CN209197576U - A kind of anti-UAV system of high-precision - Google Patents
A kind of anti-UAV system of high-precision Download PDFInfo
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- CN209197576U CN209197576U CN201821900341.4U CN201821900341U CN209197576U CN 209197576 U CN209197576 U CN 209197576U CN 201821900341 U CN201821900341 U CN 201821900341U CN 209197576 U CN209197576 U CN 209197576U
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- fuselage
- tripod head
- fixedly mounted
- directional tripod
- lithium battery
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Abstract
The utility model discloses a kind of anti-UAV system of high-precision, it include: rotor wing unmanned aerial vehicle and electromagnetic launcher, wherein, rotor wing unmanned aerial vehicle includes rotor blade, motor, rocker arm, undercarriage, fuselage, target localization and tracking system, lithium battery, flight control system and all-directional tripod head, target localization and tracking system is fixedly mounted on the side of fuselage, lithium battery is fixedly mounted on fuselage, for for motor, target localization and tracking system, flight control system and all-directional tripod head power supply, all-directional tripod head is fixedly mounted on the lower section of fuselage, electromagnetic launcher is mounted on the lower section of all-directional tripod head and connect with lithium battery, flight control system is fixedly mounted on the top of fuselage, for controlling electromagnetic launcher rotation by all-directional tripod head.The anti-UAV system of the high-precision is structurally reasonable, can locking and track automatically target, power consumption, influences small, to other normal legal working electronic equipment of periphery are small.
Description
Technical field
The utility model relates to field of aerospace technology, specifically provide a kind of anti-UAV system of high-precision.
Background technique
At present unmanned plane take photo by plane, self-timer, investigation, the fields such as news report are widely used, but due to nothing
Man-machine difficult to regulate, the phenomenon for causing unmanned plane disorderly to fly is generally existing, and unmanned plane, which flies around, will cause very big security risk,
The event for especially invading obstacle free airspace protection zone occurs again and again, has seriously threatened the normal operation and passenger's life peace on airport
Entirely.Since flying height is low during takeoff and landing for aircraft, maneuverability is poor, encounters the lift-off object such as unmanned plane, is difficult to take
Effective means are evaded in time, may threaten flight safety, or flight is caused to be delayed.So being needed to ensure flight safety
A clean region is created in the region of takeoff and landing.Some country prohibited some important scenes landings nobody
Machine, each ground zoning have no-fly zone.
In order to guarantee that the safety in no-fly airspace, anti-UAV system become the Research Emphasis of related fields, more often at present
For the anti-UAV system of hand-held, interference is generated to unmanned plane by transmitting electromagnetic wave band, thus reach expel or
The purpose shot down.Since the flying height of unmanned plane is big, distance is remote, speed is fast, lead to the electromagnetic wave for holding anti-UAV system
Transmitter power is high, power consumption is fast, target poor location, and powerful electromagnetic radiation, also will affect other normal legals of periphery
The electronic equipment of work.Therefore how to reduce electromagnetic radiation power, the precision of raising target positioning is ground as related fields
The emphasis of hair.
Utility model content
In consideration of it, the purpose of this utility model is to provide a kind of anti-UAV system of high-precision, it is existing hand-held to solve
The problems such as anti-UAV system electromagnetic wave transmitter power of formula is high, power consumption is fast, target poor location.
Technical solution provided by the utility model is: a kind of anti-UAV system of high-precision, comprising: rotor wing unmanned aerial vehicle and electricity
Magnetic ejector, wherein rotor wing unmanned aerial vehicle include rotor blade, motor, rocker arm, undercarriage, fuselage, target localization and tracking system,
Lithium battery, flight control system and all-directional tripod head, rotor blade are mounted on motor, and motor is fixedly mounted on the one of rocker arm
End, the other end of rocker arm are fixedly mounted on fuselage, and undercarriage is symmetrically mounted on fuselage down either side, target localization and tracking system
It is fixedly mounted on the side of fuselage, for the aircraft in locating and tracking no-fly zone, lithium battery is fixedly mounted on fuselage, is used for
For the power supply of motor, target localization and tracking system, flight control system and all-directional tripod head, all-directional tripod head is fixedly mounted on fuselage
Lower section, electromagnetic launcher is mounted on the lower section of all-directional tripod head and connect with lithium battery, and flight control system is fixedly mounted on
The top of fuselage, for controlling the state of flight of rotor wing unmanned aerial vehicle and controlling electromagnetic launcher rotation by all-directional tripod head.
It is preferred that the fuselage is carbon fibre composite fuselage.
Further preferably, one layer of metal mesh is wrapped up on lithium battery and all-directional tripod head surface.
Further preferably, the electromagnetic launcher can emit multiwave electromagnetic signal.
The anti-UAV system of high-precision provided by the utility model can capture the target flown in the air and progress automatically
Locking tracking, after tracing into a certain distance, target is expelled by can achieve to objective emission electromagnetic signal or
The purpose shot down, to improve the accuracy to strike target.
The anti-UAV system of high-precision provided by the utility model has the beneficial effect that:
1, can lock and track automatically target by target localization and tracking system, substantially increase strike target it is accurate
Degree；
2, it when striking target, since distance objective is closer, does not need to carry powerful electromagnetic radiation equipment, not only subtract
The small power consumption of lithium battery, while also mitigating the influence to other normal legal working electronic equipment of periphery；
3, the self-contained electronic signal equipment of anti-UAV system and electromagnetic launcher are isolated using metal mesh, it can be with
Interference when mitigating electromagnetic launcher transmitting electromagnetic wave to anti-UAV system itself.
Detailed description of the invention
With reference to the accompanying drawing and embodiment is described in further detail the utility model:
Fig. 1 is the structural schematic diagram of the anti-UAV system of high-precision provided by the utility model；
Fig. 2 is the right view of Fig. 1；
Fig. 3 is the top view of Fig. 1；
Wherein, 1, rotor blade, 2, motor, 3, rocker arm, 4, undercarriage, 5, fuselage, 6, target localization and tracking system, 7, lithium
Battery, 8, electromagnetic launcher, 9, flight control system, 10, all-directional tripod head.
Specific embodiment
The utility model is further explained below in conjunction with specific embodiment, but limitation is not originally practical
It is novel.
As shown in Figure 1 to Figure 3, the utility model provides a kind of anti-UAV system of high-precision, comprising: rotor wing unmanned aerial vehicle
With electromagnetic launcher 8, wherein rotor wing unmanned aerial vehicle includes rotor blade 1, motor 2, rocker arm 3, undercarriage 4, fuselage 5, target positioning
Tracking system 6, lithium battery 7, flight control system 9 and all-directional tripod head 10, rotor blade 1 are mounted on motor 2, and motor 2 is solid
Dingan County is mounted in one end of rocker arm 3, and the other end of rocker arm 3 is fixedly mounted on fuselage 5, and undercarriage 4 is symmetrically mounted on 5 two sides of fuselage
Lower section, target localization and tracking system 6 are fixedly mounted on the side of fuselage 5, for the aircraft in locating and tracking no-fly zone, lithium electricity
Pond 7 is fixedly mounted on fuselage 5, for being motor 2, target localization and tracking system 6, flight control system 9 and all-directional tripod head
10 power supplies, all-directional tripod head 10 are fixedly mounted on the lower section of fuselage 5, and electromagnetic launcher 8 is mounted on the lower section of all-directional tripod head 10
And connect with lithium battery 7, flight control system 9 is fixedly mounted on the top of fuselage 5, for controlling the flight shape of rotor wing unmanned aerial vehicle
State and by all-directional tripod head 10 control electromagnetic launcher 8 rotate, wherein the target localization and tracking system be the prior art,
This patent repeats no more.
The working principle of the anti-UAV system of the high-precision is as follows: when there is unknown unmanned vehicle to enter no-fly region,
Start the anti-UAV system, lithium battery is motor power supply, and motor is started to work, and drives rotor blade rotation to generate liter
Power makes anti-UAV system go up to the air；After lift-off, by flight control system start target localization and tracking system to it is unknown nobody fly
Row device carries out target lock-on and tracking, and when tracking a certain distance, flight control system is rotated by all-directional tripod head
Electromagnetic launcher, to carry out orientation adjustment to it, to enable electromagnetic launcher to be directed at lock onto target and emit multiband electromagnetism
Signal, until target shot down or flown away from no-fly region, it is preferable that flight control system by the motor on all-directional tripod head come
Drive electromagnetic launcher rotation.
In order to which electromagnetic launcher and the self-contained electronic signal equipment of rotor wing unmanned aerial vehicle is isolated, to mitigate electromagnetic launcher
Interference when emitting electromagnetic wave to anti-UAV system itself, as the improvement of technical solution, the fuselage 5 is that carbon fiber is compound
Material fuselage, further preferably, lithium battery 7 and 10 surface of all-directional tripod head wrap up one layer of metal mesh.
As the improvement of technical solution, the electromagnetic launcher 8 can emit multiwave electromagnetic signal.
Specific embodiment of the present utility model is write according to progressive mode, and each embodiment party is highlighted
The difference of case, similar portion can be with cross-reference.
The embodiments of the present invention is elaborated above in conjunction with attached drawing, but the utility model is not limited to
Above embodiment can also not depart from the utility model within the knowledge of a person skilled in the art
Various changes can be made under the premise of objective.
Claims (4)
1. a kind of anti-UAV system of high-precision characterized by comprising rotor wing unmanned aerial vehicle and electromagnetic launcher (8), wherein
Rotor wing unmanned aerial vehicle includes rotor blade (1), motor (2), rocker arm (3), undercarriage (4), fuselage (5), target localization and tracking system
(6), lithium battery (7), flight control system (9) and all-directional tripod head (10), rotor blade (1) are mounted on motor (2), motor
(2) it is fixedly mounted on one end of rocker arm (3), the other end of rocker arm (3) is fixedly mounted on fuselage (5), and undercarriage (4) is symmetrically pacified
Mounted in fuselage (5) down either side, target localization and tracking system (6) is fixedly mounted on the side of fuselage (5), prohibits for locating and tracking
Fly the aircraft in area, lithium battery (7) is fixedly mounted on fuselage (5), for being motor (2), target localization and tracking system
(6), flight control system (9) and all-directional tripod head (10) power supply, all-directional tripod head (10) are fixedly mounted under fuselage (5)
Side, electromagnetic launcher (8) are mounted on the lower section of all-directional tripod head (10) and connect with lithium battery (7), and flight control system (9) is solid
Dingan County is mounted in the top of fuselage (5), for controlling the state of flight of rotor wing unmanned aerial vehicle and by all-directional tripod head (10) control electricity
Magnetic ejector (8) rotation.
2. the anti-UAV system of high-precision described in accordance with the claim 1, it is characterised in that: the fuselage (5) is multiple for carbon fiber
Condensation material fuselage.
3. the anti-UAV system of high-precision described in accordance with the claim 1, it is characterised in that: lithium battery (7) and all-directional tripod head
(10) one layer of metal mesh is wrapped up on surface.
4. according to the anti-UAV system of high-precision described in any one of claims 1 to 3, it is characterised in that: the electromagnetism hair
Emitter (8) can emit multiwave electromagnetic signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821900341.4U CN209197576U (en) | 2018-11-19 | 2018-11-19 | A kind of anti-UAV system of high-precision |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821900341.4U CN209197576U (en) | 2018-11-19 | 2018-11-19 | A kind of anti-UAV system of high-precision |
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| Publication Number | Publication Date |
|---|---|
| CN209197576U true CN209197576U (en) | 2019-08-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201821900341.4U Active CN209197576U (en) | 2018-11-19 | 2018-11-19 | A kind of anti-UAV system of high-precision |
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| Country | Link |
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| CN (1) | CN209197576U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111272019A (en) * | 2020-03-27 | 2020-06-12 | 牛三库 | Intelligent elastic net |
| CN112344798A (en) * | 2020-11-19 | 2021-02-09 | 中国人民解放军国防科技大学 | Non-cooperative flight target flexible capturing system inspired by humane magic spider creatures |
| DE102022004723A1 (en) | 2022-12-15 | 2024-06-20 | Diehl Defence Gmbh & Co. Kg | HPEM drone with horn integrated into the landing gear |
-
2018
- 2018-11-19 CN CN201821900341.4U patent/CN209197576U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111272019A (en) * | 2020-03-27 | 2020-06-12 | 牛三库 | Intelligent elastic net |
| CN112344798A (en) * | 2020-11-19 | 2021-02-09 | 中国人民解放军国防科技大学 | Non-cooperative flight target flexible capturing system inspired by humane magic spider creatures |
| DE102022004723A1 (en) | 2022-12-15 | 2024-06-20 | Diehl Defence Gmbh & Co. Kg | HPEM drone with horn integrated into the landing gear |
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