CN106444828A - Small unmanned aerial vehicle ground station system based on LabView - Google Patents
Small unmanned aerial vehicle ground station system based on LabView Download PDFInfo
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- CN106444828A CN106444828A CN201610822365.1A CN201610822365A CN106444828A CN 106444828 A CN106444828 A CN 106444828A CN 201610822365 A CN201610822365 A CN 201610822365A CN 106444828 A CN106444828 A CN 106444828A
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- 238000004891 communication Methods 0.000 claims abstract description 58
- 238000012544 monitoring process Methods 0.000 claims abstract description 11
- 238000012546 transfer Methods 0.000 claims description 10
- 238000012545 processing Methods 0.000 claims description 9
- 238000013500 data storage Methods 0.000 claims description 7
- 230000002452 interceptive effect Effects 0.000 claims description 7
- 239000004973 liquid crystal related substance Substances 0.000 claims description 4
- 230000000694 effects Effects 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 4
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
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- 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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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Abstract
The invention discloses a small unmanned aerial vehicle ground station system based on LabView. The system comprises an unmanned aerial vehicle control station and a satellite control station; the unmanned aerial vehicle control station comprises a communication control module, a data telemeasuring unit is connected to the input end of the communication control module, and a real-time data displaying unit is connected to the output end of the communication control module; the satellite control station comprises a wireless communication data chain, and ground station control equipment is connected to the wireless communication data chain; a far-end receiver comprises a flight monitoring module, the flight monitoring module is provided with a downlink data channel and an uplink control channel, the downlink data channel achieves data exchanging with the unmanned aerial vehicle control station through an SPI bus interface, a telemeasuring data pack downloaded by an unmanned aerial vehicle is played back through a data chain state displayer and a data statistic module to be used for analyzing the flight path, the flight attitude, the state and the like of the unmanned aerial vehicle, therefore, an information processor of the unmanned aerial vehicle is more precise, and the control effect is better.
Description
Technical field
The present invention relates to earth station system design field, specially a kind of SUAV ground based on LabView
Face station system.
Background technology
Unmanned plane is the not manned aircraft being manipulated with the presetting apparatus provided for oneself by radio robot, to no
Man-machine control aspect, unmanned plane itself carries autopilot or presetting apparatus, can quickly realize very much it is flown
Navigation attitude, the manipulation in course line, the takeoff and landing of unmanned plane can by same conventional airplane the same it is also possible to realize in the way of it is exclusive,
As unmanned plane can be thrown using hand or takes off by the way of sliding race, also can realize landing by way of parachuting, this just greatly saves
Demand to takeoff and landing place.
With photoelectric technology, radiotechnics, nanometer technology, microelectric technique fast development, unmanned plane will be towards little
When type, flexibility, flight are long, the directions such as autonomy-oriented, long-range are controlled to develop, urgent based on the field such as dual-use
Need, it is more rapid that SUAV will develop, but current UAV system boat system, for the jamming performance of signal
Relatively strong, easily out of hand, when earth station's detecting system is operated, it is difficult to detect the particular location of unmanned plane, no
Cruise beneficial to unmanned plane uses, and the data of be passed back accurately can not learn position coordinates simultaneously, is sometimes prone to mistake
Place controls by mistake, leads to the monitoring system of unmanned plane can not use well.
Content of the invention
For problem above, the invention provides a kind of SUAV earth station system based on LabView, it is provided with
Ground station control equipment, as the man-machine interface of UAS, in earth station, the uplink by communication system for the control staff
Road direction unmanned plane issue " order ", control flight route or renewal pre-planning flight course, and unmanned plane is carried various
The state of each subsystem, flying height, air speed and relative position etc. on the data of mission payload acquisition, unmanned plane, unmanned plane
Transmitting and receive and can be controlled by master station or by attached satellite control station, ground satellite station pass through radio or cable and
Control station enters row data communication, with have man-machine between have direct radio link to communicate, control station is generally equipped with communication system,
Also communicated with other external systems, this includes obtaining in atmosphere data, and network interactive information between other system；From upper
Level receives an assignment；Superior or other office report information, can be with the problem in effectively solving background technology.
For achieving the above object, the present invention provides following technical scheme：A kind of SUAV ground based on LabView
Stand system, including unmanned aerial vehicle (UAV) control station and satellite control station, the communication link of described unmanned aerial vehicle (UAV) control station and satellite control station it
Between be connected with remote receiver, described unmanned aerial vehicle (UAV) control station includes communication control module, the input of described communication control module
It is connected with telemetry unit, the output end of communication control module is connected with the real-time display unit of data；Described satellite control station
Including wireless communication data chain, wireless communication data chain is built-in with interactive database, the input of described wireless communication data chain
End is connected with air traffic prewarning unit, and wireless communication data chain is also associated with ground station control equipment；Described remote receiver
Including flight monitoring module, described flight monitoring module is provided with downlink data channel and upload control passage, described descending
Data channel carries out data exchange by spi bus interface and unmanned aerial vehicle (UAV) control station, and upload control passage and satellite control station enter
Row data exchange.
As a kind of preferred technical scheme of the present invention, described communication control module includes embedded Control center, described
Embedded Control center adopt 64 ARM11 family chip, and the output end at embedded Control center respectively with communications parameter
Configuration module is connected with off controller, and the data terminal at described embedded Control center is connected with data collector.
As a kind of preferred technical scheme of the present invention, described telemetry unit is included described in fictitious air instrumentation
The output end of fictitious air instrumentation is connected with driver, and the output end of described driver is connected with data checking module, institute
State the input that data checking module is connected to data storage, the output end of described data storage is set with fictitious air instrument
Standby data terminal is connected.
As a kind of preferred technical scheme of the present invention, the real-time display unit of described data includes serial ports configuration module sum
According to library initialization module, the output end of described serial ports configuration module is connected with data processing module, described data library initialization
The data terminal of module is connected with data processing module, and the output end of database initialization module is connected with data collecting card.
As a kind of preferred technical scheme of the present invention, described air traffic prewarning unit includes threshold value setting module and net
Network configurator, the output end of described network configurator is connected with wireless signal transceiver, the data of described wireless signal transceiver
End is connected with threshold value setting module.
As a kind of preferred technical scheme of the present invention, described ground station control equipment includes data transfer radio station and reception
Antenna, the output end in described data transfer radio station is connected with liquid crystal display, the input in described data transfer radio station and control
Keyboard processed is connected.
As a kind of preferred technical scheme of the present invention, described downlink data channel includes RS232 serial communication equipment, institute
The output end stating RS232 serial communication equipment is connected with signal amplifier；Described upload control passage includes satellite locator, institute
The output end stating satellite locator is connected with modem.
As a kind of preferred technical scheme of the present invention, described embedded Control center is also associated with Data-Link status display
Device data statistical module, the output end of described Data-Link status displays is connected with data cache module, described data statistics
The input of module is connected with data cache module.
Compared with prior art, the invention has the beneficial effects as follows：Should the SUAV earth station based on LabView be
System, is provided with ground station control equipment, and as the man-machine interface of UAS, in earth station, control staff passes through communication system
The up-link of system issues " order " to unmanned plane, the flight course controlling flight route or updating pre-planning, and to unmanned plane
The state of each subsystem, flying height, air speed and relative position on data that the various mission payloads carrying obtain, unmanned plane
Deng, the transmitting of unmanned plane with receive and can be controlled by master station or by attached satellite control station, ground satellite station passes through nothing
Line electricity or cable and control station enter row data communication, with have man-machine between have direct radio link to communicate, control station is usual
Equipped with communication system, also communicated with other external systems, this includes obtaining in atmosphere data, and network between other system
Interactive information；Receive an assignment from higher level；Superior or other office report information, whole unmanned plane device has small volume, weight
Amount is light, low cost, mobility are good, flight time length, be easy to hidden, without airfield runway the advantages of.
Brief description
Fig. 1 is present configuration schematic diagram；
Fig. 2 is electrical block diagram of the present invention.
In figure：1- unmanned aerial vehicle (UAV) control station；2- satellite control station；3- remote receiver；4- communication control module；5- remote measurement number
According to unit；The real-time display unit of 6- data；7- wireless communication data chain；8- air traffic prewarning unit；9- ground station control sets
Standby；10- flight monitoring module；11- downlink data channel；12- upload control passage；13- embedded Control center；14- data
Transceiver；15- communications parameter configuration module；16- fictitious air instrumentation；17- data storage；18- driver；19- number
According to checking module；20- serial ports configuration module；21- database initialization module；22- data processing module；23- data collecting card；
24- interactive database；25- threshold value setting module；26- network configurator；27- wireless signal transceiver；28-SPI bus connects
Mouthful；29- data transfer radio station；30- reception antenna；31- liquid crystal display；32- control keyboard；33- on off controller；34-
RS232 serial communication equipment；35- signal amplifier；36- satellite locator；37- modem；38- Data-Link status display
Device；39- data statistics module；40- data cache module.
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 description is it is clear that described embodiment is only a part of embodiment of the present invention, rather than whole embodiments.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 not making creative work
Embodiment, broadly falls into the scope of protection of the invention.
Embodiment：
Refer to Fig. 1 and Fig. 2, the present invention provides a kind of technical scheme：A kind of SUAV ground based on LabView
Stand system, including unmanned aerial vehicle (UAV) control station 1 and satellite control station 2, the communication chain of described unmanned aerial vehicle (UAV) control station 1 and satellite control station 2
It is connected with remote receiver 3, described unmanned aerial vehicle (UAV) control station 1 includes communication control module 4, described communication control module 4 between road
Including embedded Control center 13, described embedded Control center 13 is also associated with Data-Link status displays 38 sum according to statistics
Module 39, the output end of described Data-Link status displays 38 is connected with data cache module 40, described data statistics module 39
Input be connected with data cache module 40, described embedded Control center 13 adopt 64 ARM11 family chip, and
The output end at embedded Control center 13 is connected with communications parameter configuration module 15 and on off controller 33 respectively, described embedded
The data terminal of formula control centre 13 is connected with data collector 14, and the input of described communication control module 4 is connected with remote measurement number
According to unit 5, described telemetry unit 5 includes the output end of fictitious air instrumentation 16 described in fictitious air instrumentation 16
It is connected with driver 18, the output end of described driver 18 is connected with data checking module 19, and described data checking module 19 is even
It is connected to the input of data storage 17, the output end of described data storage 17 and the data terminal of fictitious air instrumentation 16
It is connected, the output end of communication control module 4 is connected with the real-time display unit of data 6, the real-time display unit 6 of described data includes
Serial ports configuration module 20 database initialization module 21, the output end of described serial ports configuration module 20 and data processing module 22
It is connected, the data terminal of described database initialization module 21 is connected with data processing module 22, database initialization module
21 output end is connected with data collecting card 23；Described satellite control station 2 includes wireless communication data chain 7, wireless communication data
It is built-in with interactive database 24 according to chain 7, the input of described wireless communication data chain 7 is connected with air traffic prewarning unit 8,
Described air traffic prewarning unit 8 includes threshold value setting module 25 and network configurator 26, the output of described network configurator 26
End is connected with wireless signal transceiver 27, and the data terminal of described wireless signal transceiver 27 is connected with threshold value setting module 25,
Wireless communication data chain 7 is also associated with ground station control equipment 9, and described ground station control equipment 9 includes data transfer radio station 29
With reception antenna 30, the output end in described data transfer radio station 29 is connected with liquid crystal display 31, described data transfer radio station
29 input is connected with control keyboard 32；Described remote receiver 3 includes flight monitoring module 10, described flight monitoring mould
Downlink data channel 11 and upload control passage 12 are provided with block 10, downlink data channel 11 includes RS232 serial communication and sets
Standby 34, the output end of described RS232 serial communication equipment 34 is connected with signal amplifier 35；Described upload control passage 12 includes
Satellite locator 36, the output end of described satellite locator 36 is connected with modem 37, and described downlink data channel 11 leads to
Cross spi bus interface 28 and carry out data exchange with unmanned aerial vehicle (UAV) control station 1, upload control passage 12 and satellite control station 2 enter line number
According to exchange.
(1) described unmanned aerial vehicle (UAV) control station 1 is connected with unmanned plane automatic flight control system, realize artificial real time remote control or
Select and activate the mission program of airborne storage, control unmanned plane along given radius, joined along land grid with certain speed
Examination point is flown, and point-of-interest is carried out investigations.The reference point of interpenetration network in mission planning, and consider point of observation surrounding terrain
And accordingly the moment sun, with respect to the position of this point, to observe from favourable direction, obtains optimal image effect.
(2) described communications parameter configuration module 15 mainly completes the identification to airborne task device type, to corresponding task
Equipment is adjusted and controls, the display including task device state data (image or other categorical data) and storage, institute
State ground (encoder, the emitter, receiver etc.) part of communication link and corresponding operational control unit, the such as liter of antenna
Fall, the manual or automatic control of antenna, frequency error factor etc. in the case of necessity, also include monitor part, main communication state displaying,
Communication link is realized communicating between control station and unmanned plane.
(3) the real-time display unit 6 of described data is used for monitoring position and the flight track of unmanned plane, and necessary data
Calculate；The mission planning to be completed of described embedded Control center 13 and necessary task computation, storage retains previous task and flies
Row flight path, to reappear if necessary in the future, lists selectable unmanned plane during flying program；Described fictitious air instrumentation 16 can
To obtain weather turntable data, receive an assignment requirement, sends the data obtaining from oneself unmanned plane to other users.
(4) described remote receiver 3 is by, while to the selection of messaging parameter, realizing the switch control rule to serial ports,
The telemetry data packet simultaneously unmanned plane being passed to data radio station enters row cache；Described data processing module 22 passes through serial port protocol pair
The telemetry data packet that unmanned plane passes down is parsed, and is then passed to data disaply moudle data memory module；Described data shows
Show module data processing module can be parsed after data shown in real time and played back；Described data memory module 17 is used for
The storage telemetry data packet that passes down of unmanned plane, include the navigation attitude of unmanned plane, highly, course, speed etc., also storage unmanned plane simultaneously
Way point information in flight course for the son；Described Data-Link status displays 38 data statistical module 39 is mainly to unmanned plane
The telemetry data packet passing down is played back, for being analyzed to the flight path of unmanned plane, flight attitude, state etc..
The operation principle of the present invention：It is somebody's turn to do the SUAV earth station system based on LabView, be provided with ground station control
Equipment, as the man-machine interface of UAS, in earth station, control staff passes through the up-link of communication system to unmanned plane
Issue " order ", the flight course controlling flight route or updating pre-planning, and the various mission payloads that unmanned plane is carried obtain
Data, the state of each subsystem, flying height, air speed and relative position etc., the transmitting of unmanned plane and reception on unmanned plane
Can be controlled by master station or by attached satellite control station, ground satellite station is carried out with control station by radio or cable
Data communication, with have man-machine between have direct radio link to communicate, control station is generally equipped with communication system, also with other outside
Portion's system is communicated, and this includes obtaining in atmosphere data, and network interactive information between other system；Accept to appoint from higher level
Business；Superior or other office report information, whole unmanned plane device have small volume, lightweight, low cost, mobility are good,
Flight time length, be easy to hidden, without airfield runway the advantages of.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention
Any modification, equivalent and improvement made within god and principle etc., should be included within the scope of the present invention.
Claims (8)
1. a kind of SUAV earth station system based on LabView, including unmanned aerial vehicle (UAV) control station (1) and satellite control station
(2), it is connected with remote receiver (3) between described unmanned aerial vehicle (UAV) control station (1) and the communication link of satellite control station (2), it is special
Levy and be：Described unmanned aerial vehicle (UAV) control station (1) includes communication control module (4), and the input of described communication control module (4) connects
There is telemetry unit (5), the output end of communication control module (4) is connected with the real-time display unit of data (6)；Described satellite control
System station (2) includes wireless communication data chain (7), and wireless communication data chain (7) is built-in with interactive database (24), described wireless
The input of communication data chain (7) is connected with air traffic prewarning unit (8), and wireless communication data chain (7) is also associated with ground
Stand control equipment (9)；Described remote receiver (3) includes flight monitoring module (10), and described flight monitoring module (10) is upper to pacify
Equipped with downlink data channel (11) and upload control passage (12), described downlink data channel (11) passes through spi bus interface
(28) carry out data exchange with unmanned aerial vehicle (UAV) control station (1), upload control passage (12) and satellite control station (2) carry out data friendship
Change.
2. a kind of SUAV earth station system based on LabView according to claim 1 it is characterised in that：Institute
State communication control module (4) and include embedded Control center (13), described embedded Control center (13) adopts 64 ARM11's
Family chip, and the output end of embedded Control center (13) respectively with communications parameter configuration module (15) and on off controller
(33) it is connected, the data terminal of described embedded Control center (13) is connected with data collector (14).
3. a kind of SUAV earth station system based on LabView according to claim 1 it is characterised in that：Institute
State the output end connection that telemetry unit (5) includes the described fictitious air instrumentation (16) of fictitious air instrumentation (16)
There is driver (18), the output end of described driver (18) is connected with data checking module (19), described data checking module
(19) it is connected to the input of data storage (17), the output end of described data storage (17) and fictitious air instrumentation
(16) data terminal is connected.
4. a kind of SUAV earth station system based on LabView according to claim 1 it is characterised in that：Institute
State the real-time display unit of data (6) and include serial ports configuration module (20) database initialization module (21), described serial ports configuration
The output end of module (20) is connected with data processing module (22), the data terminal of described database initialization module (21) and number
It is connected according to processing module (22), the output end of database initialization module (21) is connected with data collecting card (23).
5. a kind of SUAV earth station system based on LabView according to claim 1 it is characterised in that：Institute
State air traffic prewarning unit (8) and include threshold value setting module (25) and network configurator (26), described network configurator (26)
Output end be connected with wireless signal transceiver (27), the data terminal of described wireless signal transceiver (27) and threshold value setting module
(25) it is connected.
6. a kind of SUAV earth station system based on LabView according to claim 1 it is characterised in that：Institute
State ground station control equipment (9) and include data transfer radio station (29) and reception antenna (30), described data transfer radio station (29)
Output end is connected with liquid crystal display (31), and the input of described data transfer radio station (29) is connected with control keyboard (32)
Connect.
7. a kind of SUAV earth station system based on LabView according to claim 1 it is characterised in that：Institute
State downlink data channel (11) and include RS232 serial communication equipment (34), the output end of described RS232 serial communication equipment (34)
It is connected with signal amplifier (35)；Described upload control passage (12) includes satellite locator (36), described satellite locator
(36) output end is connected with modem (37).
8. a kind of SUAV earth station system based on LabView according to claim 1 it is characterised in that：Institute
State embedded Control center (13) and be also associated with Data-Link status displays (38) data statistical module (39), described Data-Link
The output end of status displays (38) is connected with data cache module (40), the input of described data statistics module (39) and number
It is connected according to cache module (40).
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| CN201610822365.1A CN106444828A (en) | 2016-09-14 | 2016-09-14 | Small unmanned aerial vehicle ground station system based on LabView |
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| CN201610822365.1A CN106444828A (en) | 2016-09-14 | 2016-09-14 | Small unmanned aerial vehicle ground station system based on LabView |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108646784A (en) * | 2018-06-21 | 2018-10-12 | 河南天腾航空科技有限公司 | A kind of unmanned plane night Regional Atmospheric Environment monitoring method |
| CN109841092A (en) * | 2019-01-28 | 2019-06-04 | 西安爱生技术集团公司 | A kind of unmanned aerial vehicle command and control system |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102033546A (en) * | 2010-11-09 | 2011-04-27 | 上海交通大学 | Low-altitude airship flight control system and flight control method thereof |
| CN102353377A (en) * | 2011-07-12 | 2012-02-15 | 北京航空航天大学 | High altitude long endurance unmanned aerial vehicle integrated navigation system and navigating and positioning method thereof |
| CN104049625A (en) * | 2014-07-09 | 2014-09-17 | 华南农业大学 | Internet-of-things irrigation facility regulating and controlling platform and method based on unmanned aerial vehicle |
| US20150338855A1 (en) * | 2013-02-15 | 2015-11-26 | Disney Enterprises, Inc. | Controlling unmanned aerial vehicles as a flock to synchronize flight in aerial displays |
| CN205017328U (en) * | 2015-08-27 | 2016-02-03 | 杨珊珊 | Intelligence relay system and unmanned aerial vehicle thereof |
| CN205121341U (en) * | 2015-10-27 | 2016-03-30 | 四川豪斯特电子技术有限责任公司 | Unmanned aerial vehicle ground command system |
| CN105824318A (en) * | 2016-02-19 | 2016-08-03 | 深圳供电局有限公司 | Many rotor unmanned aerial vehicle communication and safety monitoring system |
-
2016
- 2016-09-14 CN CN201610822365.1A patent/CN106444828A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102033546A (en) * | 2010-11-09 | 2011-04-27 | 上海交通大学 | Low-altitude airship flight control system and flight control method thereof |
| CN102353377A (en) * | 2011-07-12 | 2012-02-15 | 北京航空航天大学 | High altitude long endurance unmanned aerial vehicle integrated navigation system and navigating and positioning method thereof |
| US20150338855A1 (en) * | 2013-02-15 | 2015-11-26 | Disney Enterprises, Inc. | Controlling unmanned aerial vehicles as a flock to synchronize flight in aerial displays |
| CN104049625A (en) * | 2014-07-09 | 2014-09-17 | 华南农业大学 | Internet-of-things irrigation facility regulating and controlling platform and method based on unmanned aerial vehicle |
| CN205017328U (en) * | 2015-08-27 | 2016-02-03 | 杨珊珊 | Intelligence relay system and unmanned aerial vehicle thereof |
| CN205121341U (en) * | 2015-10-27 | 2016-03-30 | 四川豪斯特电子技术有限责任公司 | Unmanned aerial vehicle ground command system |
| CN105824318A (en) * | 2016-02-19 | 2016-08-03 | 深圳供电局有限公司 | Many rotor unmanned aerial vehicle communication and safety monitoring system |
Non-Patent Citations (1)
| Title |
|---|
| 张浩然: "基于LabVIEW的小型无人机地面站系统研究与设计", 《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108646784A (en) * | 2018-06-21 | 2018-10-12 | 河南天腾航空科技有限公司 | A kind of unmanned plane night Regional Atmospheric Environment monitoring method |
| CN109841092A (en) * | 2019-01-28 | 2019-06-04 | 西安爱生技术集团公司 | A kind of unmanned aerial vehicle command and control system |
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Application publication date: 20170222 |