CN206618980U - Unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding - Google Patents
Unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding Download PDFInfo
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- CN206618980U CN206618980U CN201621301605.5U CN201621301605U CN206618980U CN 206618980 U CN206618980 U CN 206618980U CN 201621301605 U CN201621301605 U CN 201621301605U CN 206618980 U CN206618980 U CN 206618980U
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Abstract
Unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding disclosed in the utility model, including flight system, relay system, remote control and command centre；Flight system includes flight controller, power plant module, head, image capture module, navigation module and airborne communication system；Airborne communication system is by 2.4GHz receiving modules, 1.2GHz figures pass transmitter module and 900MHz digital transmission modules are constituted；Relay system is deployed in ground, and it passes sending module by 1.2GHz figures transmitting/receiving module, video laminating module, 900MHz digital transmission modules and 5.8GHz figure and constituted；Remote control includes communication module, display module, MCU, memory module and control module；Command centre includes 900MHz digital transmission modules, video laminating module, 1.2GHz figures transmitting/receiving module and command centre's giant-screen.The utility model carries out data processing and forwarding by being deployed in the relay system on ground, realizes the long term distance data communication of the equipment such as unmanned plane and command centre, remote control, alleviates the weight of unmanned plane.
Description
Technical field
The utility model is related in unmanned plane corollary equipment technical field, particularly a kind of unmanned plane based on ground forwarding
Short distance remote control telemetering system.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..
Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane is divided into reconnaissance plane and target drone.The people
With aspect, unmanned plane+sector application is that unmanned plane has really just been needed；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation,
Disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture wave
The application in unrestrained etc. field, has greatly expanded the purposes of unmanned plane in itself, developed country also actively extension sector application with
Develop unmanned air vehicle technique.
Civilian unmanned plane in weight by strictly limiting, but in order to ground carry out data interaction, traditional unmanned plane is not
Obtain and do not carry mass communication equipment and data processing equipment, cause its endurance to be restricted, fly hand and pass through no-manned machine distant control
Device short distance manipulates the flight of unmanned plane, and traditional unmanned plane is simultaneously unstable by airborne equipment and with remote control direct communication
Fixed, signal transmission is apart from short, and unmanned plane can not do long term distance flight, and which limits its application.
In view of this, the present inventor's especial manufacture go out it is a kind of realize that unmanned plane and ground carries out that long term distance interacts based on
Thus the unmanned plane short-distance and medium-distance remote control telemetering system of ground forwarding, this case produces.
Utility model content
The purpose of this utility model is unmanned plane short-distance and medium-distance remote control telemetering system of the offer based on ground forwarding, and it leads to
The relay system progress data processing and forwarding for being deployed in ground are crossed, the equipment such as unmanned plane and command centre, remote control are realized
Long term distance data communication, alleviates the weight of unmanned plane.
To achieve these goals, the technical solution of the utility model is as follows：
Unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding, including flight system, relay system, remote control
And command centre；
The flight system includes flight controller, power plant module, head, image capture module, navigation module and airborne
Communication system, wherein airborne communication system pass transmitter module by 2.4GHz receiving modules, 1.2GHz figures and 900MHz numbers pass mould
Block is constituted；Navigation module, flight controller, head, image capture module and 1.2GHz figures pass transmitter module and are sequentially connected, power
Module, 2.4GHz receiving modules and 900MHz digital transmission modules are connected with flight controller respectively；
The relay system is deployed in ground, and it is passed by 1.2GHz figures transmitting/receiving module, video laminating module, 900MHz numbers
Module and 5.8GHz figures pass sending module composition, wherein the 1.2GHz figures transmitting/receiving module and airborne communication system of relay system
1.2GHz figures pass transmitter module communication, the 900MHz numbers of the 900MHz digital transmission modules of relay system and airborne communication system pass mould
Block communicates, and video laminating module passes with 1.2GHz figures transmitting/receiving module, 900MHz digital transmission modules and 5.8GHz figure send mould respectively
Block is connected；
The remote control includes communication module, display module, MCU, memory module and control module；Wherein communication module by
5.8GHz figures transmitting/receiving module, 2.4GHz transport modules and signal gain module composition, display module optimize mould by video drive
Block, video playback module and systematic parameter display module composition, control module are instructed defeated by key command input module and remote sensing
Enter module composition；The 5.8GHz figures transmitting/receiving module passes sending module with the 5.8GHz figures of relay system and communicated, 5.8GHz figures
Transmitting/receiving module is also connected with the video drive optimization module and video playback module of display module；2.4GHz transport modules and machine
The 2.4GHz receiving modules communication of communication system is carried, and 2.4GHz transport modules, signal gain module and MCU are sequentially connected, and are
System parameter display module, memory module, key command input module and remote sensing instruction input module are connected with MCU respectively；It is described
A variety of self-defined flight models and parameter are stored in memory module；
The command centre includes 900MHz digital transmission modules, video laminating module, 1.2GHz figures transmitting/receiving module and commander
Center giant-screen, the 900MHz digital transmission modules, 1.2GHz figures transmitting/receiving module and command centre's giant-screen are folded with video respectively
Plus module is connected, the 900MHz digital transmission modules of command centre communicate with the 900MHz digital transmission modules of airborne communication system, 1.2GHz
Figure transmitting/receiving module passes transmitter module with the 1.2GHz figures of airborne communication system and communicated.
The flight system, remote control, relay system and command centre also include a power module, wherein relay system
Power module be power module of voltage regulation, the power module of flight system connects with other modules or controller of flight system respectively
Connect, the power module of remote control is connected with other modules in remote control respectively, power module of voltage regulation distinguishes its of relay system
He is connected module, and the power module of command centre is connected with other modules of command centre respectively.
The unmanned plane short-distance and medium-distance remote control telemetering system also includes the PC for being connected with 900MHz digital transmission modules, the PC
Communicated by 900MHz digital transmission modules with the 900MHz digital transmission modules of airborne communication system.
The video playback playing module uses 8 cun of liquid crystal display, and systematic parameter display module uses LCD screen.
The power module uses 2S lithium battery.
The navigation module is CNSS satellite navigation systems.
After adopting the above technical scheme, operation principle of the present utility model is as follows：
First, in remote control, the control module being made up of rocking bar instruction input module and key command input module is to single
Piece microcomputer（MCU）Electric signal is sent, and is carried out by signal gain module after signal amplification, 2.4GHz transmission is transferred to
Module, is then converted to electromagnetic wave signal long distance descriscent unmanned plane and sends corresponding parameter information,
In the flight system of unmanned plane, the 2.4GHz receiving modules of airborne communication system receive above-mentioned parameter information and come real
Existing corresponding unmanned plane during flying action, mainly flight controller receives the parameter, the navigation information control of navigation module
Brake force module carries out UAV Flight Control（Control direction, height etc.）, and control head and image capture module progress
IMAQ, and practical flight parameter is also sent to by flight controller by the 900MHz digital transmission modules of airborne communication system
Relay system and command centre, while image capture module collects image information from head, then pass transmitting mould by 1.2GHz figures
Block is sent to relay system and command centre；
Flight parameter and image are sent from flight system is specifically：The 1.2GHz figures of airborne communication system pass transmitter module hair
Go out video electromagnetic wave signal to be received by the 1.2GHz figure transmitting/receiving modules of relay system and command centre and be converted into video flowing letter
Number flow to video laminating module（OSD）In, the 900MHz digital transmission modules of airborne communication system send out navigation and data parameters
Electromagnetic wave signal is received by relay system and the 900MHz digital transmission modules of command centre and flowed in OSD, in relay system and commander
Vision signal is carried out in the OSD at center to be overlapped with unmanned plane during flying parameter, and data parameters are shown on the video images；
After relay system overlap-add procedure, its 5.8GHz figure transmission module is pushed, under the communication module of remote control
Received under 5.8GHz figure transmission modules, and be converted into video stream signal, flowed in video drive optimization module, optimize
Afterwards, video stream signal flows to video playback module and played out, and video playback playing module uses 8 cun of liquid crystal display；
The a variety of self-defined flight models and parameter of memory module storage, input electrical signal is carried out using key command input module,
MCU transfers self-defined flight model and parameter from memory module, and is shown in the LCD screen of systematic parameter display module；
Directly the video image with flight parameter is shown by command centre's giant-screen after command centre's overlap-add procedure
Show to come.
The utility model beneficial effect is：The data strengthened by relay system between ground remote control device and unmanned plane are handed over
Mutual edge distance, but OSD designs are also mitigated nobody by unmanned plane during flying apart from farther, more stablizing for signal transmission on ground
The weight of machine, reduces part and also make it that the electromagnetic compatibility inside unmanned plane is more preferably good, be also beneficial to the pure image to no data
Secondary forwarding is carried out, quickly unmanned plane during flying parameter and image information display can be come out, quickly obtained by command centre
Know unmanned plane during flying state, it, which is acted on, also resides in winged hand from remote control and command centre it can be seen that all flight is joined
Number, and the supplemental characteristic for carrying out the pure image of secondary forwarding carries out screening and set according to customer demand, is forwarded to client institute
The command centre specified, carries out the aerial real-time video monitoring that data were screened in viewing superposition.
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Brief description of the drawings
Fig. 1 is structured flowchart of the present utility model.
Label declaration book
Flight system 1, flight controller 11, power plant module 12, head 13, image capture module 14, navigation module 15, machine
Communication system 16 is carried, 2.4GHz receiving modules 161,1.2GHz figures pass transmitting mould 162,900MHz digital transmission modules 163, power module
17, relay system 2,1.2GHz figures transmitting/receiving module 21, video superposition mould 22,900MHz digital transmission modules 23,5.8GHz figures pass hair
Send module 24, power module of voltage regulation 25, remote control 3, communication module 31,5.8GHz figures transmitting/receiving module 311,2.4GHz transmission moulds
Block 312, signal gain module 313, display module 32, video drive optimization module 321, video playback module 322, systematic parameter
Display module 323, MCU33, memory module 34, control module 35, key command input module 351, remote sensing instruction input module
352, power module 36, command centre 4,900MHz digital transmission modules 41, video laminating module 42,1.2GHz figure transmitting/receiving modules
43, command centre's large-size screen monitors 44, power module 45, PC 5,900MHz digital transmission modules 51.
Embodiment
As shown in figure 1, the unmanned plane short-distance and medium-distance remote control based on ground forwarding that embodiment one of the present utility model is disclosed
Telemetry system, including flight system 1, relay system 2, remote control 3 and command centre 4；
Flight system 1 includes flight controller 11, power plant module 12, head 13, image capture module 14, navigation module 15
With airborne communication system 16, wherein airborne communication system 16 passes transmitter module 162 by 2.4GHz receiving modules 161,1.2GHz figures
And 900MHz digital transmission modules 163 are constituted；Navigation module 15, flight controller 11, head 13, the and of image capture module 14
1.2GHz figures pass transmitter module 162 and are sequentially connected, power plant module 12,2.4GHz receiving modules 161 and 900MHz digital transmission modules 163
It is connected respectively with flight controller 11；
Relay system 2 is deployed in ground, and it is by 1.2GHz figures transmitting/receiving module 21, video laminating module 22,900MHz numbers
Transmission module 23 and 5.8GHz figure pass sending module 24 constitute, wherein the 1.2GHz figures transmitting/receiving module 21 of relay system with it is airborne
The 1.2GHz figures of communication system pass transmitter module 162 and communicated, the 900MHz digital transmission modules 23 and airborne communication system of relay system
900MHz digital transmission modules 163 communicate, video laminating module 22 respectively with 1.2GHz figures transmitting/receiving module 21,900MHz numbers pass mould
Block 23 and 5.8GHz figures pass sending module 24 and connected；
Remote control includes communication module 31, display module 32, MCU33, memory module 34 and control module 35；Wherein communicate
Module 31 is made up of 5.8GHz figures transmitting/receiving module 311,2.4GHz transport modules 312 and signal gain module 313, display module
32 are made up of video drive optimization module 321, video playback module 322 and systematic parameter display module 323, control module 35 by
Key command input module 351 is constituted with remote sensing instruction input module 352；5.8GHz figures transmitting/receiving module 311 and relay system
5.8GHz figures pass sending module 24 and communicate, 5.8GHz figures transmitting/receiving module 311 also optimizes mould with the video drive of display module
Block 321 and video playback module connection 322；The 2.4GHz receiving modules 161 of 2.4GHz transport modules 312 and airborne communication system
Communicate, and 2.4GHz transport modules 312, signal gain module 313 and MCU33 are sequentially connected, systematic parameter display module 323,
Memory module 34, key command input module 351 and remote sensing instruction input module 352 are connected with MCU33 respectively；Memory module 34
On store a variety of self-defined flight models and parameter；
Command centre 4 includes 900MHz digital transmission modules 41, video laminating module 42,1.2GHz figures transmitting/receiving module 43 and referred to
Wave center giant-screen 44,900MHz digital transmission modules 41,1.2GHz figures transmitting/receiving module 43 and command centre's giant-screen 44 respectively with
Video laminating module 42 is connected, the 900MHz digital transmission modules 43 of command centre and the 900MHz digital transmission modules of airborne communication system
163 communications, 1.2GHz figures transmitting/receiving module 43 passes transmitter module 162 with the 1.2GHz figures of airborne communication system and communicated.
Flight system 1, remote control 3, relay system 2 and command centre 4 also include a power module, wherein relay system
Power module be power module of voltage regulation 25, other modules of power module of voltage regulation and relay system are connected respectively, flight system 1
Power module 17 be connected respectively with other modules or controller of flight system, the power module 36 of remote control respectively with remote control
Other modules connection in device, the power module 45 of command centre is connected with other modules of command centre respectively.
Unmanned plane short-distance and medium-distance remote control telemetering system also includes the PC 5 for being connected with 900MHz digital transmission modules 51, the PC 5
163 are communicated with the 900MHz digital transmission modules of airborne communication system 11 by 900MHz digital transmission modules 51, it is higher by the mobility
PC the planning director data in unmanned plane during flying path can be sent as flight system, and receive unmanned plane during flying parameter etc.
Data.
In the present embodiment, the video playback playing module 322 of remote control 3 is using 8 cun of liquid crystal display, systematic parameter display mould
Block 323 uses LCD screen.Above-mentioned each power module uses 2S lithium battery.
The navigation module used in flight system for CNSS satellite navigation systems, GNSS contain GPS, GLONASS,
Compass (Big Dipper), Galileo systems.
The operation principle of unmanned plane short-distance and medium-distance remote control telemetering system is as follows disclosed in the present embodiment：
First, in remote control 3, the control mould being made up of rocking bar instruction input module 352 and key command input module 351
Block 35 gives one chip microcomputer（MCU33）Electric signal is sent, and is carried out by signal gain module 313 after signal amplification, is passed
It is defeated to arrive 2.4GHz transport modules 312, it is then converted to electromagnetic wave signal long distance descriscent unmanned plane and sends corresponding parameter information,
In the flight system of unmanned plane, the 2.4GHz receiving modules 161 of airborne communication system receive above-mentioned parameter information
To realize corresponding unmanned plane during flying action, mainly flight controller 11 receives the parameter, and navigation module 15 is led
Information of navigating control power plant module 12 carries out UAV Flight Control（Control direction, height etc.）, and control head 13 and image
Acquisition module 14 carries out IMAQ, and practical flight parameter is also passed through airborne communication system 16 by flight controller 11
900MHz digital transmission modules 163 are sent to relay system 2 and command centre 4, while image capture module 14 is collected from head 13
Image information, then relay system 2 and command centre 4 are sent to by 1.2GHz figure biography transmitter modules 162；
Flight parameter and image are sent from flight system is specifically：The 1.2GHz figures of airborne communication system pass transmitter module
162, which send video electromagnetic wave signal, is received and is turned by relay system 2 and the 1.2GHz figures transmitting/receiving module 21,43 of command centre 4
Turn to video stream signal and flow to video laminating module 22,43（OSD）In, the 900MHz digital transmission modules 163 of airborne communication system are sent out
The electromagnetic wave signal of navigation and data parameters is sent out by relay system and the 900MHz digital transmission modules 23 of command centre, 41 receiving streams
Into OSD, carry out vision signal in relay system and the OSD22 of command centre, 43 and unmanned plane during flying parameter be overlapped,
Data parameters are shown on the video images；
After the overlap-add procedure of relay system 2, its 5.8GHz figures transmission module 24 is pushed, under the communication module of remote control 3
5.8GHz figures transmission module received for 311 times, and be converted into video stream signal, flow in video drive optimization module 322, enter
After row optimization, video stream signal flows to video playback module 321 and played out, and video playback playing module 321 uses 8 cun
Liquid crystal display；The a variety of self-defined flight models and parameter stored in memory module 34, enter using key command input module
Row input electrical signal, MCU33 transfers self-defined flight model and parameter from memory module 34, and is shown in systematic parameter display mould
In the LCD screen of block 323；
Directly by command centre's giant-screen 44 by the video image with flight parameter after the overlap-add procedure of command centre 4
Show.
Specific embodiment of the utility model is these are only, not to the restriction of protection domain of the present utility model.
The equivalent variations that all mentalities of designing according to this case are done, each fall within the protection domain of this case.
Claims (6)
1. the unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding, it is characterised in that：Including flight system, relaying system
System, remote control and command centre；
The flight system includes flight controller, power plant module, head, image capture module, navigation module and airborne communication
System, wherein airborne communication system pass transmitter module and 900MHz digital transmission module groups by 2.4GHz receiving modules, 1.2GHz figures
Into；Navigation module, flight controller, head, image capture module and 1.2GHz figures pass transmitter module and are sequentially connected, power mould
Block, 2.4GHz receiving modules and 900MHz digital transmission modules are connected with flight controller respectively；
The relay system is deployed in ground, and it is by 1.2GHz figures transmitting/receiving module, video laminating module, 900MHz digital transmission modules
And 5.8GHz figures pass sending module composition, wherein the 1.2GHz figures transmitting/receiving module of relay system and airborne communication system
1.2GHz figures pass transmitter module communication, the 900MHz digital transmission modules of relay system and the 900MHz digital transmission modules of airborne communication system
Communication, video laminating module passes sending module with 1.2GHz figures transmitting/receiving module, 900MHz digital transmission modules and 5.8GHz figure respectively
Connection；
The remote control includes communication module, display module, MCU, memory module and control module；Wherein communication module by
5.8GHz figures transmitting/receiving module, 2.4GHz transport modules and signal gain module composition, display module optimize mould by video drive
Block, video playback module and systematic parameter display module composition, control module are instructed defeated by key command input module and remote sensing
Enter module composition；The 5.8GHz figures transmitting/receiving module passes sending module with the 5.8GHz figures of relay system and communicated, 5.8GHz figures
Transmitting/receiving module is also connected with the video drive optimization module and video playback module of display module；2.4GHz transport modules and machine
The 2.4GHz receiving modules communication of communication system is carried, and 2.4GHz transport modules, signal gain module and MCU are sequentially connected, and are
System parameter display module, memory module, key command input module and remote sensing instruction input module are connected with MCU respectively；It is described
A variety of self-defined flight models and parameter are stored in memory module；
The command centre includes 900MHz digital transmission modules, video laminating module, 1.2GHz figures transmitting/receiving module and command centre
Giant-screen, the 900MHz digital transmission modules, 1.2GHz figures transmitting/receiving module and command centre's giant-screen respectively with video superposition mould
Block is connected, and the 900MHz digital transmission modules of command centre communicate with the 900MHz digital transmission modules of airborne communication system, and 1.2GHz figures are passed
Receiving module passes transmitter module with the 1.2GHz figures of airborne communication system and communicated.
2. the unmanned plane short-distance and medium-distance remote control telemetering system as claimed in claim 1 based on ground forwarding, it is characterised in that：Institute
Stating flight system, remote control, relay system and command centre also includes the power module of a power module, wherein relay system
For power module of voltage regulation, the power module of flight system respectively with the flight controller of flight system, power plant module, head, figure
As acquisition module, navigation module, airborne communication system connection, the power module of remote control respectively with the communication mould in remote control
Block, display module, MCU, memory module and control module connection, the 1.2GHz figure biographies of power module of voltage regulation relay system respectively connect
Receive module, video laminating module, 900MHz digital transmission modules and 5.8GHz figures and pass sending module connection, the power supply mould of command centre
Block is big with the 900MHz digital transmission modules of command centre, video laminating module, 1.2GHz figures transmitting/receiving module and command centre respectively
Screen is connected.
3. the unmanned plane short-distance and medium-distance remote control telemetering system as claimed in claim 2 based on ground forwarding, it is characterised in that：Institute
State the lithium battery that power module uses 2S.
4. the unmanned plane short-distance and medium-distance remote control telemetering system as claimed in claim 1 based on ground forwarding, it is characterised in that：Institute
The PC that unmanned plane short-distance and medium-distance remote control telemetering system also includes being connected with 900MHz digital transmission modules is stated, the PC passes through 900MHz
Digital transmission module communicates with the 900MHz digital transmission modules of airborne communication system.
5. the unmanned plane short-distance and medium-distance remote control telemetering system as claimed in claim 1 based on ground forwarding, it is characterised in that：Institute
The liquid crystal display that video playback playing module uses 8 cun is stated, systematic parameter display module uses LCD screen.
6. the unmanned plane short-distance and medium-distance remote control telemetering system as claimed in claim 1 based on ground forwarding, it is characterised in that：Institute
Navigation module is stated for CNSS satellite navigation systems.
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| CN201621301605.5U CN206618980U (en) | 2016-11-30 | 2016-11-30 | Unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding |
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| CN201621301605.5U CN206618980U (en) | 2016-11-30 | 2016-11-30 | Unmanned plane short-distance and medium-distance remote control telemetering system based on ground forwarding |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106444555A (en) * | 2016-11-30 | 2017-02-22 | 厦门汉航精密科技有限公司 | Ground forwarding-based unmanned aerial vehicle medium-short distance remote control and remote measuring system |
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2016
- 2016-11-30 CN CN201621301605.5U patent/CN206618980U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106444555A (en) * | 2016-11-30 | 2017-02-22 | 厦门汉航精密科技有限公司 | Ground forwarding-based unmanned aerial vehicle medium-short distance remote control and remote measuring system |
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