CN205666840U - Unmanned aerial vehicle flight control jamming system - Google Patents
Unmanned aerial vehicle flight control jamming system Download PDFInfo
- Publication number
- CN205666840U CN205666840U CN201620549621.XU CN201620549621U CN205666840U CN 205666840 U CN205666840 U CN 205666840U CN 201620549621 U CN201620549621 U CN 201620549621U CN 205666840 U CN205666840 U CN 205666840U
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- China
- Prior art keywords
- signal generator
- interference
- flight control
- evac
- switch
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- Expired - Fee Related
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title claims abstract description 12
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 claims description 16
- 230000001105 regulatory effect Effects 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims 1
- 230000005611 electricity Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 abstract description 2
- 230000002452 interceptive effect Effects 0.000 abstract 4
- 230000001629 suppression Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
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- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle flight control jamming system, including interfering signal generator, transmitter and interference suppressor, interference suppressor's the output and the input of interfering signal generator are connected, and the output of interfering signal generator is connected with the input of transmitter, interfering signal generator and transmitter are established on the telescopic link of adjustable length. The utility model discloses an electromagnetic wave of the wideer frequency channel of release ratio unmanned aerial vehicle control signal, it increases noise or strong signal suppression technique to adopt to directional or qxcomm technology's interference mode makes unmanned aerial vehicle control failure, thereby makes unmanned aerial vehicle lose control, reaches the purpose of its flight of restriction.
Description
Technical field
This utility model relates to a kind of unmanned plane interference unit, is specifically related to a kind of UAV Flight Control EVAC.
Background technology
Current all kinds of unmanned vehicle constantly occurs, the harm of unmanned vehicle particularly unmanned plane gradually displays.
Owing to unmanned plane is a flying platform, by carry different payload can cross scouting, communication, the most attack
Business.Therefore, in particular task or tricky time, need illegal unmanned plane is disturbed, thus reach safety, secrecy want
Ask.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of easy to use, unmanned plane during flying control that interference effect is good
EVAC processed.
For solving above-mentioned technical problem, technical solution adopted in the utility model is:
A kind of UAV Flight Control EVAC, including interference signal generator, emitter and interference suppressor；Described
The outfan of interference suppressor is connected with the input of interference signal generator, the outfan of interference signal generator and emitter
Input connect；Described interference signal generator and emitter are located on the expansion link of adjustable-length.
Further, described interference signal generator includes that the oscillating circuit being sequentially connected with, voltage controlled oscillator and power are put
Big device；Described emitter includes radio frequency transmitter circuitry and launches antenna；Power amplifier is connected with radio frequency transmitter circuitry, and radio frequency is sent out
Radio road is connected with launching antenna.
Further, described interference suppressor includes that the power supply for system power supply, interference switch, frequency modulation switch, power are adjusted
Joint switch and display screen；Interference switch is connected with power supply, and frequency modulation switch is connected with voltage controlled oscillator, power regulating switch and power
Amplifier connects.
Further, described interference signal generator is that GPS disturbs signal generator.
Further, also including wearable headring on staff's head, expansion link is located at the top of headring, interference control
Device processed is hand-held.
Further, the outside of described headring is additionally provided with flash lamp.
Use and have the beneficial effects that produced by technique scheme:
The flight of unmanned plane (including the unmanned plane such as helicopter, multiple wing, fixed-wing unmanned plane) is mainly by unmanned aerial vehicle (UAV) control
Device sends control signal, and this control signal is mainly the electromagnetic wave signal of fixed frequency range.This utility model is unmanned by release ratio
The electromagnetic wave of the broader frequency range of machine control signal, uses and increases noise or strong signal compact technique, do with orientation or omnidirectional
The mode of disturbing makes unmanned aerial vehicle (UAV) control lose efficacy, so that unmanned plane is out of hand, reaches to limit the purpose of its flight.For unmanned plane
GPS positions cruise, can increase GPS and disturb signal so that it is GPS controls cruise and lost efficacy, thus cannot be normal in interference signal
Flight.Ultimately result in unmanned plane to be engaged in some illegal activities and cannot succeed.
Accompanying drawing explanation
Fig. 1 is the structural representation of this utility model first embodiment；
Fig. 2 is the structural representation of this utility model the second embodiment；
In figure: 1, headring, 2, interference signal generator, 3, emitter, 4, interference suppressor, 5, flash lamp, 6, interference opens
Close, 7, frequency modulation switch, 8, power regulating switch, 9, display screen, 10, expansion link.
Detailed description of the invention
With detailed description of the invention, this utility model is described in further detail below in conjunction with the accompanying drawings.
As it is shown in figure 1, this utility model first embodiment, a kind of UAV Flight Control EVAC, including interference letter
Number generator 2, emitter 3 and interference suppressor 4；The outfan of described interference suppressor 4 and the input disturbing signal generator 2
End connects, and the outfan of interference signal generator 2 is connected with the input of emitter 3；Interference signal generator 2 and emitter 3
It is located on the expansion link 10 of adjustable-length.Interference signal generator 2 includes oscillating circuit, voltage controlled oscillator and the merit being sequentially connected with
Rate amplifier；Described emitter 3 includes radio frequency transmitter circuitry and launches antenna；Power amplifier is connected with radio frequency transmitter circuitry,
Radio frequency transmitter circuitry is connected with launching antenna.Interference suppressor 4 includes the power supply for system power supply, interference switch 6, frequency modulation switch
7, power regulating switch 8 and display screen 9；Interference switch 6 is connected with power supply, and frequency modulation switch 7 is connected with voltage controlled oscillator, and power is adjusted
Joint switch 8 is connected with power amplifier.
Described interference signal generator 2 disturbs signal generator for GPS.
This utility model by the electromagnetic wave of the release ratio broader frequency range of unmanned aerial vehicle (UAV) control signal, use increase noise or
Strong signal compact technique, makes unmanned aerial vehicle (UAV) control lose efficacy with orientation or omnidirectional's conflicting mode, so that unmanned plane is out of hand, reaches
To the purpose limiting its flight.GPS for unmanned plane positions cruise, can increase GPS and disturb signal, make in interference signal
Its GPS controls cruise and lost efficacy, thus cannot normal flight.Ultimately result in unmanned plane to be engaged in some illegal activities and cannot succeed.
As in figure 2 it is shown, the second embodiment of the present utility model, also include wearable headring 1 on staff's head, stretch
Contracting bar 10 is located at the top of headring 1, and interference suppressor 4 is hand-held.The outside of headring 1 is additionally provided with flash lamp 5.
The present embodiment uses wear-type, easy to use, is worn on the head by headring 1 by staff in use, both made
EVAC has certain height, prevents EVAC itself from being affected by peripheral obstacle, and EVAC has again one simultaneously
Fixed mobility, movement is more convenient fast；Interference suppressor 4 by staff hand held in, regulate, control very convenient.
Interference suppressor 4 uses plug-in with the connecting line of interference signal generator 2, and the on-chip power of EVAC is at interference suppressor
In 4, change or charge ratio is more convenient.Interference switch 6 is for controlling the operations of EVAC, and frequency modulation switch 7 is used for regulating voltage-controlled
The scope of oscillator output frequencies, power regulating switch 8 is for regulating the power of output frequency, and display screen 9 is for display interference
The frequency range used.The flash lamp 5 arranged outside headring 1, can be used for reminding surrounding people to note keeping away when staff moves
Allow.
Claims (6)
1. a UAV Flight Control EVAC, it is characterised in that: include disturb signal generator (2), emitter (3) and
Interference suppressor (4)；The outfan of described interference suppressor (4) is connected with the input of interference signal generator (2), interference letter
Number outfan of generator (2) is connected with the input of emitter (3)；Described interference signal generator (2) and emitter (3) set
On the expansion link (10) of adjustable-length.
UAV Flight Control EVAC the most according to claim 1, it is characterised in that: described interference signal generator
(2) oscillating circuit, voltage controlled oscillator and the power amplifier being sequentially connected with is included；Described emitter (3) includes radio-frequency transmissions electricity
Road and transmitting antenna；Power amplifier is connected with radio frequency transmitter circuitry, and radio frequency transmitter circuitry is connected with launching antenna.
UAV Flight Control EVAC the most according to claim 2, it is characterised in that: described interference suppressor (4)
Including power supply, interference switch (6), frequency modulation switch (7), power regulating switch (8) and display screen (9) for system power supply；Interference
Switch (6) is connected with power supply, and frequency modulation switch (7) is connected with voltage controlled oscillator, and power regulating switch (8) is with power amplifier even
Connect.
UAV Flight Control EVAC the most according to claim 1, it is characterised in that: described interference signal generator
(2) it is that GPS disturbs signal generator.
UAV Flight Control EVAC the most according to claim 1, it is characterised in that: also include wearable in work
Headring (1) on personnel's head, expansion link (10) is located at the top of headring (1), and interference suppressor (4) is hand-held.
UAV Flight Control EVAC the most according to claim 5, it is characterised in that: the outside of described headring (1)
It is additionally provided with flash lamp (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620549621.XU CN205666840U (en) | 2016-06-08 | 2016-06-08 | Unmanned aerial vehicle flight control jamming system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620549621.XU CN205666840U (en) | 2016-06-08 | 2016-06-08 | Unmanned aerial vehicle flight control jamming system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205666840U true CN205666840U (en) | 2016-10-26 |
Family
ID=57156583
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620549621.XU Expired - Fee Related CN205666840U (en) | 2016-06-08 | 2016-06-08 | Unmanned aerial vehicle flight control jamming system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205666840U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106849965A (en) * | 2017-04-07 | 2017-06-13 | 北京智宇翔云科技有限公司 | A kind of aerial signal output circuit and interference unit |
| CN107328306A (en) * | 2017-06-21 | 2017-11-07 | 北京东远润兴科技有限公司 | A kind of low slow small flight equipment counter devices and methods therefor |
| CN107566079A (en) * | 2017-10-12 | 2018-01-09 | 深圳市吉赫兹电子有限公司 | The civilian unmanned plane of full frequency band flies control signal and accurately disturbs counter System and method for |
| 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 |
| CN109613554A (en) * | 2018-12-21 | 2019-04-12 | 成都航天科工微电子***研究院有限公司 | A kind of multiple target low altitude safe prevention and control system and method |
-
2016
- 2016-06-08 CN CN201620549621.XU patent/CN205666840U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106849965A (en) * | 2017-04-07 | 2017-06-13 | 北京智宇翔云科技有限公司 | A kind of aerial signal output circuit and interference unit |
| CN107328306A (en) * | 2017-06-21 | 2017-11-07 | 北京东远润兴科技有限公司 | A kind of low slow small flight equipment counter devices and methods therefor |
| 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 |
| CN107566079A (en) * | 2017-10-12 | 2018-01-09 | 深圳市吉赫兹电子有限公司 | The civilian unmanned plane of full frequency band flies control signal and accurately disturbs counter System and method for |
| CN109613554A (en) * | 2018-12-21 | 2019-04-12 | 成都航天科工微电子***研究院有限公司 | A kind of multiple target low altitude safe prevention and control system and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180719 Address after: 050000 platinum Road business 120, South Berlin Road, Xinhua District, Shijiazhuang, Hebei, 108-27 Patentee after: Hebei Qin Yin Technology Co.,Ltd. Address before: 050003 No. 97 Heping West Road, Qiaodong District, Shijiazhuang, Hebei Patentee before: Army Engineering University of PLA |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20191025 Address after: 050000 No. 97 Heping West Road, Xinhua District, Hebei, Shijiazhuang Patentee after: ARMY ENGINEERING University OF PLA Address before: 050000 platinum Road business 120, South Berlin Road, Xinhua District, Shijiazhuang, Hebei, 108-27 Patentee before: Hebei Qin Yin Technology Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161026 Termination date: 20200608 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |