CN206741310U - Multiple no-manned plane communication control system - Google Patents
Multiple no-manned plane communication control system Download PDFInfo
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- CN206741310U CN206741310U CN201720465393.2U CN201720465393U CN206741310U CN 206741310 U CN206741310 U CN 206741310U CN 201720465393 U CN201720465393 U CN 201720465393U CN 206741310 U CN206741310 U CN 206741310U
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Abstract
The utility model discloses a kind of multiple no-manned plane communication control system, including earth station and more set UASs, the earth station includes ground monitoring system and data communication system, for monitoring UAS, sends order to UAS and receives the data message that UAS is passed back；Wherein often covering UAS includes being used for wireless communication unit, microcomputer unit, the flight control units for controlling unmanned plane during flying posture, the positioning unit for realizing global positioning navigation, driver element, the mechanical structure unit for unmanned plane normal flight, the perception unit for perceiving surrounding environment, electric power detection unit and the power supply of driving unmanned plane operating for realizing function of surfing the Net；The utility model greatly reduces the complexity of equipment redundancy and system, and enhance the portability of multiple no-manned plane communication control system by one-to-many multiple no-manned plane Control on Communication mode.
Description
Technical field
UAV Communication control field is the utility model is related to, more particularly, to a kind of multiple no-manned plane communication control system.
Background technology
With the fast development of UAS and its correlation technique, the application of unmanned plane is increasingly extensive.Military, civilian
In terms of commercialization, unmanned plane is widely used in the fields such as scouting, cargo assault, agricultural plant protection and target tracking of taking photo by plane.
But with application environment, gradually complicated and task difficulty gradually increases, and traditional single unmanned plane is in the task of execution
During easily limited by including the flight visual field, cruising ability is poor, the factor such as cooperative ability deficiency restricts between unmanned plane,
Task can not be performed well.By contrast, multiple no-manned plane is performed in unison with having significant advantage, such as multi-machine collaborative during task
Tracking etc..And for the work compound problem of multiple no-manned plane, the existing equal Shortcomings of multiple no-manned plane communication control system.At present
Unmanned aerial vehicle control platform mostly use man-to-man Control on Communication mode, function is single and does not have multiple air combat function.
And realize the lifting of the Control on Communication mode equipment complexity of multi-to-multi, system portable ability by integrating more complete equipments
Difference and communication, which exist, to be disturbed.The Control on Communication mode of current this multi-to-multi can not also flexibly realize to single rack and to multi rack nobody
The switching of machine control.
Utility model content
The shortcomings that main purpose of the present utility model is to overcome prior art and deficiency, there is provided a kind of multiple no-manned plane communication
Control system, the utility model greatly reduce equipment redundancy and system by one-to-many multiple no-manned plane Control on Communication mode
Complexity, and enhance the portability of multiple no-manned plane communication control system.
In order to achieve the above object, the utility model uses following technical scheme：
The utility model discloses a kind of multiple no-manned plane communication control system, including earth station to cover UASs more with,
The earth station includes ground monitoring system and data communication system, for monitoring UAS, is sent to UAS
The data message that order and reception UAS are passed back；Wherein often covering UAS includes being used for the nothing for realizing function of surfing the Net
Line communication unit, microcomputer unit, the flight control units for controlling unmanned plane during flying posture, for realizing that the whole world is fixed
The positioning unit of position navigation, the driver element of driving unmanned plane operating, the mechanical structure unit for unmanned plane normal flight, use
In the perception unit, electric power detection unit and the power supply that perceive surrounding environment；Described wireless communication unit and microcomputer
Unit is connected, and radio communication function and service on net are provided for UAS；Described positioning unit and flight control units
It is joined directly together, realizes unmanned plane location navigation；Described driver element is joined directly together with flight control units；Described machinery knot
Structure unit is connected with driver element, and is equipped on a whole set of UAS, realizes unmanned plane operating flight；Described perception unit
It is joined directly together with microcomputer unit, installed in UAS periphery；Described electric power detection unit connects power supply and flown
Row control unit, send electric quantity data to flight control units in time；Described power supply directly enters to a whole set of UAS
Row power supply.
As preferable technical scheme, the wireless communication unit uses 3G/4G wireless Internet cards and WIFI wireless network cards
Carry out radio communication.
As preferable technical scheme, the flight control units are to include carrying barometer, accelerometer and gyroscope
The flight control panel of sensor, the flight control panel can utilize the numerical value for obtaining current flight state lower plate set sensor.
As preferable technical scheme, the positioning unit includes M8N-GPS modules and compass, realizes to UAS
Positioning.
As preferable technical scheme, the driver element includes brushless electric machine and electricity is adjusted, and is controlled by flight control units
Driver element, for drive mechanism unit so as to realizing unmanned plane airflight.
As preferable technical scheme, it is described perception unit include ultrasonic wave module, temperature sensor, humidity sensor with
And PM2.5 sensors, for obtaining ultrasonic wave, temperature, humidity and the PM2.5 parameters of external environment, realize to external environment condition
Monitoring in real time.
The utility model compared with prior art, has the following advantages that and beneficial effect：
1st, the utility model is directly by one-to-many multiple no-manned plane Control on Communication mode, greatly reduce equipment redundancy and
The complexity of system, and enhance the portability of multiple no-manned plane communication control system.
2nd, the utility model also introduces the function of packet control, realizes the task control to single or multiple unmanned units,
Improve collaboration capabilities and the flexibility of unmanned aerial vehicle group.
3rd, data communication mode of the present utility model mainly uses 3G/4G mobile communication, has communication distance length, and communicate model
Enclose wide, the features such as time delay is low.
Brief description of the drawings
Fig. 1 is the hardware annexation schematic diagram of the utility model multiple no-manned plane communication control system.
Fig. 2 is the system architecture diagram of the utility model multiple no-manned plane communication control system.
Fig. 3 is the group-net communication schematic diagram of the utility model multiple no-manned plane communication control system.
Embodiment
The utility model is described in further detail with reference to embodiment and accompanying drawing, but implementation of the present utility model
Mode not limited to this.
Embodiment
As shown in figure 1, a kind of multiple no-manned plane communication control system of the utility model, including earth station and more set unmanned plane systems
System, the earth station includes ground monitoring system and data communication system, for monitoring UAS, is sent out to UAS
Lose one's life and make and receive the data message that UAS is passed back.Wherein often covering UAS includes being used to realize function of surfing the Net
Wireless communication unit, microcomputer unit, for controlling the flight control units of unmanned plane during flying posture, for realizing the whole world
The positioning unit of location navigation, the driver element of driving unmanned plane operating, the mechanical structure unit for unmanned plane normal flight,
Perception unit, electric power detection unit and power supply for perceiving surrounding environment etc..
Described wireless communication unit is connected with microcomputer unit, for UAS provide radio communication function and
Service on net；Described positioning unit is joined directly together with flight control units, realizes unmanned plane location navigation；Described driving list
Member is joined directly together with flight control units；Described mechanical structure unit is connected with driver element, and is equipped on a whole set of unmanned plane
System, realize unmanned plane operating flight；Described perception unit is joined directly together with microcomputer unit, installed in unmanned plane week
Side；Described electric power detection unit connection power supply and flight control units, send electric quantity data to flight control units in time；
Described power supply is directly powered to a whole set of UAS, is positioned over fuselage.
Above-mentioned wireless communication unit mainly includes 3G/4G wireless Internet cards and WIFI wireless network cards, is interconnected for realizing
Net service and access to wireless communication network.
Above-mentioned flight control units include carrying the flight control of the sensors such as barometer, accelerometer and gyroscope
Plate；Flight control panel can utilize the numerical value for obtaining current flight state lower plate set sensor, such as acceleration, height, carry out
Bicyclic PID control, maintain UAS flight stability.
Above-mentioned positioning unit includes M8N-GPS modules and compass, is used not only for realizing Beidou navigation simultaneously, GPS
Navigation and GLONASS navigation, moreover it is possible to obtain the current course of unmanned plane.Positioning unit can be implemented as UAS and provide essence
Accurate positioning, earth station is helped to obtain UAS current location in time, moreover it is possible to help UAS according to current course
Deviation adjusts course in time.
Above-mentioned driver element mainly includes brushless electric machine and electricity is adjusted, and controls driver element by flight control units, is used for
Drive mechanism unit is so as to realizing that unmanned plane operates in the air.
Above-mentioned mechanical structure unit is connected with driver element, mainly includes the members such as unmanned plane frame, chassis, propeller
Part.Wherein frame also includes horn, fuselage etc..
Above-mentioned perception unit includes ultrasonic wave module, temperature sensor, humidity sensor, PM2.5 sensors etc., is used for
The parameters of external environment are obtained, realize the real-time monitoring to external environment condition.Wherein ultrasonic wave module can be realized to nobody
The judgement of machine flight system peripheral obstacle, help the timely obstacle avoidance of unmanned plane.
Above-mentioned microcomputer unit waits the packet that satellite receiver is sent, after obtaining next step flight orders,
Flight control command is sent to flight control units, control unmanned plane establishes new aerial mission and completes flight attitude.Meanwhile
Microcomputer unit is used to obtain the value for perceiving unit all the sensors, while total data is updated into server in real time.
Above-mentioned electric power detection unit includes voltage-current sensor, for realizing the reality to unmanned plane during flying system charge
When detect.
Above-mentioned power supply is used to be powered a whole set of UAS.
Above-mentioned earth station includes ground monitoring system and data communication system, for monitoring unmanned plane, is sent out to unmanned plane
Lose one's life and make and receive the data message that unmanned plane is passed back.
In the present embodiment, the implementation method of above-mentioned multiple no-manned plane communication control system is as follows：
Often set UAS possesses unique ID number.The server registers that unmanned plane needs ground station to dispose before take-off should
Group number, ID number, IP address, geography information and the last time renewal time of UAS.Earth station will establish and safeguard
Close the tables of data of group number, ID number, IP address, geography information and last time renewal time index.Group number is realized to unmanned plane
Packet numbering, ID number realize the uniquely tagged to UAS, and IP address, which is used to realize, to communicate, and geography information is used for earth station
Acquisition is currently at the geographical position in the unmanned aerial vehicle group under state of flight residing for every frame unmanned plane, and last time renewal time is used
In judging whether unmanned plane fails to realize that tables of data updates at the appointed time, that is, it is used to identifying the logical of the unmanned plane and earth station
Interrogate failure or interruption.
After all unmanned planes take off, such as Fig. 2, above- mentioned information is sent to by earth station by wireless communication unit timing and taken
Business device, earth station's end server end automatically update other data item letter of corresponding unmanned plane ID number in earth station's end data table
Breath, including IP address, geography information and last time renewal time, the tables of data contain all be currently under state of flight
UAS above-mentioned details.
The ground monitoring system of earth station monitors the details of unmanned aerial vehicle group by reading the information of the tables of data in real time
Whether and identifying currently has UAS to be in communicating interrupt or malfunction.
Earth station sends the packet comprising ID number and order control information to unmanned generator terminal by data communication system
Wireless communication unit realizes the control to single unmanned plane.After the unmanned plane ID number of packet is received with the decoded packet data
The ID number arrived is consistent, then performs；Otherwise do not perform.Such as Fig. 3, earth station can also be by sending comprising group number and order control letter
The packet of breath realizes the packet control to unmanned plane.When receiving the unmanned plane group number of packet with being obtained after the decoded packet data
Group number it is consistent, then perform the order and forward the packet to other UASs；Otherwise only forwarding packet, is not performed
The order.
Above-described embodiment is the preferable embodiment of the utility model, but embodiment of the present utility model is not by above-mentioned
The limitation of embodiment, it is other it is any without departing from Spirit Essence of the present utility model with made under principle change, modify, replace
Generation, combination, simplify, should be equivalent substitute mode, be included within the scope of protection of the utility model.
Claims (6)
1. a kind of multiple no-manned plane communication control system, it is characterised in that including earth station and more set UASs, the ground
Stand including ground monitoring system and data communication system, for monitoring UAS, send order to UAS and connect
Receive the data message that UAS is passed back；Wherein often covering UAS includes being used for the radio communication list for realizing function of surfing the Net
Member, microcomputer unit, the flight control units for controlling unmanned plane during flying posture, for realizing global positioning navigation
Positioning unit, driving unmanned plane operating driver element, the mechanical structure unit for unmanned plane normal flight, for perceiving week
Perception unit, electric power detection unit and the power supply in collarette border；Described wireless communication unit is connected with microcomputer unit,
Radio communication function and service on net are provided for UAS；Described positioning unit is joined directly together with flight control units,
Realize unmanned plane location navigation；Described driver element is joined directly together with flight control units；Described mechanical structure unit with
Driver element is connected, and is equipped on a whole set of UAS, realizes unmanned plane operating flight；Described perception unit and microcomputer
Calculation machine unit is joined directly together, installed in UAS periphery；Described electric power detection unit connection power supply and flight control is single
Member, send electric quantity data to flight control units in time；Described power supply is directly powered to a whole set of UAS.
2. multiple no-manned plane communication control system according to claim 1, it is characterised in that the wireless communication unit uses
3G/4G wireless Internet cards and WIFI wireless network cards carry out radio communication.
3. multiple no-manned plane communication control system according to claim 1, it is characterised in that the flight control units are bag
The flight control panel for carrying barometer, accelerometer and gyro sensor is included, the flight control panel, which can utilize to obtain, works as
The numerical value of preceding state of flight lower plate set sensor.
4. multiple no-manned plane communication control system according to claim 1, it is characterised in that the positioning unit includes M8N-
GPS module and compass, realize the positioning to UAS.
5. multiple no-manned plane communication control system according to claim 1, it is characterised in that the driver element includes brushless
Motor and electricity are adjusted, and driver element is controlled by flight control units, for drive mechanism unit so as to realizing that unmanned plane is aerial
Flight.
6. multiple no-manned plane communication control system according to claim 1, it is characterised in that the perception unit includes ultrasound
Ripple module, temperature sensor, humidity sensor and PM2.5 sensors, for obtaining the ultrasonic wave of external environment, temperature, wet
Degree and PM2.5 parameters, realize the real-time monitoring to external environment condition.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201720465393.2U CN206741310U (en) | 2017-04-28 | 2017-04-28 | Multiple no-manned plane communication control system |
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| CN201720465393.2U CN206741310U (en) | 2017-04-28 | 2017-04-28 | Multiple no-manned plane communication control system |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106970650A (en) * | 2017-04-28 | 2017-07-21 | 暨南大学 | Multiple no-manned plane communication control system and control method |
| CN108255195A (en) * | 2018-01-19 | 2018-07-06 | 启迪国信科技有限公司 | Unmanned plane and UAV system |
| CN109814597A (en) * | 2019-02-03 | 2019-05-28 | 唐山坤翼创新科技有限公司 | The control method of concentrating type plant protection drone control system |
| CN111724631A (en) * | 2020-05-29 | 2020-09-29 | 北京三快在线科技有限公司 | Unmanned aerial vehicle service management system, method, readable storage medium and electronic device |
| CN111866052A (en) * | 2019-04-28 | 2020-10-30 | 丰鸟航空科技有限公司 | Unmanned aerial vehicle data processing method, device, terminal and storage medium |
-
2017
- 2017-04-28 CN CN201720465393.2U patent/CN206741310U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106970650A (en) * | 2017-04-28 | 2017-07-21 | 暨南大学 | Multiple no-manned plane communication control system and control method |
| CN106970650B (en) * | 2017-04-28 | 2023-11-24 | 暨南大学 | Multi-unmanned aerial vehicle communication control system and control method |
| CN108255195A (en) * | 2018-01-19 | 2018-07-06 | 启迪国信科技有限公司 | Unmanned plane and UAV system |
| CN109814597A (en) * | 2019-02-03 | 2019-05-28 | 唐山坤翼创新科技有限公司 | The control method of concentrating type plant protection drone control system |
| CN111866052A (en) * | 2019-04-28 | 2020-10-30 | 丰鸟航空科技有限公司 | Unmanned aerial vehicle data processing method, device, terminal and storage medium |
| CN111866052B (en) * | 2019-04-28 | 2022-12-13 | 丰鸟航空科技有限公司 | Unmanned aerial vehicle data processing method, device, terminal and storage medium |
| CN111724631A (en) * | 2020-05-29 | 2020-09-29 | 北京三快在线科技有限公司 | Unmanned aerial vehicle service management system, method, readable storage medium and electronic device |
| CN111724631B (en) * | 2020-05-29 | 2021-09-24 | 北京三快在线科技有限公司 | Unmanned aerial vehicle service management system, method, readable storage medium and electronic device |
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