CN206479172U - Unmanned aerial vehicle group intelligent scheduling monitoring system - Google Patents
Unmanned aerial vehicle group intelligent scheduling monitoring system Download PDFInfo
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- CN206479172U CN206479172U CN201621486913.XU CN201621486913U CN206479172U CN 206479172 U CN206479172 U CN 206479172U CN 201621486913 U CN201621486913 U CN 201621486913U CN 206479172 U CN206479172 U CN 206479172U
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Abstract
The utility model discloses a kind of unmanned aerial vehicle group intelligent scheduling monitoring system, multiple communication platforms are arranged at intervals with the edge or inside of area to be monitored, communication platform is provided with can carry out the wireless telecommunications system of image information transmission with unmanned plane, and the equipment that wired or wireless transmission can be carried out with director server；To multiple unmanned planes coordinate by the time point and flight path of area to be monitored.Charging device is wired charging device or wireless charging device, and communication platform is fixed, or is portable communication platform.The utility model solves great amount of images information and transmits problem in real time, so as to meet the purpose for implementing monitoring.Solving unmanned plane must frequent charge the problem of could keep regular flight condition.Solve each unmanned plane of many sorties different moment can not 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 utility model 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 system
System.
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, and aeroplane photography instrument is used as using unmanned plane
Turn into the main flow developed at present.Unmanned plane can be applied to take photo by plane, forest protection, the condition of a disaster prospecting etc. monitoring application scenario.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 carry out take photo by plane etc. apply when, generally by nobody
Machine is shot to current environment scene, and the ambient image photographed is stored in into 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 unmanned plane whole process shoots and 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 operated in real time.Due to all kinds of natural calamities and accident frequency
Hair, if can not understand state of affairs progress in time, can seriously limit the rescue to disaster and assess 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 what the unmanned planes 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 monitored in real time.
Again, it is existing that the monitoring in small range region can only be directed to by way of unmanned plane carries out no worker monitor, when facing
During the monitoring of a wide range of and overlength distance, it is impossible to realize region and the time coordination of many sorties automatically.And blind area can not 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 high many spiral Vertical Lift unmanned planes, increase is taken off, and sortie progress is frequent to be monitored and monitors simultaneously.In fact, no matter
How spiral Vertical Lift unmanned plane during flying mileage increases, and has scope limitation, 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,
The high tracking system real-time dynamic of mobility strong, synchronizing information.
Utility model content
The problem of the utility model exists for the management of existing unmanned plane and deficiency, it is proposed that a kind of scope is wide, without dead angle,
The high unmanned plane panorama tracking system real-time dynamic of mobility strong, synchronizing information.
Adopt the following technical scheme that to achieve the above object：A kind of unmanned aerial vehicle group intelligent scheduling monitoring system, including nobody
Machine and director server, it is characterized in that：N communication platform is arranged at intervals with the edge or inside of area to be monitored, and to being supervised
Survey region and be divided into p monitoring section；The communication platform is provided with can carry out the wireless telecommunications of image information transmission with unmanned plane
Equipment, each communication platform is provided with the equipment that wired or wireless transmission is carried out with director server；The communication platform is provided with nothing
Man-machine landing platform, and unmanned plane charging device；The unmanned plane includes lithium battery, d GPS locating module, flight driving mould
Block, capture apparatus and wireless communication module；Each communication platform is at least equipped with a unmanned plane.
The charging device is wired charging device or wireless charging device.
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；It is respectively arranged with each flexible baffle before electromagnet, 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 is set 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.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 '.
The wireless charging device, charging hair is provided with being internally provided with inner chamber, inner chamber for unmanned plane landing platform
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
Be connected after mu balanced circuit with the battery charger in unmanned plane；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 the gps coordinate judging distance platform of unmanned plane in itself,
When the position at place is when 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 neck, and neck top is set
Fastener is equipped with, one end of fastener is hinged on neck side wall, and the other end of fastener is connected to neck opposite side wall by locking member.
The communication platform is fixed, or is portable communication platform.The portable communication platform is included containing drive
The car body and track of power, the rail wheel Matching installation of vehicle bottom is on track；Wireless telecommunications are provided with the car body to set
Standby and d GPS locating module and power module；Wireless telecommunications system is used to set up server communication over long distances and to unmanned plane
Set up short distance communication；The side of the car body is provided with unmanned plane hoistable platform.The front end of the unmanned plane landing platform and
Rear end is respectively arranged with front end signal transmitter A and back end signal transmitter B, the body front-end and back-end difference of the unmanned plane
It is provided with front end signal receiver A ' and back end signal receiver B '.Front end signal transmitter A as front end guidance signal source, after
End signal transmitter B guides signal source as rear end.
Beneficial effect：The utility model solves topmost three problems of monitoring unmanned：One is to solve big spirogram
As information transmits problem in real time, so as to meet the purpose for implementing monitoring.Two be solve unmanned plane must frequent charge could protect
The problem of holding regular flight condition.Three be solve each unmanned plane of many sorties different moment can not effective scheduling problem, realize
Reasonable distribution flight range and flight time, it is to avoid repeat to monitor and leakage side problem.
The utility model has image information real-time Transmission function, each unmanned plane and the coverage closest to communication platform
When meeting the requirement of image information transmission range, the image information newly stored is transmitted to immediate communication platform.So as to each nothing
It is man-machine that great amount of images information can be transferred to nearest communication platform with most fast speed, and in time will letter by the communication platform
Breath passes to director server.It need not be maked a return voyage without landing with regard to image information transmission can be carried out.
The utility model is adapted to the function of monitoring on a large scale, and each communication platform United Dispatching cooperates, and unmanned plane is continuous
Rise and fall within each dispatching platform, constantly change and the unmanned function of continuation of the journey realizes uninterrupted monitoring task, realize remote continuous prison
The characteristics of survey.
The utility model can be to each unmanned plane electric energy supplement, and alternately flight is so as to realize continuous monitoring.Realize electric energy and
When supplement.
Brief description of the drawings
Fig. 1 is one of communication platform course line of the present utility model path schematic diagram；
Fig. 2 is the two of communication platform course line of the present utility model path schematic diagram；
Fig. 3 is the unmanned plane landing platform containing wired charging device；
Fig. 4 is Fig. 3 A-A cross-sectional views；
Fig. 5 is Fig. 3 circuit connection block diagram；
Fig. 6 is the unmanned plane landing platform schematic diagram containing wireless charging function；
Fig. 7 is affixed to the base side structural representation on unmanned plane bottom bracket；
Fig. 8 is Fig. 7 schematic top plan view；
Fig. 9 is the circuit connection block diagram used in this Fig. 6 and Fig. 7；
Figure 10 is the structural representation of portable communication platform.
Label in figure, 1 is communication platform, and 2 be area to be monitored, and 3 be unmanned plane during flying circuit, and 4 be divided monitoring
Area, 5 be unmanned plane landing platform, and 6 be electroconductive elastic sheet, and 7 be conductive contact, and 8 be groove, and 9 be non-conductive socket, and 10 be that leading edge is soft
Property baffle plate, 11 be both sides flexible baffle, 12 be electromagnet, and 13 be socket, and 14 be plug, 20 be front end guidance signal source, 21 are
Rear end guides signal source, and 22 be the car body of portable communication platform, and 23 be track, and 30 be neck, and 31 be base, and 32 be fastener,
33 be charging receiving coil, and 34 be magnet arrangement, and 35 be bearing pin, and 36 be the parallel bracket of unmanned motor spindle, and 37 rise for unmanned plane
Platform drops, and 38 be charging transmitting coil, and 39 be electromagnetism iron ring.
Embodiment
Embodiment 1：A kind of unmanned aerial vehicle group intelligent scheduling monitoring system, is in area to be monitored referring to Fig. 1 or Fig. 2, Fig. 1
Edge is provided with multiple communication platforms 1, and Fig. 2 is that detected region 2 is divided into p monitoring section.Communication platform 1 is provided with can be with nothing
The wireless telecommunications system of man-machine carry out image information transmission, because unmanned plane is constantly recorded and stored by high-definition camera largely
Data, not easily pass through wireless network transmissions（Not only signal stabilization is poor for wireless network transmissions, and needs flow very big, cost
It is very high）.When unmanned plane is close to certain communication platform 1, the image information that can be set up by wife and unmanned plane in LAN is transmitted,
Ensure rapidly and efficiently to transmit data.Unmanned plane uses many spiral unmanned planes, can control flying speed and can be detained in the air, nobody
Machine in the coverage scope by communication platform 1, appropriate reduction flying speed wait after the completion of data transfer again quickly through.
Properly, real-time Transmission is can be achieved in unmanned plane to distance substantially between adjacent communication platform 1, and the Monitoring Data of carrying is synchronized to
Nearest communication platform 1.
The equipment that communication platform 1 can carry out wired or wireless transmission with director server, communication platform 1 can contain more perfect
Transceiver, and short distance between communication platform 1 communicates with one another function, can be wirelessly by mass data
It is transferred to server.
Communication platform 1 is provided with unmanned plane landing platform 5, and unmanned plane charging device.Unmanned plane include lithium battery,
D GPS locating module, flight drive module, capture apparatus and wireless communication module.Each communication platform 1 is at least equipped with a nothing
It is man-machine.
When carrying out wireless monitor task, it is monitored while starting multiple unmanned planes, 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 1, will newly it deposit
The image information of storage is transmitted to immediate communication platform 1, by the communication platform 1 by wired or wireless network by image information
Transmit to director server, by director server to being monitored and analyzed in the unmanned plane for flying state, or send broadcast.
Each unmanned plane electricity as little as safe flight electricity scope when, select suitable communication platform 1 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 1.
This implementation uses wired charging device, and referring to Fig. 3 and Fig. 4, the middle part of unmanned plane landing platform 5 is provided with two
Matching installation has non-conductive socket 9 respectively in groove 8, groove 8, and two non-conductive sockets 9 are connected by wire with charger and power supply；
Two parallel electroconductive elastic sheets 6, the front end of two parallel electroconductive elastic sheets 6 are additionally provided with the middle part of unmanned plane landing platform 5
Or middle part is provided with conductive contact 7, after two electroconductive elastic sheets 6 are depressed, two conductive contacts 7 can insert corresponding conductive slotting respectively
In groove 9；Flexible baffle is fixed with the leading edge of unmanned plane landing platform 5, the both sides of unmanned plane landing platform 5 are provided with diverging
The flexible baffle of shape, most narrow section of both sides flexible baffle is more than or equal to unmanned plane both sides width；Divide on each flexible baffle
Electromagnet 12 is not provided with, and the front side and both sides of unmanned plane body are respectively arranged with magnetic conductor, each magnetic conductor and corresponding electromagnet
12 positions correspondence；The front side bottom of unmanned plane is respectively arranged with two conductive contact blades, and the width of two conductive contact blades is led with described two
The electric width of shell fragment 6 is consistent.
Referring to Fig. 5, electromagnet 12 is connected with controller output end, and signal output part and the controller of wireless telecommunications system are believed
The connection of number input；When unmanned plane sends falling signal and close unmanned plane landing platform 5, electromagnet is controlled by controller
12 are powered, and unmanned plane is positioned, two conductive contact blades of unmanned plane is pasted with two electroconductive elastic sheets 6 of unmanned plane landing platform 5
Charging is closed, when stopping charging after charging terminates, it is necessary to which unmanned plane is performed when taking off task, controls electromagnet 12 to break by controller
Electricity, starts unmanned plane and takes off.The front-end and back-end of the unmanned plane landing platform 5 be respectively arranged with front end signal transmitter A and
Back end signal transmitter B, the body front-end and back-end of the unmanned plane are respectively arranged with front end signal receiver A ' and rear end letter
Number receiver B '.Front end signal transmitter A is as front end guidance signal source, and back end signal transmitter B guides signal as rear end
Source.Front end signal transmitter A is different with signal projector B signal to be used to distinguish anteroposterior position.
Embodiment 2：Another unmanned aerial vehicle group intelligent scheduling monitoring system, on the basis of embodiment 1, by wired charging device
Wireless charging device is revised as, referring to Fig. 6, charging is installed in being internally provided with inner chamber, inner chamber for unmanned plane landing platform 7
Transmitting coil 38, charging transmitting coil 38 is electrically connected by relay normally open Duan Yu cities, and whether the coil of relay is powered will be by
Controller is controlled.
Referring to Fig. 7 and Fig. 8, base 31 is installed with the parallel bar support of unmanned motor spindle, is set inside base 31
There is charging receiving coil 33.Base 31 on the parallel bar support 36 of unmanned motor spindle is provided with neck 30, neck 30
Portion is provided with fastener 32, and one end of fastener 32 is hinged on the side wall of neck 30 by bearing pin 35, and the other end of fastener 32 passes through lock
Tight part is connected to the opposite side wall of neck 30.
Referring to Fig. 9, the output end of the charging receiving coil 33 inside base 31 is sequentially connected rectification circuit and voltage stabilizing
It is connected after circuit with the battery charger in unmanned plane.
In addition, being provided with electromagnetism iron ring 39 in the inner chamber of unmanned plane landing platform 37, and set inside the base 1
There is magnet arrangement 34., can be by base 1 in order to ensure the surface of charging transmitting coil 88 is located at the bottom on unmanned machine support
Length L >=electromagnet loop diameter D.
Electromagnetism iron ring 39 is connected with controller output end, and signal output part and the controller signals of wireless telecommunications system are inputted
End connection, the coil control end of relay is connected with controller output end.
When the unmanned plane region nearby maked a return voyage, pass through the gps coordinate judging distance platform of unmanned plane in itself
Position, when the position at place is when in the range of setting, platform can be powered by magnetic induction loop, and unmanned plane is drawn down, nothing
Base 31 on people's motor spindle parallel bar support can be adsorbed in the optional position of platform surface, charged, filled by charge coil
Stopped power supply after the completion of electricity, gravitation disappears therewith.
Embodiment 3：Another unmanned aerial vehicle group intelligent scheduling monitoring system, does on the basis of embodiment 1 or embodiment 2
Go out to improve, and embodiment 1 or embodiment 2 unlike, it is fixed, this reality that embodiment 1 or embodiment 2, which employ communication platform,
Apply example and employ portable communication platform.
Shown in Figure 8, portable communication platform includes car body and track 23 containing driving force, portable communication platform
The rail wheel Matching installation of the bottom of car body 22 is on track 23；Wireless telecommunications system and GPS location mould are provided with the car body
Block and power module；Wireless telecommunications system is used to set up server communication over long distances and set up unmanned plane short distance to lead to
News；The side of the car body is provided with unmanned plane hoistable platform.The front-end and back-end of the unmanned plane landing platform are set respectively
There are front end signal transmitter A and back end signal transmitter B, the body front-end and back-end of the unmanned plane are respectively arranged with front end letter
Number receiver A ' and back end signal receiver B '.
Claims (9)
1. a kind of unmanned aerial vehicle group intelligent scheduling monitoring system, including unmanned plane and director server, it is characterized in that：In area to be monitored
Edge or inside be arranged at intervals with n communication platform, and p monitoring section is divided into area to be monitored；The communication platform
The wireless telecommunications system of image information transmission can be carried out with unmanned plane by being provided with, and each communication platform is provided with to be carried out with director server
The equipment of wired or wireless transmission；The communication platform is provided with unmanned plane landing platform, and unmanned plane charging device；It is described
Unmanned plane includes lithium battery, d GPS locating module, flight drive module, capture apparatus and wireless communication module；Each communication platform
At least equipped with a unmanned plane.
2. unmanned aerial vehicle group intelligent scheduling monitoring system according to claim 1, it is characterized in that：The charging device is wired
Charging device or wireless charging device.
3. unmanned aerial vehicle group intelligent scheduling monitoring system 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, after two electroconductive elastic sheets are depressed, and 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 of drop 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.
4. unmanned aerial vehicle group intelligent scheduling monitoring system 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 system according to claim 2, it is characterized in that：In unmanned plane landing platform
It is internally provided with inner chamber, inner chamber and charging transmitting coil is installed, the charging transmitting coil passes through relay normally open Duan Yu cities
Electrical connection；Base is installed with the parallel bar support of unmanned motor spindle, chassis interior is provided with charging receiving coil, is charged
The output end of receiving coil is sequentially connected after rectification circuit and mu balanced circuit to be connected with the battery charger in unmanned plane；Together
When, electromagnetism iron ring is provided with the inner chamber of unmanned plane landing platform, and the chassis interior is provided with magnet arrangement；It is described
Electromagnetism iron ring is connected with controller output end, and the signal output part of wireless telecommunications system is connected with controller signals input, after
The coil control end of electrical equipment is connected with controller output end.
6. unmanned aerial vehicle group intelligent scheduling monitoring system according to claim 5, it is characterized in that positioned at the flat of unmanned motor spindle
Base on row bar support is provided with neck, and neck top is provided with fastener, and one end of fastener is hinged on neck side wall, fastener
The other end neck opposite side wall is connected to by locking member.
7. unmanned aerial vehicle group intelligent scheduling monitoring system according to claim 1, it is characterized in that：The communication platform is fixation
Formula, or be portable communication platform.
8. unmanned aerial vehicle group intelligent scheduling monitoring system according to claim 7, it is characterized in that：The portable communication platform
Including car body and track containing driving force, the rail wheel Matching installation of vehicle bottom is on track；Nothing is provided with the car body
Line communication apparatus and d GPS locating module and power module；Wireless telecommunications system be used for server set up over long distances communication and
Short distance communication is set up to unmanned plane；The side of the car body is provided with unmanned plane hoistable platform.
9. unmanned aerial vehicle group intelligent scheduling monitoring system according to claim 7, 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 |
|---|---|---|---|
| CN201621486913.XU CN206479172U (en) | 2016-12-31 | 2016-12-31 | Unmanned aerial vehicle group intelligent scheduling monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621486913.XU CN206479172U (en) | 2016-12-31 | 2016-12-31 | Unmanned aerial vehicle group intelligent scheduling monitoring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206479172U true CN206479172U (en) | 2017-09-08 |
Family
ID=59751370
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621486913.XU Expired - Fee Related CN206479172U (en) | 2016-12-31 | 2016-12-31 | Unmanned aerial vehicle group intelligent scheduling monitoring system |
Country Status (1)
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| CN (1) | CN206479172U (en) |
Cited By (2)
| 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 |
| CN112422785A (en) * | 2020-10-14 | 2021-02-26 | 中国航天科工集团第二研究院 | Video monitoring and processing method and system for unmanned distributed mobile deployment |
-
2016
- 2016-12-31 CN CN201621486913.XU patent/CN206479172U/en not_active Expired - Fee Related
Cited By (3)
| 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 |
| CN107656544B (en) * | 2017-11-10 | 2020-10-23 | 广东工业大学 | Unmanned aerial vehicle control method and system |
| CN112422785A (en) * | 2020-10-14 | 2021-02-26 | 中国航天科工集团第二研究院 | Video monitoring and processing method and system for unmanned distributed mobile deployment |
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Granted publication date: 20170908 Termination date: 20211231 |