illegal things by unmanned plane, outdoor
Unmanned plane be positioned with kinds of schemes, including the positioning based on satellite navigations such as GPS, the track and localization based on certain particular signal source
(as arranged bracelet signal source, the relative position of unmanned machine testing bracelet signal source realizes Relatively orientation, due to reviewing
The identity of unmanned plane so that staff further cannot be investigated in the case where tracing, for this purpose, we have proposed a kind of base
In electronic information unmanned aerial vehicle (UAV) control unmanned plane identification system.
The content of the invention
It is an object of the invention to provide a kind of be based on electronic information unmanned aerial vehicle (UAV) control unmanned plane identification system, with
Propose in solving above-mentioned background technology as unmanned plane being capable of remote control so that some illegal molecules are made by unmanned plane
Some illegal things are made, the identity as unmanned plane cannot be reviewed so that staff cannot enter one in the case where tracing
The problem that step is looked into.
For achieving the above object, the present invention provides following technical scheme:It is a kind of to be based on electronic information unmanned aerial vehicle (UAV) control nothing
Man-machine identification system, including:Remote sensing aircraft, satellite, ground signal transceiver base station and remote sensing control device, the remote sensing fly
Row device, satellite, ground signal transceiver base station and remote sensing control device constitute the hardware of unmanned plane identification system;
Remote sensing aircraft 1:Remote sensing aircraft includes:Wireless transmit/receive units, signal amplifier, wave filter, central processing unit,
Identity information storage unit, positioning subsystem, flight subsystem and warning feedback subsystem, wireless transmit/receive units are used to connect
Receive and sending signal play a part of to exchange with satellite information, information transmit-receive mode is radio wave transmissions, signal amplifier
Increase the reception signal capabilities of wireless transmit/receive units, filter circuit increases the flatness that signal is received, and central processing unit is used as winged
The judgement mastery reaction of row device control system, the identity information and nonce of identity information storage unit storage remote sensing aircraft
According to, the control system that positioning subsystem and flight subsystem are used for during remote sensing aircraft traveling, wireless transmit/receive units
The control signal of reception is contrasted with the information in identity information storage unit, the prestored information in identity information storage unit
Warning feedback subsystem sends reminder alarm afterwards, and information real-time Transmission to ground signal is received and dispatched base by identity information storage unit
Stand;
Satellite 2:Remote sensing flying vehicles control order is transmitted by satellite, and information transmission mode is radio wave transmissions,
Remote sensing aircraft meets the service system of satellite, and satellite plays a part of information transmit-receive transfer in unmanned plane identification system;
Ground signal transceiver base station 3:Ground signal transceiver base station is radar signal reception system, is manipulated with satellite and remote sensing
Device enters row information and mutually passes, and information transmit-receive mode is radio wave transmissions;
Remote sensing control device 4:Remote sensing control device includes signal receiving unit, operating interactive unit, instruction encoding unit, coding
Processor, coding transmitting element and display unit, remote sensing control device pass through operating interactive unit and instruction encoding unit to flight
Device control system carries out coding input, the control command that prestores in input coding identity information storage unit, signal receiving unit
The signal that ground signal transceiver base station sends is received, display unit shows operating interactive unit and prompt command, and coding sends single
First sending method is radio wave transmissions.
Preferably, the frequency range of the radio wave is 1-400000MHz.
Preferably, the positioning subsystem meets GPS services and Big Dipper positioning service.
Preferably, the remote sensing aircraft has a battery module, and the battery module is solar storage battery, and battery mould
Block is electrically connected with flight control system.
Preferably, the identity information storage unit obtains the positional information of remote sensing aircraft by central processing unit and flies
Row state, and the prestored information by the positional information and state of flight of remote sensing aircraft with identity information storage unit makees to compare in real time
Compared with.
Compared with prior art, the invention has the beneficial effects as follows:Should be based on the unmanned fuselage of electronic information unmanned aerial vehicle (UAV) control
Part identifying system, to ground signal transceiver base station, positional information can be controlled in time, for remote sensing aircraft for identity information output
Tracking it is convenient, by for the location positioning of unmanned plane, being conducive to the tracking of unmanned plane.
Description of the drawings
Fig. 1 is present system schematic diagram;
Fig. 2 is remote sensing aerocraft system schematic diagram of the present invention;
Fig. 3 is remote sensing control device systematic schematic diagram of the present invention.
In figure:1 remote sensing aircraft, 2 satellites, 3 ground signal transceiver base stations, 4 remote sensing control devices.
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. 1-3 are referred to, the present invention provides a kind of technical scheme:It is a kind of to be based on electronic information unmanned aerial vehicle (UAV) control unmanned plane
Identification system, including:Remote sensing aircraft 1, satellite 2, ground signal transceiver base station 3 and remote sensing control device 4, the remote sensing fly
Row device 1, satellite 2, ground signal transceiver base station 3 and remote sensing control device 4 constitute the hardware of unmanned plane identification system;
Remote sensing aircraft 1:Remote sensing aircraft 1 includes:Wireless transmit/receive units, signal amplifier, wave filter, central authorities are processed
Device, identity information storage unit, positioning subsystem, flight subsystem and warning feedback subsystem, wireless transmit/receive units are used
In receiving and sending signal play a part of and 2 communication for information of satellite, information transmit-receive mode is radio wave transmissions, and signal is put
Big device increases the reception signal capabilities of wireless transmit/receive units, and filter circuit increases the flatness that signal is received, and central processing unit is made
For the judgement mastery reaction of flight control system, the identity information of identity information storage unit storage remote sensing aircraft 1 and face
When data, the control system that positioning subsystem and flight subsystem are used for during the traveling of remote sensing aircraft 1, wireless receiving and dispatching
The control signal that unit is received is contrasted with the information in identity information storage unit, prestoring in identity information storage unit
After information, warning feedback subsystem sends reminder alarm, and information real-time Transmission to ground signal is received and dispatched by identity information storage unit
Base station 3;
Satellite 2:1 control command of remote sensing aircraft is transmitted by satellite 2, and information transmission mode is passed for radio wave
Defeated, remote sensing aircraft 1 meets the service system of satellite 2, and satellite 2 plays information transmit-receive transfer in unmanned plane identification system
Effect;
Ground signal transceiver base station 3:Ground signal transceiver base station 3 is radar signal reception system, is grasped with satellite 2 and remote sensing
Control device 4 enters row information and mutually passes, and information transmit-receive mode is radio wave transmissions;
Remote sensing control device 4:Remote sensing control device 4 includes signal receiving unit, operating interactive unit, instruction encoding unit, volume
Code processor, coding transmitting element and display unit, remote sensing control device 4 pass through operating interactive unit and instruction encoding unit to flying
Row device control system carries out coding input, the control command that prestores in input coding identity information storage unit, and signal receives single
Unit receives the signal that ground signal transceiver base station 3 sends, and display unit shows operating interactive unit and prompt command, and coding sends
Unit sending method is radio wave transmissions.
Wherein, the frequency range of the radio wave is 1-400000MHz, and the frequency range that the unmanned plane identification system is used is
840.5-845MHz, 1430-1444MHz, 2408-2440MHz, the positioning subsystem meet GPS services and Big Dipper positioning clothes
Business, Big Dipper positioning service are used more accurately for domestic for what China independently researched and developed, and GPS positioning system is interior at the international level to be made
It is most wide with rate, meet both the above positioning service and cause unmanned plane identification system practicality wide, the remote sensing aircraft 1 has
There is battery module, be that flight control system is powered, the battery module is solar storage battery, and energy-conserving and environment-protective, increase are continued a journey
Mileage, and battery module and flight control system electric connection, the identity information storage unit are obtained by central processing unit
The positional information and state of flight of remote sensing aircraft 1 are taken, and the positional information and state of flight of remote sensing aircraft 1 are believed with identity
The prestored information of breath memory element is made comparisons in real time.
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 (5)
1. it is a kind of to be based on electronic information unmanned aerial vehicle (UAV) control unmanned plane identification system, it is characterised in that to include:Remote sensing is flown
Device (1), satellite (2), ground signal transceiver base station (3) and remote sensing control device (4), the remote sensing aircraft (1), satellite (2),
Face signal transmitting and receiving base station (3) and remote sensing control device (4) constitute the hardware of unmanned plane identification system;
Remote sensing aircraft (1):Remote sensing aircraft (1) includes:Wireless transmit/receive units, signal amplifier, wave filter, central authorities are processed
Device, identity information storage unit, positioning subsystem, flight subsystem and warning feedback subsystem, wireless transmit/receive units are used
In receiving and sending signal play a part of and satellite (2) communication for information, information transmit-receive mode is radio wave transmissions, signal
Amplifier increases the reception signal capabilities of wireless transmit/receive units, and filter circuit increases the flatness that signal is received, central processing unit
As the judgement mastery reaction of flight control system, the identity information of identity information storage unit storage remote sensing aircraft (1)
And ephemeral data, the control system that positioning subsystem and flight subsystem are used for during remote sensing aircraft (1) traveling, nothing
The control signal that line Transmit-Receive Unit is received is contrasted with the information in identity information storage unit, in identity information storage unit
Prestored information after warning feedback subsystem send reminder alarm, information real-time Transmission to ground is believed by identity information storage unit
Number transceiver base station (3);
Satellite (2):Remote sensing aircraft (1) control command is transmitted by satellite (2), and information transmission mode is passed for radio wave
Defeated, remote sensing aircraft (1) meets the service system of satellite (2), and satellite (2) plays information transmit-receive in unmanned plane identification system
The effect of transfer;
Ground signal transceiver base station (3):Ground signal transceiver base station (3) is radar signal reception system, with satellite (2) and remote sensing
Control device (4) enters row information and mutually passes, and information transmit-receive mode is radio wave transmissions;
Remote sensing control device (4):Remote sensing control device (4) includes signal receiving unit, operating interactive unit, instruction encoding unit, volume
Code processor, coding transmitting element and display unit, remote sensing control device (4) is by operating interactive unit and instruction encoding unit pair
Flight control system carries out coding input, the control command that prestores in input coding identity information storage unit, and signal is received
Unit receives the signal that ground signal transceiver base station (3) sends, and display unit shows operating interactive unit and prompt command, coding
Transmitting element sending method is radio wave transmissions.
2. according to claim 1 a kind of based on electronic information unmanned aerial vehicle (UAV) control unmanned plane identification system, which is special
Levy and be:The frequency range of the radio wave is 1-400000MHz.
3. according to claim 1 a kind of based on electronic information unmanned aerial vehicle (UAV) control unmanned plane identification system, which is special
Levy and be:The positioning subsystem meets GPS services and Big Dipper positioning service.
4. according to claim 1 a kind of based on electronic information unmanned aerial vehicle (UAV) control unmanned plane identification system, which is special
Levy and be:The remote sensing aircraft (1) with battery module, the battery module be solar storage battery, and battery module with
Flight control system is electrically connected with.
5. according to claim 1 a kind of based on electronic information unmanned aerial vehicle (UAV) control unmanned plane identification system, which is special
Levy and be:The identity information storage unit obtains the positional information and flight shape of remote sensing aircraft (1) by central processing unit
State, and the prestored information by the positional information and state of flight of remote sensing aircraft (1) with identity information storage unit makees to compare in real time
Compared with.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611144110.0A CN106598037A (en) | 2016-12-13 | 2016-12-13 | UAV identity recognition system based on electronic information UAV control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611144110.0A CN106598037A (en) | 2016-12-13 | 2016-12-13 | UAV identity recognition system based on electronic information UAV control |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106598037A true CN106598037A (en) | 2017-04-26 |
Family
ID=58597799
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201611144110.0A Pending CN106598037A (en) | 2016-12-13 | 2016-12-13 | UAV identity recognition system based on electronic information UAV control |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106598037A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107544542A (en) * | 2017-09-29 | 2018-01-05 | 中航天元防务技术(北京)有限公司 | A kind of unmanned vehicle enemy and we's recognition methods based on line-of-sight propagation |
CN108155959A (en) * | 2017-12-15 | 2018-06-12 | 成都爱科特科技发展有限公司 | UAV TT & C's signal detecting method under a kind of complex network environment |
CN108200056A (en) * | 2017-12-29 | 2018-06-22 | 广东工业大学 | A kind of proof of identity method and system of unmanned device |
CN108298044A (en) * | 2018-03-17 | 2018-07-20 | 烟台尼达船艇科技开发有限公司 | A kind of water life-saving robot |
CN114326790A (en) * | 2021-12-06 | 2022-04-12 | 特金智能科技(上海)有限公司 | Unmanned aerial vehicle violation determination method and device, electronic equipment and storage medium |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN203596823U (en) * | 2013-09-24 | 2014-05-14 | 中国航天空气动力技术研究院 | Unmanned plane high-altitude base station communication system |
CN105259916A (en) * | 2015-10-30 | 2016-01-20 | 杨珊珊 | Scheduling apparatus of unmanned aircraft and scheduling method of scheduling apparatus |
CN105608930A (en) * | 2016-02-03 | 2016-05-25 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle management system and method |
CN205327433U (en) * | 2016-02-03 | 2016-06-22 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle maintains management system |
CN105761550A (en) * | 2016-03-01 | 2016-07-13 | 北京航空航天大学 | Unmanned aerial vehicle (UAV) air operation security control method, UAV and server |
CN105827607A (en) * | 2016-03-31 | 2016-08-03 | 赵文洁 | Unmanned aerial vehicle identification system |
CN205656502U (en) * | 2016-05-09 | 2016-10-19 | 王彦成 | System for unmanned aerial vehicle management and control device and corresponding |
CN106060079A (en) * | 2016-07-11 | 2016-10-26 | 顺丰科技有限公司 | Unmanned aerial vehicle authentication system and method |
-
2016
- 2016-12-13 CN CN201611144110.0A patent/CN106598037A/en active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN203596823U (en) * | 2013-09-24 | 2014-05-14 | 中国航天空气动力技术研究院 | Unmanned plane high-altitude base station communication system |
CN105259916A (en) * | 2015-10-30 | 2016-01-20 | 杨珊珊 | Scheduling apparatus of unmanned aircraft and scheduling method of scheduling apparatus |
CN105608930A (en) * | 2016-02-03 | 2016-05-25 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle management system and method |
CN205327433U (en) * | 2016-02-03 | 2016-06-22 | 辽宁猎鹰航空科技有限公司 | Unmanned aerial vehicle maintains management system |
CN105761550A (en) * | 2016-03-01 | 2016-07-13 | 北京航空航天大学 | Unmanned aerial vehicle (UAV) air operation security control method, UAV and server |
CN105827607A (en) * | 2016-03-31 | 2016-08-03 | 赵文洁 | Unmanned aerial vehicle identification system |
CN205656502U (en) * | 2016-05-09 | 2016-10-19 | 王彦成 | System for unmanned aerial vehicle management and control device and corresponding |
CN106060079A (en) * | 2016-07-11 | 2016-10-26 | 顺丰科技有限公司 | Unmanned aerial vehicle authentication system and method |
Non-Patent Citations (1)
Title |
---|
张传超: "《2015中国无人机***峰会论文集》", 30 September 2015, 航空工业出版社 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107544542A (en) * | 2017-09-29 | 2018-01-05 | 中航天元防务技术(北京)有限公司 | A kind of unmanned vehicle enemy and we's recognition methods based on line-of-sight propagation |
CN108155959A (en) * | 2017-12-15 | 2018-06-12 | 成都爱科特科技发展有限公司 | UAV TT & C's signal detecting method under a kind of complex network environment |
CN108200056A (en) * | 2017-12-29 | 2018-06-22 | 广东工业大学 | A kind of proof of identity method and system of unmanned device |
CN108200056B (en) * | 2017-12-29 | 2021-03-16 | 广东工业大学 | Identity verification method and system for unmanned device |
CN108298044A (en) * | 2018-03-17 | 2018-07-20 | 烟台尼达船艇科技开发有限公司 | A kind of water life-saving robot |
CN114326790A (en) * | 2021-12-06 | 2022-04-12 | 特金智能科技(上海)有限公司 | Unmanned aerial vehicle violation determination method and device, electronic equipment and storage medium |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106598037A (en) | UAV identity recognition system based on electronic information UAV control | |
CN204316545U (en) | Based on the Unmanned Aerial Vehicle Data link system of mobile communications network | |
CN109727493A (en) | Based on the unmanned plane monitoring system of integrated answering machine and its response, ADS-B OUT/IN method | |
CN106712833B (en) | Aircraft integrated information processing subsystem and spaceflight TT&C system | |
CN203528817U (en) | Mountain tourism emergency rescue system based on unmanned plane | |
US9595198B2 (en) | Unmanned aerial system position reporting system | |
CN105676249A (en) | Navigation airplane communication navigation monitoring system and method based on 4G/3G/BDS | |
CN206515700U (en) | A kind of UAV Flight Control System based on smart mobile phone | |
CN110060515B (en) | GNSS-based aircraft monitoring system and method | |
CN106301532A (en) | A kind of based on Embedded UAV TT & C's data link system | |
CN110392049A (en) | Airborne unmanned plane identification module and real name identification method | |
CN208818836U (en) | Positioning device and positioning system | |
CN106550287A (en) | The VHF talkback units that integrated AIS is received | |
CN208224759U (en) | A kind of unmanned aerial vehicle observing and controlling tracking system | |
CN106875655A (en) | A kind of unmanned aerial vehicle data communication jamproof system and method | |
CN205396546U (en) | Unmanned vehicles system | |
CN108022442A (en) | A kind of vehicle monitoring system and its application method based on cloud pipe end | |
US20180364706A1 (en) | Autonomous distress tracking device | |
CN108075822A (en) | Mounted on " low slow small " carry-on portable multi-mode supervision equipment | |
CN206323513U (en) | The VHF talkback units that integrated AIS is received | |
CN207766265U (en) | A kind of satellite system being loaded with ADS-B | |
CN106772443A (en) | A kind of anti-navigation signal base station of vehicular and anti-ballistic boat locomotive | |
Niu et al. | Design of data transmission system of human-autonomous devices for UAV inspection of transmission line status | |
CN108803636A (en) | A kind of UAV Flight Control System based on operation system of smart phone | |
CN202798797U (en) | Vehicle-mounted network navigation system based on embedded Linux |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170426 |
|
RJ01 | Rejection of invention patent application after publication |