CN207850190U - A kind of anti-unmanned aerial vehicle control system - Google Patents
A kind of anti-unmanned aerial vehicle control system Download PDFInfo
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- CN207850190U CN207850190U CN201721737105.0U CN201721737105U CN207850190U CN 207850190 U CN207850190 U CN 207850190U CN 201721737105 U CN201721737105 U CN 201721737105U CN 207850190 U CN207850190 U CN 207850190U
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Abstract
This application discloses a kind of anti-unmanned aerial vehicle control systems, are arranged in anti-drone body, the fixed-wing rotor for the anti-unmanned plane that takes off vertically；It is arranged in anti-drone body bottom, the ejection parachuting net for being captured to the black winged unmanned plane of target；Setting carries out the laser gun of laser destruction for winged unmanned plane black to target in anti-drone body bottom.As it can be seen that in the present invention, fixed-wing rotor, ejection parachuting net and laser gun are integrated in jointly on anti-unmanned plane, the advantages of each can be provided simultaneously with, thus it is possible to which the black winged unmanned plane in different scenes is captured or destroyed, the application range of anti-unmanned plane is substantially increased.
Description
Technical field
The utility model is related to unmanned plane field, more particularly to a kind of anti-unmanned aerial vehicle control system.
Background technology
In recent years, the application of unmanned plane is more and more extensive, in aerial reconnaissance, attack operations, night scene take photo by plane in can
See the figure of unmanned plane.Currently, can be substantially divided by carrying out destruction mode to unmanned plane by three kinds, one is blocking interference type,
Namely the sound wave either frequency sent out using unmanned plane countermeasure set, it forces unmanned plane to make a return voyage automatically either and lands automatically,
Its principle is mainly to interfere the GPS signal of unmanned plane either navigation system, to allow unmanned plane can not precise positioning,
Unmanned plane is forced to make a return voyage or force-land, but during interfering unmanned plane, it is possible to it can be to the aircarrier aircraft in course line
Interference is also resulted in, to cause the accident of bigger；Either directly unmanned plane is hit down using the bright method of violence, it is clear-cut straight
It connects, still, the unmanned plane remains after destroying can directly be fallen, and cause security risk；Also or it is by pacifying on unmanned plane
Huge catching net is filled to be captured to unmanned plane, but operation difficulty is larger, smaller scope of application.
Can adapt in different scenes it can be seen that providing a kind of novel anti-unmanned plane, to black winged unmanned plane into
Row destroys, and is those skilled in the art's urgent problem to be solved.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of anti-unmanned aerial vehicle control system, to improve anti-unmanned plane
The scope of application that black winged unmanned plane is destroyed.Its concrete scheme is as follows：
A kind of anti-unmanned aerial vehicle control system, including：
It is arranged in anti-drone body, the fixed-wing rotor for the anti-unmanned plane that takes off vertically；
It is arranged in the anti-drone body bottom, the ejection parachuting net for being captured to the black winged unmanned plane of target；
Setting carries out the laser of laser destruction for winged unmanned plane black to the target in the anti-drone body bottom
Big gun.
Preferably, further include：
It is arranged in the anti-drone body, for the anti-unmanned plane and the earth station to be established communication connection
Communication equipment.
Preferably, further include：
It is arranged in the anti-drone body, is hung for obtaining the photoelectricity of image information of the black winged unmanned plane of the target
Cabin.
Preferably, further include：
It is arranged in the anti-drone body, the data information for being obtained to the anti-unmanned plane carries out processing identification
Processor.
Preferably, further include：
It is arranged in the front end of the anti-drone body, the locator for positioning the black winged unmanned plane position of the target.
Preferably, further include：
It is arranged in the front end of the drone body, the navigator for navigating to the anti-unmanned plane.
Preferably, further include：
It is arranged in the anti-drone body, the maintenance of equipment for repairing the anti-unmanned plane.
Preferably, further include：
It is arranged in the anti-drone body, the power supply unit for being powered for the anti-unmanned plane.
Preferably, further include：
It is arranged in the drone body, for scouting, identifying that the scouting of the black winged unmanned plane of the target tracks load.
In the utility model, a kind of anti-unmanned aerial vehicle control system, including：It is arranged in anti-drone body, is used for
Take off vertically the fixed-wing rotor of anti-unmanned plane；Setting is carried out in anti-drone body bottom for winged unmanned plane black to target
The ejection parachuting net of capture；Setting carries out laser destruction in anti-drone body bottom, for winged unmanned plane black to target and swashs
Light big gun.
As it can be seen that in the present invention, when anti-unmanned plane receives the task of the black winged unmanned plane of target of earth station's transmission
It, need not be by runway when information, so that it may to be taken off vertically to sky using the fixed-wing rotor being arranged in anti-drone body
In, when anti-unmanned plane during flying to it is aerial when, just with the high-speed flight of fixed-wing pattern to the preset range of the black winged unmanned plane of target, and
And being captured or being destroyed for winged unmanned plane black to target is selected according to the flying scene of the black winged unmanned plane of target, that is, such as
The black winged unmanned plane of fruit target is then laser destruction to be carried out using laser gun winged unmanned plane black to target, if mesh in military base
It is then to be captured using ejection parachuting net winged unmanned plane black to target in civic area, can remove nothing to mark black winged unmanned plane
Man-machine directly landing realizes the capture or destruction of winged unmanned plane black to target 100% to injury caused by ground staff；It is aobvious
So, the anti-unmanned plane in the utility model can destroy the black winged unmanned plane under different flying scenes, substantially increase
The application range of anti-unmanned plane.
Description of the drawings
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is the embodiments of the present invention, for those of ordinary skill in the art, without creative efforts, also
Other attached drawings can be obtained according to the attached drawing of offer.
Fig. 1 is a kind of structure chart for anti-unmanned aerial vehicle control system that the utility model embodiment provides；
Fig. 2 is the structure chart for the anti-unmanned aerial vehicle control system of another kind that the utility model embodiment provides.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
The utility model embodiment discloses a kind of anti-unmanned aerial vehicle control system, as shown in Figure 1, the system includes：
It is arranged in anti-drone body, the fixed-wing rotor 101 for the anti-unmanned plane that takes off vertically；
It is arranged in anti-drone body bottom, the ejection parachuting net 102 for being captured to the black winged unmanned plane of target；
Setting carries out the laser gun 103 of laser destruction for winged unmanned plane black to target in anti-drone body bottom.
In recent years, with the continuous development of science and technology, the application of unmanned plane is more and more extensive, such as：It can be by nobody
Machine is applied in agricultural, is monitored to farmland crops using unmanned plane, can be with to reduce the loss of crops
Unmanned plane is applied in military field, the situation of enemy army is monitored, but there are also criminal, using unmanned plane come
Carry out some terrorist activities, or obtain some illegal information, for this kind of situation, it is necessary to people to these it is black fly nobody
Machine is destroyed, to ensure the safety of people's lives information.
Currently, rotor either fixed-wing is usually used in most of anti-unmanned plane, wherein fixed-wing has flight speed
Degree is fast, voyage is remote and the advantages such as efficient, but it the shortcomings that it is also more apparent, for example have to by runway help-fly and drop
It falls, can not hover；And rotor has the characteristics that landing convenience and mobility strong, not needing special runway can directly rise
Fly, greatly reduce the cost of anti-unmanned plane, but the flying speed of rotor is relatively slow, voyage is shorter and efficiency all can not show a candle to admittedly
Determine the wing.
For this case, fixed-wing and rotor are integrated in jointly in anti-drone body in the present invention,
That is fixed-wing rotor 101 can obtain simple and effective VTOL side in such a way that fixed-wing and rotor are combined
Case, fixed-wing rotor 101 have various advantages relative to other types, it can not be limited by landing place, again
Have the characteristics of Fixed Wing AirVehicle high maneuverability, so, when anti-unmanned plane receives the destruction task of the black winged unmanned plane of target
When, it will not be limited by scene of taking off, can take off at any time, quickly execute destruction task.
Specifically, when anti-unmanned plane receives the mission bit stream of the black winged unmanned plane of target, need not be utilized by runway
Fixed-wing rotor 101 rollings takeoff to aerial, when anti-unmanned plane take off vertically to it is aerial when, may turn on fixed-wing pattern, it is high
Speed, high maneuverability winged unmanned plane black to target patrol, the black winged unmanned plane of tracking lock target, and persistently close to target
Black winged unmanned plane, and in suitable distance range, winged unmanned plane black to target destroys.As it can be seen that by rotor and fixation
The wing integrates, and anti-unmanned plane can not only be enable to take off vertically, and reduces the cost of anti-unmanned plane, and because anti-nothing
It is man-machine to have the advantages of rotor and fixed-wing, so the anti-unmanned plane is enabled to be applicable to more flying scenes.
In the present embodiment, parachuting net 102 will be launched and laser gun 103 is integrated in the bottom of anti-drone body jointly
Portion can be in the form of launching parachuting net 102 according to the flying field of the black winged unmanned plane of target, selection or laser gun
103 form substantially increases the application of anti-unmanned plane in the utility model to capture or destroy the black winged unmanned plane of target
Range.It is also contemplated that when being captured using the ejection winged unmanned plane black to target of parachuting net 102, it will not be to the day of people
Often life interferes, and is suitable for civic area；It is clear-cut straight when being destroyed using the winged unmanned plane black to target of laser gun 103
It connects, can realize 100% kill probability, be suitable for military area.
Specifically, when the preset range of anti-unmanned plane during flying to the black winged unmanned plane of target, so that it may with to the black winged nothing of target
It is man-machine to be destroyed.If the black winged unmanned plane of target is in civic area, so that it may to utilize the ejection being arranged on anti-unmanned plane
The winged unmanned plane black to target of parachuting net 102 captures, that is, when the photoelectric nacelle being arranged on anti-unmanned plane finds that target is black
When flying unmanned plane, can the ejection parachuting net in anti-drone body bottom be set for expansion rapidly, winged unmanned plane black to target carries out
It captures.After being captured using 102 winged unmanned plane black to target of ejection parachuting net, the black winged unmanned plane of target is with ejection parachuting net
102 directly drop to ground, will not be damaged to ground staff, after when anti-unmanned plane, to target, black winged unmanned plane destroys,
Runway can not be needed with vertical landing, it is only necessary to which the level land of very little can land, and substantially increase anti-in the utility model
The efficiency of unmanned plane work, reduces the cost of anti-unmanned plane.
It should be noted that after being captured using the ejection winged unmanned plane black to target of parachuting net 102, it can be with Selection utilization
Anti- unmanned plane directly carries the black winged unmanned plane of target and lands, or after capturing target black winged unmanned plane, allows target
Directly voluntarily umbrella is fallen black winged unmanned plane, will not in addition occupy the load of anti-unmanned plane, is not in because capturing the black winged nothing of target
Man-machine quality is larger, and the case where cause anti-unmanned plane air crash, system is caught compared to other large size unmanned plane nets, is had higher
Mobility, it is easy to operate, be not in that the black winged unmanned plane of target is lost and the case where can not capturing.Certainly, in practical application,
Parachuting is specifically carried out using any parachuting net mode winged unmanned plane black to target, all for the purpose of reaching practical application, this
Place is not construed as limiting.
It is understood that if the black winged unmanned plane of target is in military applications, general operational base is more spacious, will not
There is a large amount of residential block, so the black winged unmanned plane landing of target, will not interfere the life of the people, in the case,
Anti- unmanned plane can utilize the winged unmanned plane black to target of laser gun 103 being arranged in anti-drone body bottom to strike, until
The black winged unmanned plane of target is destroyed.It is also contemplated that being destroyed using the winged unmanned plane black to target of laser gun 103, destroy
It is efficient, 100% kill probability may be implemented.
As it can be seen that in the present invention, when anti-unmanned plane receives the task of the black winged unmanned plane of target of earth station's transmission
It, need not be by runway when information, so that it may to be taken off vertically to sky using the fixed-wing rotor being arranged in anti-drone body
In, when anti-unmanned plane during flying to it is aerial when, just with the high-speed flight of fixed-wing pattern to the preset range of the black winged unmanned plane of target, and
And winged unmanned plane black to target is selected to be captured or destroyed according to the flying scene of the black winged unmanned plane of target, that is, if
The black winged unmanned plane of target is then laser destruction to be carried out using laser gun winged unmanned plane black to target, if target in military base
Black winged unmanned plane is then to be captured using ejection parachuting net winged unmanned plane black to target in civic area, can remove nobody from
Machine directly lands to injury caused by ground staff, and then realizes the capture or destruction of winged unmanned plane black to target 100%；It is aobvious
So, the anti-unmanned plane in the utility model can destroy the black winged unmanned plane under different flying scenes, substantially increase
The application range of anti-unmanned plane.
Based on above-described embodiment, as a preferred embodiment, the present embodiment carries out specifically a upper embodiment
Illustrate, as shown in Fig. 2, anti-unmanned aerial vehicle control system provided by the utility model further includes：
It is arranged in anti-drone body, the communication equipment 104 for anti-unmanned plane and earth station to be established to communication connection.
It is arranged in anti-drone body, the photoelectric nacelle 105 of the image information for obtaining the black winged unmanned plane of target.
It is arranged in anti-drone body, the data information for being obtained to anti-unmanned plane carries out the processor of processing identification
106。
Specifically, can be by anti-unmanned plane and earth station using the communication equipment 104 being arranged in anti-drone body
Communication connection is established, that is, anti-unmanned plane can receive the message of earth station's monitoring, meanwhile, the information on anti-unmanned plane
It can be by 104 real-time Transmission of communication equipment to earth station, so that the staff of earth station is according to the letter on anti-unmanned plane
Breath, is in real time adjusted the working condition of anti-unmanned plane.
It is understood that flying quality of the image data compared to the black winged unmanned plane of target that miscellaneous equipment is got,
Image information can more accurate, intuitively reflect the working condition of the black winged unmanned plane of target, so, in the present embodiment,
The image information of the black winged unmanned plane of target can be obtained using the photoelectric nacelle 105 being arranged in anti-drone body, then,
According to the data information for the black winged unmanned plane of target that image information acquisition arrives, winged unmanned plane black to target is captured or is destroyed.
It, being capable of better winged nothing black to target moreover, the data information got by the photoelectric nacelle 105 being arranged on anti-unmanned plane
It is man-machine to be destroyed.Certainly, the model of photoelectric nacelle 105 is not limited specifically herein, all are to reach practical application
Purpose.
It is also contemplated that when getting the status information of the black winged unmanned plane of target using photoelectric nacelle 105, in order to right
The black winged unmanned plane of target is preferably destroyed, and continual winged unmanned plane black to target is needed to be identified and track, at this point,
Can also utilize the processor 106 that is arranged in anti-drone body to the data information to the black winged unmanned plane of target of acquisition into
Row processing, to ensure that anti-unmanned plane can destroy black winged unmanned plane.Also, communication equipment in this process, can also be passed through
106 will treated that data information is transmitted to earth station in real time, to facilitate the staff on ground according to the data got
Information disposes anti-unmanned plane the action of next step.
Based on above-described embodiment, as a preferred embodiment, the present embodiment carries out specifically a upper embodiment
Illustrate, anti-unmanned aerial vehicle control system provided by the utility model further includes：
It is arranged in the front end of anti-drone body, the locator 107 for positioning the black winged unmanned plane position of target.
It is arranged in the front end of drone body, the navigator 108 for navigating to anti-unmanned plane.
It is also contemplated that in order to ensure to the black winged unmanned plane of target accurately capture or strike, it is also necessary to low coverage
From winged unmanned plane black to target be identified, with ensure winged unmanned plane black to target it is accurate capture or destruction.So when anti-
Unmanned plane with a distance from the black winged unmanned plane of target farther out when, scout that load is black to target to fly using the tracking that is arranged on anti-unmanned plane
Unmanned plane is scouted, but when nobody anti-black from target winged unmanned plane is closer, so that it may with using being arranged in anti-drone body
On locator 107 and navigator 108, winged unmanned plane black to target carry out more accurate positioning and identification, when instead nobody
Machine navigates to winged unmanned plane black to target in the black winged unmanned plane preset range of target and is captured or destroyed.Certainly, it is actually answering
With in the middle, can the locator that is positioned of winged unmanned plane black to target and navigator it is varied, all are to reach practical
For the purpose of, it is not construed as limiting herein.
Based on above-described embodiment, as a preferred embodiment, the present embodiment carries out specifically a upper embodiment
Illustrate, anti-unmanned aerial vehicle control system provided by the utility model further includes：
It is arranged in anti-drone body, the maintenance of equipment 109 for repairing anti-unmanned plane.
It is arranged in anti-drone body, the power supply unit 110 for being powered for anti-unmanned plane.
It is understood that in order to enable anti-unmanned plane is preferably worked, instead without being also provided with energy on human body
It is enough to the maintenance of equipment 109 repaired when anti-unmanned plane failure and the power supply unit 110 being powered for anti-unmanned plane, with
The normal work of anti-unmanned plane is ensured, certainly herein for the concrete form of maintenance of equipment and power supply unit on anti-unmanned plane
It does not limit specifically, all are for the purpose of it can reach practical application.
Based on above-described embodiment, as a preferred embodiment, the present embodiment carries out specifically a upper embodiment
Illustrate, anti-unmanned aerial vehicle control system provided by the utility model further includes：
It is arranged in drone body, for scouting, identifying that the scouting of the black winged unmanned plane of target tracks load 111.
It is also contemplated that scouting tracking load 111 as task device most basic in anti-unmanned plane, the main of it is appointed
Business is that winged unmanned plane black to target is detected, identified and tracked, and then realizes the destruction of winged unmanned plane black to target.It can manage
Solution, can realize winged unmanned plane black to target scouted, the scouting that tracks tracking load it is varied, such as：It can be with
Using photoelectric sensor daytime winged unmanned plane black to target scout, using infrared sensor in night winged nothing black to target
It is man-machine to be scouted, it not only can accurately measure the distance of the black winged unmanned plane of target using laser radar, but also can be with
The shape and behavioral characteristics of the high-precision extraction black winged unmanned plane of target, realize that winged unmanned plane black to target more accurately tests the speed
And tracking.
Certainly, in practical application, various scoutings tracking load have respective advantage and disadvantage, it is possible to it is anti-nobody
A variety of scouting tracking load are set simultaneously on machine, so that different scouting tracking load cooperates, to ensure fly black to target
The destruction efficiency of unmanned plane.All are not construed as limiting herein for the purpose of reaching practical application.
The foregoing description of the disclosed embodiments enables those skilled in the art to realize or use the utility model.
Various modifications to these embodiments will be apparent for a person skilled in the art, general original as defined herein
Reason can be realized in other embodiments without departing from the spirit or scope of the present utility model.Therefore, this practicality is new
Type is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase
Consistent widest range.
Claims (9)
1. a kind of anti-unmanned aerial vehicle control system, which is characterized in that including：
It is arranged in anti-drone body, the fixed-wing rotor for the anti-unmanned plane that takes off vertically；
It is arranged in the anti-drone body bottom, the ejection parachuting net for being captured to the black winged unmanned plane of target；
Setting carries out the laser gun of laser destruction for winged unmanned plane black to the target in the anti-drone body bottom.
2. control system according to claim 1, which is characterized in that further include：
It is arranged in the anti-drone body, the communication for the anti-unmanned plane to be established to communication connection with earth station is set
It is standby.
3. control system according to claim 1, which is characterized in that further include：
It is arranged in the anti-drone body, the photoelectric nacelle of the image information for obtaining the black winged unmanned plane of the target.
4. control system according to claim 1, which is characterized in that further include：
It is arranged in the anti-drone body, the data information for being obtained to the anti-unmanned plane carries out the place of processing identification
Manage device.
5. control system according to claim 1, which is characterized in that further include：
It is arranged in the front end of the anti-drone body, the locator for positioning the black winged unmanned plane position of the target.
6. control system according to claim 1, which is characterized in that further include：
It is arranged in the front end of the drone body, the navigator for navigating to the anti-unmanned plane.
7. control system according to claim 1, which is characterized in that further include：
It is arranged in the anti-drone body, the maintenance of equipment for repairing the anti-unmanned plane.
8. control system according to claim 1, which is characterized in that further include：
It is arranged in the anti-drone body, the power supply unit for being powered for the anti-unmanned plane.
9. according to claim 1 to 8 any one of them control system, which is characterized in that further include：
It is arranged in the drone body, for scouting, identifying that the scouting of the black winged unmanned plane of the target tracks load.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201721737105.0U CN207850190U (en) | 2017-12-13 | 2017-12-13 | A kind of anti-unmanned aerial vehicle control system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201721737105.0U CN207850190U (en) | 2017-12-13 | 2017-12-13 | A kind of anti-unmanned aerial vehicle control system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109324632A (en) * | 2018-09-19 | 2019-02-12 | 湖南大科激光有限公司 | The anti-UAV system of UAV system laser weapon |
| CN109916227A (en) * | 2017-12-13 | 2019-06-21 | 中电科特种飞机***工程有限公司 | A kind of anti-unmanned aerial vehicle control system and method |
| CN110182363A (en) * | 2019-04-26 | 2019-08-30 | 厦门大学 | It is a kind of for capturing the flying wing type unmanned plane of unmanned plane |
-
2017
- 2017-12-13 CN CN201721737105.0U patent/CN207850190U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109916227A (en) * | 2017-12-13 | 2019-06-21 | 中电科特种飞机***工程有限公司 | A kind of anti-unmanned aerial vehicle control system and method |
| CN109324632A (en) * | 2018-09-19 | 2019-02-12 | 湖南大科激光有限公司 | The anti-UAV system of UAV system laser weapon |
| CN110182363A (en) * | 2019-04-26 | 2019-08-30 | 厦门大学 | It is a kind of for capturing the flying wing type unmanned plane of unmanned plane |
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Address after: 643000 No. 9 Aviation Avenue, Zigong Aviation Industrial Park, Sichuan Province Patentee after: China Electric Special Aircraft Systems Engineering Co., Ltd. Address before: 618300 No. 74 Taizhong Road, Guanghan City, Deyang City, Sichuan Province Patentee before: In Dianke (Deyang Guanghan) Special Aircraft System Engineering Co. Ltd. |