CN106814748A - Unmanned aerial vehicle group intelligent scheduling monitoring method - Google Patents
Unmanned aerial vehicle group intelligent scheduling monitoring method Download PDFInfo
- Publication number
- CN106814748A CN106814748A CN201611268763.XA CN201611268763A CN106814748A CN 106814748 A CN106814748 A CN 106814748A CN 201611268763 A CN201611268763 A CN 201611268763A CN 106814748 A CN106814748 A CN 106814748A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- monitored
- platform
- unmanned
- electromagnet
- 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.)
- Granted
Links
- 238000012544 monitoring process Methods 0.000 title claims abstract description 41
- 238000000034 method Methods 0.000 title claims abstract description 17
- 238000004891 communication Methods 0.000 claims abstract description 49
- 230000005540 biological transmission Effects 0.000 claims abstract description 16
- 230000005611 electricity Effects 0.000 claims description 10
- 239000004020 conductor Substances 0.000 claims description 8
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052744 lithium Inorganic materials 0.000 claims description 4
- 230000000994 depressogenic effect Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 2
- 238000012546 transfer Methods 0.000 claims description 2
- 238000010030 laminating Methods 0.000 claims 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 238000011161 development Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 230000001360 synchronised effect Effects 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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
- G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying
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)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Traffic Control Systems (AREA)
Abstract
The invention discloses a kind of unmanned aerial vehicle group intelligent scheduling monitoring method, n communication platform is arranged at intervals with the edge or inside of area to be monitored, and is divided into p monitoring section to area to be monitored；The communication platform is provided with the wireless telecommunications system that image information transmission can be carried out with unmanned plane, and the equipment that wired or wireless transmission can be carried out with director server；To m unmanned plane coordinated by the time point and flight path of area to be monitored, it is ensured that each unmanned plane of same time not pass through identical area to be monitored.The present invention solves great amount of images information and transmits problem in real time, so as to meet the purpose for implementing monitoring.Solve the problems, such as unmanned plane must frequent charge could keep regular flight condition.Solve many sorties difference moment each unmanned plane cannot effective scheduling problem, realize reasonable distribution flight range and flight time, it is to avoid repeat monitoring and leak side problem.
Description
Technical field
The invention belongs to monitoring management technical field of taking photo by plane, and in particular to a kind of unmanned aerial vehicle group intelligent scheduling monitoring method.
Background technology
With the development of unmanned air vehicle technique, its application surface is more and more wider, is embodied not in civil area and military domain
The importance that can or lack, the application of especially aeroplane photography and monitoring is more and more extensive, using unmanned plane as aeroplane photography instrument
The main flow of current development is turned into.The monitoring application scenarios such as unmanned plane can be applied to take photo by plane, the prospecting of forest protection, the condition of a disaster.Mesh
Before, it is adapted to civilian unmanned plane and is substantially many spiral Vertical Lift unmanned planes, equipped with lithium battery, d GPS locating module and flight
Drive module, and capture apparatus and storage device.User using unmanned plane take photo by plane etc. apply when, generally by nobody
Machine shoots to current environment scene, and the ambient image that will be photographed is stored in storage card, after shooting is finished, from storage
The ambient image taken by unmanned plane is taken out in card, although this mode can photograph required ambient image, is used
Family needs that after the whole shooting of unmanned plane is finished required ambient image could be obtained from storage card, it is impossible to recognize nothing in time
Man-machine captured content, it is impossible to unmanned plane is monitored and is operated in real time.Due to all kinds of natural calamities and accident frequently
Hair, if state of affairs progress can not be understood in time, can seriously limit to the rescue assessment of disaster and to the control process of accident, from
And cause even more serious casualties and economic loss.
On the other hand, to image the amount of image information to be formed very huge for unmanned plane, is considering equipment cost and equipment self-weight
In the case of, existing unmanned plane can not realize long-distance transmissions, be mounted with that the unmanned plane of wireless telecommunications also can only be strong in signal
Data are transmitted by modes such as wife or bluetooths in region.Cause communication delay Receiver Problem, it is impossible to realize interactive, it is impossible to reach
The purpose of real-time monitoring.
Again, the existing monitoring that small range region can only be directed to by way of unmanned plane carries out no worker monitor, when facing
During monitoring with overlength distance on a large scale, it is impossible to be automatically obtained region and the time coordination of many sorties.And blind area cannot be avoided
Occur with the situation for repeating monitoring.However, being used to realizing that scope is wide and the monitoring mode without dead angle in the prior art, it is more common in and carries
The mileage performance of many spiral Vertical Lift unmanned planes high, increasing the sortie that takes off carries out frequently monitoring and monitoring simultaneously.In fact, no matter
How spiral Vertical Lift unmanned plane during flying mileage increases, and has scope to limit, and must finally make a return voyage charging in time.Especially face
When failure problems must force-land or make a return voyage, monitoring effect is greatly affected.Therefore in the urgent need to a kind of scope is wide, without dead angle,
Mobility strong, synchronizing information tracking system real-time dynamic high.
The content of the invention
The problem and shortage that the present invention exists for the management of existing unmanned plane, it is proposed that a kind of scope is wide, without dead angle, motor-driven
Property strong, synchronizing information unmanned plane panorama real-time dynamic monitoring method high.
Adopt the following technical scheme that to achieve the above object：A kind of unmanned aerial vehicle group intelligent scheduling monitoring method, monitored
The edge or inside in region are arranged at intervals with n communication platform, or are divided into p monitoring section to area to be monitored；The communication
Platform is provided with the wireless telecommunications system that image information transmission can be carried out with unmanned plane, and can with director server carry out it is wired or
The equipment being wirelessly transferred；The communication platform is provided with unmanned plane landing platform, and unmanned plane charging device；The unmanned plane
Including lithium battery, d GPS locating module, flight drive module, capture apparatus and wireless communication module；Each communication platform is at least matched somebody with somebody
Have a unmanned plane；When wireless monitor task is carried out, while start m unmanned plane being monitored, 1≤m≤n, to m nothing
It is man-machine to be coordinated by the time point and flight path of area to be monitored, it is ensured that not pass through phase in each unmanned plane of same time
Same area to be monitored, and each unmanned plane covers all areas to be monitored at the appointed time；Each unmanned plane and closest communication
When the coverage of platform meets the requirement of image information transmission range, the image information of new storage is transmitted to immediate communication
Platform, is transmitted to director server image information by wired or wireless network by the communication platform, by director server to flying
The unmanned plane of state is monitored and analyzed, or sends broadcast；Each unmanned plane electricity as little as safe flight electricity scope when, just
Closely select suitable communication platform to be charged, and by the communication platform send sufficient electricity unmanned plane replace charging unmanned plane after
Continuous monitoring.
Wired charging device, is provided with two grooves, groove in the middle part of unmanned plane landing platform and matches respectively
Non-conductive socket is installed, two non-conductive sockets are connected by wire with charger and power supply；At the middle part of unmanned plane landing platform
Two parallel electroconductive elastic sheets are additionally provided with, the front end or middle part of two parallel electroconductive elastic sheets are provided with conductive contact, when two
After individual electroconductive elastic sheet is depressed, two conductive contacts can be inserted in corresponding non-conductive socket respectively；In the front of unmanned plane landing platform
Edge is fixed with flexible baffle, and the both sides of unmanned plane landing platform are provided with the flexible baffle of divergent shape, and both sides flexible baffle is most
Narrow section is more than or equal to unmanned plane both sides width；Electromagnet is respectively arranged with each flexible baffle, before unmanned plane body
Side and both sides are respectively arranged with magnetic conductor, and each magnetic conductor is corresponding with corresponding electromagnet position；The front side bottom of unmanned plane sets respectively
Two conductive contact blades are equipped with, the width of two conductive contact blades is consistent with the two electroconductive elastic sheets width；The electromagnet and controller
Output end is connected, and the signal output part of wireless telecommunications system is connected with controller signals input；When unmanned plane sends landing letter
Number and near unmanned plane landing platform when, by controller control electromagnet be powered, unmanned plane is positioned, make unmanned plane
Two conductive contact blades are fitted charging with two electroconductive elastic sheets of unmanned plane landing platform, stop charging after charging terminates, it is necessary to nobody
Machine is performed when taking off task, controls electromagnet to power off by controller, is started unmanned plane and is taken off.The unmanned plane landing platform
Front-end and back-end are respectively arranged with front end signal transmitter A and back end signal transmitter B, and the body front end of the unmanned plane is with after
End is respectively arranged with front end signal receiver A ' and back end signal receiver B '.
The wireless charging device, inner chamber is internally provided with unmanned plane landing platform, and charging hair is provided with inner chamber
Ray circle, the charging transmitting coil is electrically connected by relay normally open Duan Yu cities；On the parallel bar support of unmanned motor spindle
Base is installed with, chassis interior is provided with charging receiving coil, the output end of charging receiving coil is sequentially connected rectification circuit
It is connected with the battery charger in unmanned plane with after mu balanced circuit；Meanwhile, it is provided with the inner chamber of unmanned plane landing platform
Electromagnetism iron ring, and the chassis interior is provided with magnet arrangement；The electromagnetism iron ring is connected with controller output end, channel radio
The signal output part of news equipment is connected with controller signals input, and coil control end and the controller output end of relay connect
Connect.When the unmanned plane region nearby maked a return voyage, by the position of unmanned plane gps coordinate judging distance platform in itself,
When the position at place is in the range of setting, platform can be powered by magnetic induction loop, and unmanned plane is drawn down, unmanned plane bottom
Base on portion's parallel bar support can be adsorbed in the optional position of platform surface, charged by charge coil, after charging complete
Stop power supply, gravitation disappears therewith.Base on the parallel bar support of unmanned motor spindle is provided with draw-in groove, and draw-in groove top sets
Fastener is equipped with, one end of fastener is hinged on draw-in groove side wall, and the other end of fastener is connected to draw-in groove opposite side wall by locking member.
Beneficial effect：The present invention solves topmost three problems of monitoring unmanned：One is to solve great amount of images letter
Breath transmits problem in real time, so as to meet the purpose for implementing monitoring.Two be solve unmanned plane must frequent charge could keep just
The problem of normal state of flight.Three be solve many sorties difference moment each unmanned plane cannot effective scheduling problem, it is reasonable to realize
Distribution flight range and the flight time, it is to avoid repeat to monitor and leakage side problem.
The present invention has image information real-time Transmission function, and each unmanned plane meets with the coverage closest to communication platform
During the requirement of image information transmission range, the image information of new storage is transmitted to immediate communication platform.So as to each unmanned plane
Great amount of images information can be transferred to by nearest communication platform with most fast speed, and in time be passed information by the communication platform
Pass director server.Need not be maked a return voyage without landing can just carry out image information transmission.
The present invention is adapted to the function of monitoring on a large scale, and each communication platform United Dispatching cooperates, and unmanned plane constantly rises and falls
In each dispatching platform, constantly change and the unmanned function of continuation of the journey realizes uninterrupted monitoring task, realize remote continuous monitoring
Feature.
The present invention can be to each unmanned plane electric energy supplement, and alternately flight is so as to realize continuous monitoring.Realize that electric energy is mended in time
Fill.
Brief description of the drawings
Fig. 1 is one of communication platform course line of the invention path schematic diagram；
Fig. 2 is the two of communication platform course line of the invention path schematic diagram.
Specific embodiment
Embodiment 1：A kind of unmanned aerial vehicle group intelligent scheduling monitoring method, referring to Fig. 1, multiple is provided with the edge of area to be monitored
Communication platform, generally being equidistantly uniformly arranged.Communication platform is provided with can carry out the wireless of image information transmission with unmanned plane
Communication apparatus, is constantly recorded and storage mass data due to unmanned plane by high-definition camera, not easily passs through wireless network transmissions
（Not only signal stabilization is poor for wireless network transmissions, and needs flow very big, and cost is very high）.When unmanned plane is flat near certain communication
During platform, the image information that can be set up in LAN by wife and unmanned plane is transmitted, it is ensured that rapidly and efficiently transmit data.Unmanned plane
Using many spiral unmanned planes, flying speed can be controlled and can be detained in the air, unmanned plane is in the coverage by communication platform
Scope, it is appropriate reduce flying speed wait after the completion of data transfer again quickly through.Distance is suitable between adjacent communication platform
Words, unmanned plane is capable of achieving real-time Transmission, the Monitoring Data of carrying is synchronized into nearest communication platform substantially.
The equipment that communication platform can carry out wired or wireless transmission with director server, communication platform can contain more perfect
Short distance between transceiver, and communication platform communicates with one another function, wirelessly can pass mass data
It is defeated by server.
Communication platform is provided with unmanned plane landing platform, and unmanned plane charging device.Unmanned plane includes lithium battery, GPS
Locating module, flight drive module, capture apparatus and wireless communication module.Each communication platform at least equipped with one nobody
Machine.
When wireless monitor task is carried out, while start multiple unmanned planes being monitored, quilt is passed through to multiple unmanned planes
The time point of monitored area and flight path are coordinated.
When each unmanned plane meets the requirement of image information transmission range with the coverage closest to communication platform, will newly store
Image information transmit to immediate communication platform, image information is transmitted by wired or wireless network by the communication platform
To director server, by director server to being monitored and analyzed in the unmanned plane for flying state, or broadcast is sent.
Each unmanned plane electricity as little as safe flight electricity scope when, select suitable communication platform to be charged nearby, and
The unmanned plane of sufficient electricity is sent to replace charging unmanned plane to continue to monitor by the communication platform.
The present embodiment can use wired charging device, and two grooves are provided with the middle part of unmanned plane landing platform, recessed
Matching installation has non-conductive socket respectively in groove, and two non-conductive sockets are connected by wire with charger and power supply；Risen in unmanned plane
Two parallel electroconductive elastic sheets are additionally provided with the middle part of drop platform, the front end or middle part of two parallel electroconductive elastic sheets are provided with leads
Electrical contact, after two electroconductive elastic sheets are depressed, two conductive contacts can be inserted in corresponding non-conductive socket respectively；In unmanned plane landing
The leading edge of platform is fixed with flexible baffle, and the both sides of unmanned plane landing platform are provided with the flexible baffle of divergent shape, and both sides are soft
Property most narrow section of baffle plate be more than or equal to unmanned plane both sides width；Electromagnet is respectively arranged with each flexible baffle, nobody
The front side and both sides of machine body are respectively arranged with magnetic conductor, and each magnetic conductor is corresponding with corresponding electromagnet position；The front side of unmanned plane
Bottom is respectively arranged with two conductive contact blades, and the width of two conductive contact blades is consistent with the two electroconductive elastic sheets width；The electromagnetism
Iron is connected with controller output end, and the signal output part of wireless telecommunications system is connected with controller signals input；Work as unmanned plane
When sending falling signal and being close to unmanned plane landing platform, control electromagnet to be powered by controller, unmanned plane positioned,
Two conductive contact blades and two electroconductive elastic sheets of unmanned plane landing platform for making unmanned plane are fitted charging, stop filling after charging terminates
Electricity during task, controls electromagnet to power off, it is necessary to unmanned plane execution is taken off by controller, starts unmanned plane and takes off.It is described nobody
The front-end and back-end of machine landing platform are respectively arranged with front end signal transmitter A and back end signal transmitter B, the unmanned plane
Body front-end and back-end are respectively arranged with front end signal receiver A ' and back end signal receiver B '.
The present embodiment can also wireless charging device, be internally provided with inner chamber in unmanned plane landing platform, in inner chamber pacify
Equipped with charging transmitting coil, the charging transmitting coil is electrically connected by relay normally open Duan Yu cities；In the flat of unmanned motor spindle
Base is installed with row bar support, chassis interior is provided with charging receiving coil, the output end of charging receiving coil connects successively
It is connected with the battery charger in unmanned plane after connecing rectification circuit and mu balanced circuit；Meanwhile, in unmanned plane landing platform
Electromagnetism iron ring is provided with chamber, and the chassis interior is provided with magnet arrangement；The electromagnetism iron ring and controller output end
Connection, the signal output part of wireless telecommunications system is connected with controller signals input, coil control end and the control of relay
Device output end is connected.It is flat by unmanned plane gps coordinate judging distance in itself when the unmanned plane region nearby maked a return voyage
The position of platform, when the position at place is in the range of setting, platform can be powered by magnetic induction loop, under unmanned plane is attracted
Come, the base on unmanned motor spindle parallel bar support can be adsorbed in the optional position of platform surface, charged by charge coil,
Stopped power supply after charging complete, gravitation disappears therewith.Base on the parallel bar support of unmanned motor spindle is provided with draw-in groove,
Draw-in groove top is provided with fastener, and one end of fastener is hinged on draw-in groove side wall, and the other end of fastener is connected to card by locking member
Groove opposite side wall.
Embodiment 2：Another unmanned aerial vehicle group intelligent scheduling monitoring method, referring to Fig. 2, at the edge or interior of area to be monitored
Portion is arranged at intervals with multiple communication platforms, and is divided into multiple monitoring sections to area to be monitored.When wireless monitor task is carried out, together
Shi Qidong multiple unmanned planes be monitored, to multiple unmanned planes assisted by the time point and flight path of area to be monitored
Adjust, it is ensured that in each unmanned plane of same time not by identical area to be monitored, and each unmanned plane covering institute at the appointed time
There is area to be monitored.
Claims (7)
1. a kind of unmanned aerial vehicle group intelligent scheduling monitoring method, it is characterized in that：At the edge or internal interval setting of area to be monitored
There is n communication platform, or be divided into p monitoring section to area to be monitored；The communication platform is provided with can be carried out with unmanned plane
The wireless telecommunications system of image information transmission, and the equipment that wired or wireless transmission can be carried out with director server；The communication
Platform is provided with unmanned plane landing platform, and unmanned plane charging device；The unmanned plane include lithium battery, d GPS locating module,
Flight drive module, capture apparatus and wireless communication module；Each communication platform is at least equipped with a unmanned plane；When carrying out nothing
During line monitoring task, at the same start m unmanned plane be monitored, 1≤m≤n, to m unmanned plane by area to be monitored
Time point and flight path are coordinated, it is ensured that in each unmanned plane of same time not by identical area to be monitored, and in rule
Interior each unmanned plane of fixing time covers all areas to be monitored；Each unmanned plane meets image with the coverage closest to communication platform
During information transfer required distance, the image information of new storage is transmitted to immediate communication platform, passed through by the communication platform
Wired or wireless network transmits to director server image information, by director server to fly state unmanned plane be monitored and
Analysis, or send broadcast；Each unmanned plane electricity as little as safe flight electricity scope when, select suitable communication platform to enter nearby
Row charges, and sends the unmanned plane of sufficient electricity to replace charging unmanned plane to continue to monitor by the communication platform.
2. unmanned aerial vehicle group intelligent scheduling monitoring method according to claim 1, it is characterized in that：The charging device is included
Line charging device and wireless charging device.
3. unmanned aerial vehicle group intelligent scheduling monitoring method according to claim 2, it is characterized in that：Wired charging device,
Matching installation respectively is provided with two grooves, groove in the middle part of unmanned plane landing platform non-conductive socket, and two conductions are inserted
Groove is connected by wire with charger and power supply；Two parallel conductive bullets are additionally provided with the middle part of unmanned plane landing platform
Piece, the front end or middle part of two parallel electroconductive elastic sheets are provided with conductive contact, and after two electroconductive elastic sheets are depressed, two is conductive
Contact can be inserted in corresponding non-conductive socket respectively；Flexible baffle is fixed with the leading edge of unmanned plane landing platform, unmanned plane rises
The both sides for dropping platform are provided with the flexible baffle of divergent shape, and most narrow section of both sides flexible baffle is wide more than or equal to unmanned plane both sides
Degree；Electromagnet is respectively arranged with each flexible baffle, the front side and both sides of unmanned plane body are respectively arranged with magnetic conductor, respectively
Magnetic conductor is corresponding with corresponding electromagnet position；The front side bottom of unmanned plane is respectively arranged with two conductive contact blades, two conductive contact blades
Width it is consistent with the two electroconductive elastic sheets width；The electromagnet is connected with controller output end, the letter of wireless telecommunications system
Number output end is connected with controller signals input；When unmanned plane sends falling signal and is close to unmanned plane landing platform, lead to
Cross controller control electromagnet to be powered, unmanned plane is positioned, make two conductive contact blades of unmanned plane and unmanned plane landing platform
Two electroconductive elastic sheets laminating charge, when after charging terminates stop charge, it is necessary to unmanned plane perform take off task when, by controller
Control electromagnet power-off, starts unmanned plane and takes off.
4. unmanned aerial vehicle group intelligent scheduling monitoring method according to claim 3, it is characterized in that：The unmanned plane landing platform
Front-end and back-end be respectively arranged with front end signal transmitter A and back end signal transmitter B, the body front end of the unmanned plane and
Rear end is respectively arranged with front end signal receiver A ' and back end signal receiver B '.
5. unmanned aerial vehicle group intelligent scheduling monitoring method according to claim 2, it is characterized in that：The wireless charging device,
Inner chamber is internally provided with unmanned plane landing platform, transmitting coil is installed in inner chamber, the transmitting coil passes through relay
Electrically connected with city；Flexible baffle is fixed with the leading edge of unmanned plane landing platform, the both sides of unmanned plane landing platform are provided with
The flexible baffle of divergent shape；Electromagnet is respectively arranged with each flexible baffle, the front side of unmanned plane body and both sides are distinguished
Magnetic conductor is provided with, each magnetic conductor is corresponding with corresponding electromagnet position；The electromagnet is connected with controller output end, channel radio
The signal output part of news equipment is connected with controller signals input, and coil control end and the controller output end of relay connect
Connect；When unmanned plane sends falling signal and is close to unmanned plane landing platform, electromagnet is controlled to be powered by controller, to nobody
Machine is positioned, and when stopping charging after charging terminates, it is necessary to unmanned plane is performed when taking off task, electromagnet is controlled by controller
Power-off, starts unmanned plane and takes off.
6. unmanned aerial vehicle group intelligent scheduling monitoring method according to claim 5, it is characterized in that：Both sides flexible baffle it is most narrow
Section is more than or equal to unmanned plane both sides width.
7. unmanned aerial vehicle group intelligent scheduling monitoring method according to claim 5, it is characterized in that：The unmanned plane landing platform
Front-end and back-end be respectively arranged with front end signal transmitter A and back end signal transmitter B, the body front end of the unmanned plane and
Rear end is respectively arranged with front end signal receiver A ' and back end signal receiver B '.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611268763.XA CN106814748B (en) | 2016-12-31 | 2016-12-31 | Intelligent scheduling monitoring method for unmanned aerial vehicle group |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611268763.XA CN106814748B (en) | 2016-12-31 | 2016-12-31 | Intelligent scheduling monitoring method for unmanned aerial vehicle group |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106814748A true CN106814748A (en) | 2017-06-09 |
| CN106814748B CN106814748B (en) | 2020-07-10 |
Family
ID=59110420
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611268763.XA Active CN106814748B (en) | 2016-12-31 | 2016-12-31 | Intelligent scheduling monitoring method for unmanned aerial vehicle group |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106814748B (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107656544A (en) * | 2017-11-10 | 2018-02-02 | 广东工业大学 | A kind of method and system of unmanned aerial vehicle (UAV) control |
| CN107741219A (en) * | 2017-10-16 | 2018-02-27 | 金陵科技学院 | A kind of mine data collector |
| CN108255163A (en) * | 2018-01-24 | 2018-07-06 | 衢州职业技术学院 | The control system and control method of plant protection unmanned plane |
| CN110007689A (en) * | 2019-04-26 | 2019-07-12 | 北京中科星通技术有限公司 | The method for allocating tasks and device of anteiso- structure unmanned plane |
| CN111045446A (en) * | 2019-11-04 | 2020-04-21 | 西安天和防务技术股份有限公司 | Maintenance method, equipment and system for unmanned aerial vehicle |
| CN111722639A (en) * | 2019-03-18 | 2020-09-29 | 北京京东尚科信息技术有限公司 | Takeoff control method, device and system of unmanned aerial vehicle cluster and readable medium |
| CN112068592A (en) * | 2020-08-31 | 2020-12-11 | 南京航空航天大学 | Dispatching method for realizing fence coverage based on rechargeable unmanned aerial vehicle |
| CN112937858A (en) * | 2021-01-29 | 2021-06-11 | 天津航天中为数据系统科技有限公司 | Novel inspection method for vertical take-off and landing fixed wing unmanned aerial vehicle |
| CN113418448A (en) * | 2021-06-23 | 2021-09-21 | 西北核技术研究所 | Fragment distribution detection system and method |
| WO2022036594A1 (en) * | 2020-08-19 | 2022-02-24 | 唐山哈船科技有限公司 | Sea port patrolling system based on unmanned aerial vehicle |
| CN115762025A (en) * | 2022-12-12 | 2023-03-07 | 德昱电力工程设计有限公司 | Intelligent early warning method and system for communication optical cable |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103197684A (en) * | 2013-04-25 | 2013-07-10 | 清华大学 | Method and system for cooperatively tracking target by unmanned aerial vehicle cluster |
| CN104503349A (en) * | 2014-12-10 | 2015-04-08 | 天津大学 | Monitoring device based on unmanned aerial vehicle |
| CN104836640A (en) * | 2015-04-07 | 2015-08-12 | 西安电子科技大学 | Unmanned plane formation distributed cooperative communication method |
| CN104898690A (en) * | 2015-04-07 | 2015-09-09 | 中南大学 | Rotor unmanned aerial vehicle self journey-continuing realization method based on APM platform |
| CN105389988A (en) * | 2015-12-07 | 2016-03-09 | 北京航空航天大学 | Multi-unmanned aerial vehicle cooperation highway intelligent inspection system |
| CN105553116A (en) * | 2016-01-19 | 2016-05-04 | 刘勇 | Landing capture device for unmanned aerial vehicle |
| CN105763230A (en) * | 2016-05-03 | 2016-07-13 | 中国科学院自动化研究所 | Movable multi-rotor unmanned aerial vehicle autonomous base station system |
| US20160332748A1 (en) * | 2014-05-30 | 2016-11-17 | SZ DJI Technology Co., Ltd | Systems and methods for uav docking |
-
2016
- 2016-12-31 CN CN201611268763.XA patent/CN106814748B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103197684A (en) * | 2013-04-25 | 2013-07-10 | 清华大学 | Method and system for cooperatively tracking target by unmanned aerial vehicle cluster |
| US20160332748A1 (en) * | 2014-05-30 | 2016-11-17 | SZ DJI Technology Co., Ltd | Systems and methods for uav docking |
| CN104503349A (en) * | 2014-12-10 | 2015-04-08 | 天津大学 | Monitoring device based on unmanned aerial vehicle |
| CN104836640A (en) * | 2015-04-07 | 2015-08-12 | 西安电子科技大学 | Unmanned plane formation distributed cooperative communication method |
| CN104898690A (en) * | 2015-04-07 | 2015-09-09 | 中南大学 | Rotor unmanned aerial vehicle self journey-continuing realization method based on APM platform |
| CN105389988A (en) * | 2015-12-07 | 2016-03-09 | 北京航空航天大学 | Multi-unmanned aerial vehicle cooperation highway intelligent inspection system |
| CN105553116A (en) * | 2016-01-19 | 2016-05-04 | 刘勇 | Landing capture device for unmanned aerial vehicle |
| CN105763230A (en) * | 2016-05-03 | 2016-07-13 | 中国科学院自动化研究所 | Movable multi-rotor unmanned aerial vehicle autonomous base station system |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107741219A (en) * | 2017-10-16 | 2018-02-27 | 金陵科技学院 | A kind of mine data collector |
| CN107656544A (en) * | 2017-11-10 | 2018-02-02 | 广东工业大学 | A kind of method and system of unmanned aerial vehicle (UAV) control |
| CN107656544B (en) * | 2017-11-10 | 2020-10-23 | 广东工业大学 | Unmanned aerial vehicle control method and system |
| CN108255163A (en) * | 2018-01-24 | 2018-07-06 | 衢州职业技术学院 | The control system and control method of plant protection unmanned plane |
| CN111722639A (en) * | 2019-03-18 | 2020-09-29 | 北京京东尚科信息技术有限公司 | Takeoff control method, device and system of unmanned aerial vehicle cluster and readable medium |
| CN110007689A (en) * | 2019-04-26 | 2019-07-12 | 北京中科星通技术有限公司 | The method for allocating tasks and device of anteiso- structure unmanned plane |
| CN111045446A (en) * | 2019-11-04 | 2020-04-21 | 西安天和防务技术股份有限公司 | Maintenance method, equipment and system for unmanned aerial vehicle |
| CN111045446B (en) * | 2019-11-04 | 2023-03-10 | 西安天和防务技术股份有限公司 | Maintenance method, equipment and system for unmanned aerial vehicle |
| WO2022036594A1 (en) * | 2020-08-19 | 2022-02-24 | 唐山哈船科技有限公司 | Sea port patrolling system based on unmanned aerial vehicle |
| CN112068592A (en) * | 2020-08-31 | 2020-12-11 | 南京航空航天大学 | Dispatching method for realizing fence coverage based on rechargeable unmanned aerial vehicle |
| CN112937858A (en) * | 2021-01-29 | 2021-06-11 | 天津航天中为数据系统科技有限公司 | Novel inspection method for vertical take-off and landing fixed wing unmanned aerial vehicle |
| CN113418448A (en) * | 2021-06-23 | 2021-09-21 | 西北核技术研究所 | Fragment distribution detection system and method |
| CN113418448B (en) * | 2021-06-23 | 2022-03-22 | 西北核技术研究所 | Fragment distribution detection system and method |
| CN115762025A (en) * | 2022-12-12 | 2023-03-07 | 德昱电力工程设计有限公司 | Intelligent early warning method and system for communication optical cable |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106814748B (en) | 2020-07-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106814748A (en) | Unmanned aerial vehicle group intelligent scheduling monitoring method | |
| CN106787258A (en) | Unmanned plane, charging base station, wireless charging system and method | |
| US9828093B2 (en) | System for recharging remotely controlled aerial vehicle, charging station and rechargeable remotely controlled aerial vehicle, and method of use thereof | |
| CN108819775A (en) | A kind of power-line patrolling unmanned plane wireless charging relay system and charging method | |
| CN206517519U (en) | The wired charging system of unmanned plane | |
| US10207591B2 (en) | Mobile vehicle charging system | |
| CN105427661A (en) | Large-sized parking space detection system based on solar unmanned aerial vehicle group and working method thereof | |
| CN105717932A (en) | Unmanned plane vehicle-mounted monitoring and command system | |
| CN104503349A (en) | Monitoring device based on unmanned aerial vehicle | |
| KR101899395B1 (en) | System and method for detecting event using unmanned aerial vehicle | |
| KR20170132923A (en) | Control system for unmanned assignment of drone | |
| KR102160734B1 (en) | Image taking system using wireless rechargeable drones | |
| CN111391681B (en) | Charging system and charging management platform of portable wireless transmitting terminal that charges | |
| CN105375608A (en) | Unmanned shipborne charging system and charging method for unmanned aerial vehicle charging | |
| CN106972597A (en) | A kind of rail mounted unmanned plane automatic charge device | |
| CN106655322A (en) | Service type unmanned plane, unmanned plane charging system and charging method | |
| CN106840107A (en) | Unmanned aerial vehicle group intelligent scheduling monitoring system | |
| CN103576691B (en) | 3G police service unmanned plane managing and control system | |
| CN206479172U (en) | Unmanned aerial vehicle group intelligent scheduling monitoring system | |
| Costea et al. | Automatic battery charging system for electric powered drones | |
| CN206401916U (en) | A kind of wireless power supply system for unmanned plane | |
| JP2017221094A (en) | Movable machine charging system | |
| CN206313544U (en) | Unmanned plane wireless charging system | |
| CN106394918A (en) | Unmanned aerial vehicle carried panorama camera system and operation method thereof | |
| CN109774500A (en) | A kind of orderly charging system of laser unmanned plane |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |