CN108877299A - Multiple no-manned plane terminal airspace management-control method, system and device - Google Patents
Multiple no-manned plane terminal airspace management-control method, system and device Download PDFInfo
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- CN108877299A CN108877299A CN201810993698.XA CN201810993698A CN108877299A CN 108877299 A CN108877299 A CN 108877299A CN 201810993698 A CN201810993698 A CN 201810993698A CN 108877299 A CN108877299 A CN 108877299A
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0047—Navigation or guidance aids for a single aircraft
- G08G5/0069—Navigation or guidance aids for a single aircraft specially adapted for an unmanned aircraft
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Abstract
The invention discloses multiple no-manned plane terminal airspace management-control methods, system and device, belong to unmanned plane terminal airspace control technical field, multiple no-manned plane terminal airspace management-control method, system and device, including control device and managing and control system, control device includes the on-board data box managing patrol aviation device and being mounted on unmanned plane, satellite positioning module is mounted in unmanned plane and on-board data box, flight control modules and safety control module, managing and control system includes ground telemetering and letter biography system, unmanned aerial vehicle onboard telemetering and letter biography system, defence type detecting and early warning system and black winged aircraft interference system, it may be implemented reasonably to manage unmanned plane using dual system, versatility is high, can significant increase multiple no-manned plane airport security and stability；It is gone on patrol outside clearance zone using multiple control patrol aviation devices on duty, can prevent black winged situation from upsetting the normal order on multiple no-manned plane airport, meanwhile, greatly improve the processing speed to emergency case.
Description
Technical field
The present invention relates to unmanned plane terminal airspaces to manage technical field, more specifically to multiple no-manned plane terminal airspace
Management-control method, system and device.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer, unmanned plane
By application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+
Industrial application is that unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief,
Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Application, greatly expanded the purposes of unmanned plane itself, developed country also in actively extension industrial application and develops unmanned plane
Technology.
Since unmanned plane and common aircraft have biggish difference, in the control of multiple no-manned plane terminal airspace with
Can also there be biggish difference on existing airport, and universal and quantity recently as unmanned plane is increased, many personal and single
Position is owned by unmanned plane, especially personal small drone, often there is black winged phenomenon, that is, without relevant departments
Approval unmanned plane near airports fly, the normal takeoff and landing order on airport can be seriously affected, in addition, unmanned plane due to
There is no the operation of pilot and judgement, the requirement degree to ground wireless control system is higher, when a failure occurs, it is easy to go out
The case where existing airport paralysis, it will cause large effect.
Summary of the invention
1. technical problems to be solved
Aiming at the problems existing in the prior art, the purpose of the present invention is to provide multiple no-manned plane terminal airspace management-control method, be
System and device, it may be implemented reasonably to manage unmanned plane using dual system, can be realized by installing airborne data box additional,
Versatility is high, can significant increase multiple no-manned plane airport security and stability；Using multiple control patrol aviation devices outside clearance zone
It goes on patrol on duty, can prevent black winged situation from upsetting the normal order on multiple no-manned plane airport, meanwhile, it greatly improves to emergency case
Processing speed.
2. technical solution
To solve the above problems, the present invention adopts the following technical scheme that.
Multiple no-manned plane terminal airspace managing and control system and device, including control device and managing and control system, the control device packet
The on-board data box managing patrol aviation device and being mounted on unmanned plane is included, is mounted in the unmanned plane and on-board data box
Satellite positioning module, flight control modules and safety control module, the managing and control system include ground telemetering and letter biography system, nothing
Man-machine Airborne Telemetry and letter biography system, defence type detecting and early warning system and black winged aircraft interference system, the ground telemetering with
Letter biography system manages control tower with ground and the operation equal signal of remote control center is connect, the satellite positioning module, flight control modules
It passes system signal with letter with unmanned aerial vehicle onboard telemetering with safety control module to connect, the ground telemetering and letter biography system and nothing
Man-machine Airborne Telemetry passes system signal with letter and connect, the control patrol aviation device and ground telemetering and letter biography system and unmanned plane
Airborne Telemetry is connect with the letter equal signal of biography system, and the ground telemetering and letter biography system and control patrol aviation device include defence
Formula detecting and early warning system and black winged aircraft interference system, it may be implemented reasonably to manage unmanned plane using dual system
Control can realize that versatility is high by installing airborne data box additional, can significant increase multiple no-manned plane airport security and stability；Using
Multiple control patrol aviation devices go on patrol on duty outside clearance zone, can prevent black winged situation from upsetting the normal order on multiple no-manned plane airport
Sequence, meanwhile, greatly improve the processing speed to emergency case.
Further, the ground telemetering and letter biography system and unmanned aerial vehicle onboard telemetering and letter biography system and control patrol fly
It is two-way encrypted data transmission between row device, the control patrol aviation device and on-board data and unmanned aerial vehicle onboard telemetering and letter
It is two-way encrypted data transmission between biography system, safety can be improved.
Further, the control patrol aviation device includes four rotor aircraft shells, is consolidated on the four rotor aircrafts shell
Fixed connection is fixedly connected on the four rotor aircrafts shell and is matched with main flying wing there are four equally distributed main flying wing
Protecting frame, protecting frame has protective action to main flying wing, and the lower end of the four rotor aircrafts shell is fixedly connected with multiple drops
Bracket is fallen, the lower end of the alighting carriage is fixedly connected with resilient cushion, and resilient cushion can reduce vibration when landing, and four wing flies
The downside of row device shell is equipped with high-definition camera, is connected with holder, cloud between the high-definition camera and four rotor aircraft shells
Platform can make high-definition camera be not susceptible to shake, and be easy to improve the quality of acquisition image, the lower end of the four rotor aircrafts shell
It is fixedly connected with multiple equally distributed device sets columns.
Further, the control patrol aviation device is waterproof construction, is connected with secondary flying wing on described device collection zygostyle
When encountering rainy equal weather, managing will not intake in patrol aviation device, when control patrol aviation device compels to be down in water, pass through
Controlling secondary flying wing can be such that control patrol aviation device exercises on the water surface, take convenient for recycling.
Further, it is fixedly connected on the four rotor aircrafts shell there are four equally distributed air bag, and safe
Air bag is located between two adjacent protecting frames, and air bag, protection four wings flight can be triggered when encountering hard hit
Device shell is not damaged.
Further, the side of the on-board data box is equipped with connector, connects between the on-board data box and connector
It is connected to connecting line, the power output end connection of the connecting line and unmanned plane can connect the power supply of on-board data box and unmanned plane
It connects, versatility is stronger.
Further, multiple control patrol aviation device flight positions are respectively positioned on outside clearance zone, will not influence normal nothing
Man-machine takeoff and landing.
Further, the defence type detecting and early warning system include aircraft figure pass and remote signal receiver, it is described black
Flying aircraft interference system includes electromagnetic interference emission device.
Further, the figure on the control patrol aviation device passes equal with remote signal receiver and electromagnetic interference emission device
In device sets column, convenient for emitting and receiving signal.
Multiple no-manned plane terminal airspace managing and control system and device, it is characterised in that：Its management-control method is：
One, unmanned plane carries out signal connection by unmanned aerial vehicle onboard telemetering and letter biography system and ground telemetering and letter biography system, by
Staff manages the state of flight of unmanned plane in ground control control tower, and is carried out by operation remote control center to unmanned plane
It controls and operates, wherein satellite positioning module can determine position and the height of unmanned plane, and flight control modules can control unmanned plane
Navigation, safety control module can prevent that unmanned plane from colliding or the generation of other fortuitous events, this management-control method are equal
For the prior art；
Two, airborne data box is installed on unmanned plane（11）, on-board data box（11）It can be used as the Beck-up Control System of unmanned plane,
When the control system failure that unmanned plane carries, on-board data box（11）It can play a role automatically, meanwhile, on-board data box（11）
The flying quality of unmanned plane can be stored into cloud server in real time, make on-board data box（11）Play the function of cloud black box
Can, after generation accident, it not will cause the loss of flying quality；
Three, position of multiple control patrol aviation devices outside clearance zone close to airport is uniformly flown, defence type detecting and early warning system
The position of unmanned plane can be determined by receiving unmanned plane figure biography and remote signal, when received signal belongs to the unmanned plane in control
When, black winged aircraft interference system will not be triggered, when received signal is unknown signaling, and the normal of unmanned plane is will affect and flies
When row, it can be defaulted as black winged aircraft, the black winged aircraft lift-off such as do not need, after black winged aircraft booting in the short time
It was found that and be accurately positioned, while black winged aircraft interference system can be triggered, black winged aircraft interference system can pass through electromagnetic interference
Transmitter carries out accurate electromagnetic interference, adjust automatically electricity according to information such as working frequency, the directions of the black winged aircraft detected
Magnetic disturbance frequency and direction realize that black winged aircraft expelling and force-landing in prevention and control region；Ground telemetering and letter biography system can be
This function is played in approach area, will not influence normal unmanned plane during flying；
Four, when ground telemetering and letter pass system jam, control patrol aviation device can play temporary control function, temporarily
Safeguard the order on unmanned plane airport；
Five, it manages on patrol aviation device and high-definition camera is installed（6）, can be by the picture of shooting or realtime video transmission to cloud
Server, ground control control tower and operation remote control center, convenient for handling emergency in time or being supervised to airport surrounding enviroment
It surveys.
3. beneficial effect
Compared with the prior art, the advantage of the invention is that：
（1）This programme may be implemented reasonably to manage unmanned plane using dual system, can be real by installing airborne data box additional
Existing, versatility is high, can significant increase multiple no-manned plane airport security and stability；Using multiple control patrol aviation devices in clearance zone
Outer patrol is on duty, can prevent black winged situation from upsetting the normal order on multiple no-manned plane airport, meanwhile, it greatly improves to emergency case
Processing speed.
（2）Between ground telemetering and letter biography system and unmanned aerial vehicle onboard telemetering and letter biography system and control patrol aviation device
For two-way encrypted data transmission, it is double for managing between patrol aviation device and on-board data and unmanned aerial vehicle onboard telemetering and letter biography system
To encrypted data transmission, safety can be improved.
（3）Managing patrol aviation device includes four rotor aircraft shells, is fixedly connected with that there are four on four rotor aircraft shells
The main flying wing of even distribution is fixedly connected with the protecting frame to match with main flying wing, protecting frame pair on four rotor aircraft shells
Main flying wing has protective action, and the lower end of four rotor aircraft shells is fixedly connected with multiple alighting carriages, the lower end of alighting carriage
It is fixedly connected with resilient cushion, resilient cushion can reduce vibration when landing, and the downside of four rotor aircraft shells is equipped with high-definition camera,
Holder is connected between high-definition camera and four rotor aircraft shells, holder can make high-definition camera be not susceptible to shake, be easy to
The quality of acquisition image is improved, the lower end of four rotor aircraft shells is fixedly connected with multiple equally distributed device sets columns.
（4）Control patrol aviation device is waterproof construction, and secondary flying wing is connected on device sets column ought encounter rain equal days
When gas, managing will not intake in patrol aviation device, can by controlling secondary flying wing when control patrol aviation device compels to be down in water
It exercises control patrol aviation device on the water surface, takes convenient for recycling.
（5）Equally distributed air bag there are four being fixedly connected on four rotor aircraft shells, and air bag distinguishes position
Between two adjacent protecting frames, air bag can be triggered when encountering hard hit, four rotor aircraft shells of protection not by
Damage.
（6）The side of on-board data box is equipped with connector, and connecting line is connected between on-board data box and connector, connects
The connection of the power output end of line and unmanned plane, can connect the power supply of on-board data box and unmanned plane, versatility is stronger.
（7）Multiple control patrol aviation device flight positions are respectively positioned on outside clearance zone, will not influence taking off for normal unmanned plane
And landing.
（8）Defence type detecting and early warning system includes aircraft figure biography and remote signal receiver, black winged aircraft interference system
System includes electromagnetic interference emission device.
（9）Figure on control patrol aviation device, which is passed, is respectively positioned on device collection with remote signal receiver and electromagnetic interference emission device
In zygostyle, convenient for emitting and receiving signal.
Detailed description of the invention
Fig. 1 is the bottom substance schematic diagram of control patrol aviation device of the invention；
Fig. 2 is the superstructure schematic diagram of control patrol aviation device of the invention；
Fig. 3 is that data of the invention transmit box structure schematic diagram；
Fig. 4 is that data of the invention transmit box mounted configuration schematic diagram；
Fig. 5 is unmanned plane approach area structure top view of the invention；
Fig. 6 is sectional view at A-A in Fig. 5；
Fig. 7 is sectional view at B-B in Fig. 5；
Fig. 8 is systematic schematic diagram of the invention.
Figure label explanation：
1 four rotor aircraft shells, 2 main flying wings, 3 protecting frames, 4 alighting carriages, 5 resilient cushions, 6 high-definition cameras, 7 substitutes
Capsule, 8 device sets columns, 9 secondary flying wings, 10 holders, 11 on-board data boxes, 12 connectors, 13 connecting lines.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention；Technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description；Obviously；Described embodiments are only a part of the embodiments of the present invention；Instead of all the embodiments, it is based on
Embodiment in the present invention；It is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment；It shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the instruction such as term " on ", "lower", "inner", "outside" " top/bottom end "
Orientation or positional relationship be based on the orientation or positional relationship shown in the drawings, be merely for convenience of description the present invention and simplification retouch
It states, rather than the device or element of indication or suggestion meaning must have a particular orientation, be constructed and operated in a specific orientation,
Therefore it is not considered as limiting the invention.In addition, term " first ", " second " are used for description purposes only, and cannot understand
For indication or suggestion relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation " " is set
Be equipped with ", " be arranged/connect ", " connection " etc., shall be understood in a broad sense, such as " connection ", may be a fixed connection, be also possible to removable
Connection is unloaded, or is integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, it can also be in
Between medium be indirectly connected, can be the connection inside two elements.It for the ordinary skill in the art, can be specific
Situation understands the concrete meaning of above-mentioned term in the present invention.
Embodiment 1：
Fig. 3-4, multiple no-manned plane terminal airspace management-control method, system and device, including control device and managing and control system are please referred to, is managed
Control device includes the on-board data box 11 managing patrol aviation device and being mounted on unmanned plane, and the side of on-board data box 11 is equipped with
Connector 12 is connected with connecting line 13, the power supply output of connecting line 13 and unmanned plane between on-board data box 11 and connector 12
On-board data box 11, can connect by end connection with the power supply of unmanned plane, and versatility is stronger,
Referring to Fig. 8, being mounted on satellite positioning module, flight control modules and safety control in unmanned plane and on-board data box 11
Molding block, managing and control system include ground telemetering and letter biography system, unmanned aerial vehicle onboard telemetering and letter biography system, defence type detecting and early warning
System and black winged aircraft interference system, ground telemetering and letter biography system and ground control control tower and the operation equal signal of remote control center
Connection, satellite positioning module, flight control modules and safety control module pass system signal with unmanned aerial vehicle onboard telemetering and letter
Connection, ground telemetering pass system signal with letter with unmanned aerial vehicle onboard telemetering with letter biography system and connect, control patrol aviation device and ground
Face telemetering is connect with letter biography system and unmanned aerial vehicle onboard telemetering with the letter equal signal of biography system, ground telemetering and letter biography system and control
Patrol aviation device includes defence type detecting and early warning system and black winged aircraft interference system, and defence type detecting and early warning system includes
Aircraft figure passes and remote signal receiver, and black winged aircraft interference system includes electromagnetic interference emission device, ground telemetering and letter
It is two-way encrypted data transmission between biography system and unmanned aerial vehicle onboard telemetering and letter biography system and control patrol aviation device, control
It is two-way encrypted data transmission between patrol aviation device and on-board data and unmanned aerial vehicle onboard telemetering and letter biography system, peace can be improved
Quan Xing.
Control patrol aviation device includes four rotor aircraft shells 1, fixed company on four rotor aircraft shells 1 referring to FIG. 1-2,
It connects there are four equally distributed main flying wing 2, is fixedly connected with the guarantor to match with main flying wing 2 on four rotor aircraft shells 1
Frame 3 is protected, 3 pairs of protecting frame main flying wings 2 have protective action, and the lower end of four rotor aircraft shells 1 is fixedly connected with multiple landing branch
Frame 4, the lower end of alighting carriage 4 are fixedly connected with resilient cushion 5, and resilient cushion 5 can reduce vibration when landing, four rotor aircraft shells
1 downside is equipped with high-definition camera 6, holder 10 is connected between high-definition camera 6 and four rotor aircraft shells 1, holder 10 can
Make high-definition camera 6 be not susceptible to shake, be easy to improve the quality of acquisition image, the lower end of four rotor aircraft shells 1 is fixed to be connected
Multiple equally distributed device sets columns 8 are connected to, the figure biography and remote signal receiver and electromagnetism managed on patrol aviation device are done
It disturbs transmitter to be respectively positioned in device sets column 8, convenient for emitting and receiving signal, control patrol aviation device is waterproof construction, device
Secondary flying wing 9 is connected on collection zygostyle 8 when encountering rainy equal weather, managing will not intake in patrol aviation device, when control is patrolled
When patrolling aircraft and compeling to be down in water, it can make to manage patrol aviation device by controlling secondary flying wing 9 and be exercised on the water surface, convenient for recycling
It takes, is fixedly connected on four rotor aircraft shells 1 there are four equally distributed air bag 7, and air bag 7 is located at two
Between a adjacent protecting frame 3, air bag 7 can be triggered when encountering hard hit, four rotor aircraft shells 1 of protection are not damaged
It is bad.
Please refer to Fig. 5-7, multiple control patrol aviation device flight positions are respectively positioned on outside clearance zone, will not influence it is normal nobody
The takeoff and landing of machine.
Unmanned plane carries out signal connection by unmanned aerial vehicle onboard telemetering and letter biography system and ground telemetering and letter biography system, by
Staff manages the state of flight of unmanned plane in ground control control tower, and is carried out by operation remote control center to unmanned plane
It controls and operates, wherein satellite positioning module can determine position and the height of unmanned plane, and flight control modules can control unmanned plane
Navigation, safety control module can prevent that unmanned plane from colliding or the generation of other fortuitous events, this management-control method are equal
It is similar with civil aviation control technology for the prior art, it can be realized by those skilled in the art.
Airborne data box 11 is installed on unmanned plane, on-board data box 11 can be used as the Beck-up Control System of unmanned plane, when
When the included control system of unmanned plane fails, on-board data box 11 can play a role automatically, meanwhile, on-board data box 11 can be by nothing
Man-machine flying quality is stored into cloud server in real time, and on-board data box 11 is made to play the function of cloud black box, and thing occurs
After therefore, the loss of flying quality not will cause.
Position of multiple control patrol aviation devices outside clearance zone close to airport is uniformly flown, defence type detecting and early warning system
The position of unmanned plane can be determined by receiving unmanned plane figure biography and remote signal, when received signal belongs to the unmanned plane in control
When, black winged aircraft interference system will not be triggered, when received signal is unknown signaling, and the normal of unmanned plane is will affect and flies
When row, it can be defaulted as black winged aircraft, the black winged aircraft lift-off such as do not need, after black winged aircraft booting in the short time
It was found that and be accurately positioned, while black winged aircraft interference system can be triggered, black winged aircraft interference system can pass through electromagnetic interference
Transmitter carries out accurate electromagnetic interference, adjust automatically electricity according to information such as working frequency, the directions of the black winged aircraft detected
Magnetic disturbance frequency and direction realize that black winged aircraft expelling and force-landing in prevention and control region；Ground telemetering and letter biography system can be
This function is played in approach area, will not influence normal unmanned plane during flying.
When ground telemetering and letter pass system jam, control patrol aviation device can play temporary control function, temporarily
When safeguard unmanned plane airport order.
High-definition camera 6 is installed on control patrol aviation device, it can be by the picture of shooting or realtime video transmission to cloud
Server, ground control control tower and operation remote control center, convenient for handling emergency in time or being supervised to airport surrounding enviroment
It surveys.
This programme may be implemented reasonably to manage unmanned plane using dual system, can be real by installing airborne data box additional
Existing, versatility is high, can significant increase multiple no-manned plane airport security and stability；Using multiple control patrol aviation devices in clearance zone
Outer patrol is on duty, can prevent black winged situation from upsetting the normal order on multiple no-manned plane airport, meanwhile, it greatly improves to emergency case
Processing speed.
It is described above；It is merely preferred embodiments of the present invention；But scope of protection of the present invention is not limited thereto；
Anyone skilled in the art is in the technical scope disclosed by the present invention；According to the technique and scheme of the present invention and its
It improves design and is subject to equivalent substitution or change；It should be covered by the scope of protection of the present invention.
Claims (10)
1. multiple no-manned plane terminal airspace managing and control system and device, including control device and managing and control system, it is characterised in that：The pipe
Control device includes the on-board data box managing patrol aviation device and being mounted on unmanned plane（11）, the unmanned plane and on-board data
Box（11）It is inside mounted on satellite positioning module, flight control modules and safety control module, the managing and control system includes ground
Telemetering and letter biography system, unmanned aerial vehicle onboard telemetering and letter biography system, defence type detecting and early warning system and black winged aircraft interference are
System, the ground telemetering manages control tower with ground with letter biography system and the operation equal signal of remote control center is connect, the satellite positioning
Module, flight control modules and safety control module pass system signal with letter with unmanned aerial vehicle onboard telemetering and connect, the ground
Telemetering passes system signal with letter with unmanned aerial vehicle onboard telemetering with letter biography system and connect, the control patrol aviation device and ground telemetering
It is connect with letter biography system and unmanned aerial vehicle onboard telemetering with the letter equal signal of biography system, the ground telemetering is patrolled with letter biography system and control
Patrolling aircraft includes defence type detecting and early warning system and black winged aircraft interference system.
2. multiple no-manned plane terminal airspace managing and control system according to claim 1 and device, it is characterised in that：The ground is distant
Survey between letter biography system and unmanned aerial vehicle onboard telemetering and letter biography system and control patrol aviation device is that two-way encryption data passes
It is defeated, it is that two-way encryption data passes between the control patrol aviation device and on-board data and unmanned aerial vehicle onboard telemetering and letter biography system
It is defeated.
3. multiple no-manned plane terminal airspace managing and control system according to claim 1 and device, it is characterised in that：The control is patrolled
Patrolling aircraft includes four rotor aircraft shells（1）, the four rotor aircrafts shell（1）On be fixedly connected there are four equally distributed
Main flying wing（2）, the four rotor aircrafts shell（1）On be fixedly connected with and main flying wing（2）The protecting frame to match（3）,
The four rotor aircrafts shell（1）Lower end be fixedly connected with multiple alighting carriages（4）, the alighting carriage（4）Lower end it is solid
Surely it is connected with resilient cushion（5）, the four rotor aircrafts shell（1）Downside be equipped with high-definition camera（6）, the high-definition camera
（6）With four rotor aircraft shells（1）Between be connected with holder（10）, the four rotor aircrafts shell（1）Lower end be fixedly connected
There are multiple equally distributed device sets columns（8）.
4. multiple no-manned plane terminal airspace managing and control system according to claim 3 and device, it is characterised in that：The control is patrolled
Patrolling aircraft is waterproof construction, described device collection zygostyle（8）On be connected with secondary flying wing（9）.
5. multiple no-manned plane terminal airspace managing and control system according to claim 3 and device, it is characterised in that：Four wing flies
Row device shell（1）On be fixedly connected there are four equally distributed air bag（7）, and air bag（7）It is located at two phases
Adjacent protecting frame（3）Between.
6. multiple no-manned plane terminal airspace managing and control system according to claim 1 and device, it is characterised in that：The airborne number
According to box（11）Side be equipped with connector（12）, the on-board data box（11）With connector（12）Between be connected with connecting line
（13）, the connecting line（13）It is connect with the power output end of unmanned plane.
7. multiple no-manned plane terminal airspace managing and control system according to claim 1 and device, it is characterised in that：Multiple pipes
Control patrol aviation device flight position is respectively positioned on outside clearance zone.
8. multiple no-manned plane terminal airspace managing and control system according to claim 1 and device, it is characterised in that：The defence type
Detecting and early warning system includes aircraft figure biography and remote signal receiver, and the black winged aircraft interference system includes electromagnetic interference
Transmitter.
9. multiple no-manned plane terminal airspace managing and control system according to claim 1 or 3 and device, it is characterised in that：The pipe
Figure on control patrol aviation device, which is passed, is respectively positioned on device sets column with remote signal receiver and electromagnetic interference emission device（8）It is interior.
10. multiple no-manned plane terminal airspace managing and control system according to claim 1 and device, it is characterised in that：Its control side
Method is：
One, unmanned plane carries out signal connection by unmanned aerial vehicle onboard telemetering and letter biography system and ground telemetering and letter biography system, by
Staff manages the state of flight of unmanned plane in ground control control tower, and is carried out by operation remote control center to unmanned plane
It controls and operates, wherein satellite positioning module can determine position and the height of unmanned plane, and flight control modules can control unmanned plane
Navigation, safety control module can prevent that unmanned plane from colliding or the generation of other fortuitous events, this management-control method are equal
For the prior art；
Two, airborne data box is installed on unmanned plane（11）, on-board data box（11）It can be used as the Beck-up Control System of unmanned plane,
When the control system failure that unmanned plane carries, on-board data box（11）It can play a role automatically, meanwhile, on-board data box（11）
The flying quality of unmanned plane can be stored into cloud server in real time, make on-board data box（11）Play the function of cloud black box
Can, after generation accident, it not will cause the loss of flying quality；
Three, position of multiple control patrol aviation devices outside clearance zone close to airport is uniformly flown, defence type detecting and early warning system
The position of unmanned plane can be determined by receiving unmanned plane figure biography and remote signal, when received signal belongs to the unmanned plane in control
When, black winged aircraft interference system will not be triggered, when received signal is unknown signaling, and the normal of unmanned plane is will affect and flies
When row, it can be defaulted as black winged aircraft, the black winged aircraft lift-off such as do not need, after black winged aircraft booting in the short time
It was found that and be accurately positioned, while black winged aircraft interference system can be triggered, black winged aircraft interference system can pass through electromagnetic interference
Transmitter carries out accurate electromagnetic interference, adjust automatically electricity according to information such as working frequency, the directions of the black winged aircraft detected
Magnetic disturbance frequency and direction realize that black winged aircraft expelling and force-landing in prevention and control region；Ground telemetering and letter biography system can be
This function is played in approach area, will not influence normal unmanned plane during flying；
Four, when ground telemetering and letter pass system jam, control patrol aviation device can play temporary control function, temporarily
Safeguard the order on unmanned plane airport；
Five, it manages on patrol aviation device and high-definition camera is installed（6）, can be by the picture of shooting or realtime video transmission to cloud
Server, ground control control tower and operation remote control center, convenient for handling emergency in time or being supervised to airport surrounding enviroment
It surveys.
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110703790A (en) * | 2019-10-16 | 2020-01-17 | 一飞智控(天津)科技有限公司 | Unmanned aerial vehicle flight safety protection method and protection system based on cloud big data |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106846922A (en) * | 2017-03-14 | 2017-06-13 | 武汉天宇智戎防务科技有限公司 | Low altitude short range cluster cooperates with defence system and defence method |
| CN107204129A (en) * | 2017-05-27 | 2017-09-26 | 饶斯允 | A kind of civilian unmanned plane during flying management method and platform |
| CN107356945A (en) * | 2017-07-18 | 2017-11-17 | 华东师范大学 | A kind of portable low-altitude unmanned plane management-control method and system |
| CN107507461A (en) * | 2017-09-27 | 2017-12-22 | 中国科学院云南天文台 | A kind of unmanned plane quickly identifies system of defense |
| CN107516437A (en) * | 2017-07-12 | 2017-12-26 | 哈尔滨理工大学 | Unmanned plane managing and control system safe for operation and method in the air |
| CN107592180A (en) * | 2017-07-21 | 2018-01-16 | 合肥博雷电气有限公司 | A kind of unmanned plane countermeasure set control system |
| CN107643023A (en) * | 2017-07-21 | 2018-01-30 | 合肥博雷电气有限公司 | A kind of unmanned plane interference method |
| CN207706166U (en) * | 2017-11-29 | 2018-08-07 | 桂林电子科技大学 | A kind of receiving circuit for inveigling black winged UAV Navigation System |
-
2018
- 2018-08-29 CN CN201810993698.XA patent/CN108877299A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106846922A (en) * | 2017-03-14 | 2017-06-13 | 武汉天宇智戎防务科技有限公司 | Low altitude short range cluster cooperates with defence system and defence method |
| CN107204129A (en) * | 2017-05-27 | 2017-09-26 | 饶斯允 | A kind of civilian unmanned plane during flying management method and platform |
| CN107516437A (en) * | 2017-07-12 | 2017-12-26 | 哈尔滨理工大学 | Unmanned plane managing and control system safe for operation and method in the air |
| CN107356945A (en) * | 2017-07-18 | 2017-11-17 | 华东师范大学 | A kind of portable low-altitude unmanned plane management-control method and system |
| CN107592180A (en) * | 2017-07-21 | 2018-01-16 | 合肥博雷电气有限公司 | A kind of unmanned plane countermeasure set control system |
| CN107643023A (en) * | 2017-07-21 | 2018-01-30 | 合肥博雷电气有限公司 | A kind of unmanned plane interference method |
| CN107507461A (en) * | 2017-09-27 | 2017-12-22 | 中国科学院云南天文台 | A kind of unmanned plane quickly identifies system of defense |
| CN207706166U (en) * | 2017-11-29 | 2018-08-07 | 桂林电子科技大学 | A kind of receiving circuit for inveigling black winged UAV Navigation System |
Non-Patent Citations (2)
| Title |
|---|
| 张学平等: "低空安保无人机防控系统关键技术与应用", 第六届中国指挥控制大会论文集 * |
| 高永: "一种有效的无人机反制系统", 信息通信 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110703790A (en) * | 2019-10-16 | 2020-01-17 | 一飞智控(天津)科技有限公司 | Unmanned aerial vehicle flight safety protection method and protection system based on cloud big data |
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