CN109164818A - A kind of military unmanned air vehicle threat managing and control system - Google Patents
A kind of military unmanned air vehicle threat managing and control system Download PDFInfo
- Publication number
- CN109164818A CN109164818A CN201810866972.7A CN201810866972A CN109164818A CN 109164818 A CN109164818 A CN 109164818A CN 201810866972 A CN201810866972 A CN 201810866972A CN 109164818 A CN109164818 A CN 109164818A
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- unmanned air
- control
- emission system
- air vehicle
- counter
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- 238000009434 installation Methods 0.000 claims abstract description 6
- 238000004891 communication Methods 0.000 claims description 13
- 239000000178 monomer Substances 0.000 claims description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 230000005855 radiation Effects 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
- 244000144985 peep Species 0.000 description 1
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Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of military unmanned air vehicles to threaten managing and control system, emission system is controlled including counter flat pad and individual soldier portable, counter flat pad is made of separate unit or more military unmanned air vehicle control linkage turntables, the middle position that individual soldier portable control emission system be in separate unit counter flat pad Different Plane perhaps more military unmanned air vehicles control linkage turntable passes through wired or wirelessly manage linkage turntable with military unmanned air vehicle and link；Military unmanned air vehicle control linkage turntable includes turret systems and counter emission system, controls sighted direction and the transmitting trigger linkage of emission system with individual soldier portable respectively.Present system can haulage vehicle load or position formula installation, operator does not contact with counter weapon, National People's Congress's area will not be radiated, it is hand-held the light-weight of emission system, small power consumption, radiationless, and big power consumption, there is the counter flat pad of radiation directly to power from ground or vehicle, power-on time is long, realizes high continuation of the journey.
Description
Technical field
The invention belongs to military issue weapons equipment fields, are related to a kind of system for threatening control specifically for military unmanned air vehicle.
Background technique
With the maturation of unmanned air vehicle technique, it is all kinds of it is relevant to unmanned plane eavesdrop, peep, smuggling offences and hostile army
Thing frequent activity occurs, and in order to prevent unmanned plane from carrying out crime or military activity, it is existing to prevent from entering using unmanned plane occasion
Field and the airport with stringent no-fly zone, military key area.It preferably ensures the information security in special area, forms safety
Space, the managing and control system that anti-unmanned plane threatens all is popular research at present in the whole world.The prior art is generally using big
The counter mould group of power or unmanned plane air crash out of control is made by magnetic artillery etc., problem is that these counter weapons have mostly
Very strong radiation, directly using for the healthy and safe unfavorable of operator.Another problem is the function of original handheld launch
Consumption is very big, and the battery for breaking through weapon is not durable.
Summary of the invention
In view of the above-mentioned problems, the present invention provides a kind of military unmanned air vehicle threat managing and control system, it is therefore an objective to operator can be made
Member breaks through weapon far from the unmanned plane of high radiation, still with fine sight and can break through unmanned plane and threatens, and can grow continuation of the journey
It uses.
To achieve the above object, the invention provides the following technical scheme:
A kind of military unmanned air vehicle threat managing and control system, it is characterised in that: including the counter flat pad mutually separated and individual soldier
Hand-held controls emission system, and the counter flat pad is made of separate unit or more military unmanned air vehicle control linkage turntables；
When for separate unit, the control range of the separate unit military unmanned air vehicle control linkage turntable monomer covering horizontal 360-degree；When being more
When, the more military unmanned air vehicles control linkage turntable collectively covers the control range of horizontal 360-degree；The individual soldier portable control
Emission system processed and separate unit military unmanned air vehicle control linkage turntable are in the plane of different height, or are in described more
Military unmanned air vehicle control linkage turntable middle position, by it is wired or wirelessly with military unmanned air vehicle control linkage turn
Platform linkage；After the sighted direction of individual soldier portable control emission system determines, the same time only manages range with corresponding
Interior military unmanned air vehicle control linkage turntable linkage；Every military unmanned air vehicle control linkage turntable includes turret systems and anti-
Emission system processed, wherein the turret systems and the sighted direction of individual soldier portable control emission system link, it is described anti-
The transmitting trigger of emission system processed and individual soldier portable control emission system links.
According to one aspect of the present invention, attitude transducer built in individual soldier portable control emission system and it is wired or
Wireless communication module, attitude transducer acquires the level and pitch angle information of individual soldier portable control emission system, by having
Line or wireless communication module are sent to the turret systems.
According to one aspect of the present invention, the turret systems are clouds terrace system, and pitch angle is adjustable, and horizontal direction angle can
It adjusts, is equipped with fixed angle and limits.
According to one aspect of the present invention, host built in the turret systems and with wired or wireless communication module, it is wired
Or wireless communication module receives level and pitch angle information from individual soldier portable control emission system, is controlled by host
The turret systems move to the level and pitch angle of setting.
According to one aspect of the present invention, the counter emission system passes through interference signal mode or catching net or shell side
Formula controls unmanned plane；When using interference signal mode, the counter emission system is that high-gain wide-angle breaks through day
Line, counter antenna use powerful counter mould group；When using net mode is captured, the counter emission system is net rifle；When
When using shell mode, the counter emission system is magnetic artillery.
According to one aspect of the present invention, the counter flat pad can haulage vehicle loading or the installation of position formula.
Compared with prior art, the beneficial effects of the present invention are:
The system for threatening control designed for military unmanned air vehicle of the invention, including separate unit or three military unmanned air vehicles
Control linkage turntable and an individual soldier portable control emission system；Military unmanned air vehicle control linkage turret systems, turntable pitching
Angle, horizontal direction angle is adjustable, is equipped with fixed angle and limits；It breaks through antenna and selects high-gain wide-angle antenna, level angle 180
Degree, 120 degree of vertical angle, using powerful counter mould group；Individual soldier portable controls emission system, built-in attitude transducer
IMU can acquire individual soldier's level and pitch angle information, input to linkage turntable, and trigger is detained, and be emitted；Link turntable
It can receive the sensing level and pitch angle of individual soldier's emission system, active response is horizontally diverted to be operated with pitching, receives hair
Instruction is penetrated, is emitted；This system can haulage vehicle load or the installation of position formula, operator is in system middle position, and turntable is set
There is physics limit, guarantees not radiate National People's Congress's area.
In addition, the present invention is since ground breaks through flat pad and the separation of hand-held launch control system, hand-held individual soldier is hand-held
Formula controls the light-weight of emission system, power consumption very little, radiationless, and the ground counter flat pad for having radiation of big power consumption does not have
The requirement of carrying can directly power from ground or vehicle, therefore power-on time can accomplish to grow very much, realize high continuation of the journey.
Detailed description of the invention
Fig. 1 is the stereoscopic schematic diagram of the first embodiment of the invention.
Fig. 2 is the schematic top plan view of the first embodiment of the invention.
Fig. 3 is the partial enlarged view of Fig. 1.
Fig. 4 is Composition and control of system schematic diagram of the invention.
Fig. 5 is the stereoscopic schematic diagram of second of embodiment of the invention.
Fig. 6 is the stereoscopic schematic diagram of the third embodiment of the invention.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that 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 shall fall within the protection scope of the present invention.
[embodiment one]
As shown in Figure 1 to Figure 3, military unmanned air vehicle of the invention threatens managing and control system, by counter flat pad 1 and individual soldier's hand
It holds formula control emission system 2 to form, counter flat pad 1 is by three military unmanned air vehicle control linkage turntable 1A, 1B, 1C groups
At the installation of, position formula, three military unmanned air vehicles control linkages turntable 1A, 1B, 1C in the horizontal plane with 3 equidistant placements to
The control range of horizontal 360-degree is collectively covered, the control range of military unmanned air vehicle control linkage turntable 1A, 1B, 1C are with counter
The sky of one of the central point trisection of flat pad 1.Individual soldier portable controls emission system 2 and is in counter flat pad 1
Middle position, by it is wired or wirelessly with control linkage turntable 1A, 1B, 1C linkage of three military unmanned air vehicles；But
After the sighted direction of individual soldier portable control emission system 2 determines, the same time only with the Taiwan army in corresponding control range
Linkage turntable linkage is managed with unmanned plane.Military unmanned air vehicle control linkage turntable 1A, 1B, 1C include turret systems 3 and counter hair
Penetrate system 4, wherein turret systems 3 and individual soldier portable control emission system 2 sighted direction link, counter emission system 4 with
Individual soldier portable controls the transmitting trigger linkage of emission system 2.
As shown in figure 4, attitude transducer 201 and wired or wireless communication mould built in individual soldier portable control emission system 2
Block 202, attitude transducer 201 acquire the level and pitch angle information of individual soldier portable control emission system 2, by wired or
Wireless communication module 202 is sent to turret systems 3.
Turret systems 3 include clouds terrace system 301, and pitch angle is adjustable, and horizontal direction angle is adjustable, are equipped with fixed angle and limit.
Host 302 built in turret systems 3 and with wired or wireless communication module 303, wired or wireless communication module 303 receives from single
Soldier's hand-held control emission system 2 level and pitch angle information, by host 302 control clouds terrace system 301 move to
Acquire the level and pitch angle that individual soldier portable control emission system 2 is set.
The transmitting trigger 203 for breaking through emission system 4 and individual soldier portable control emission system 2 links, and breaks through emission system 4
Unmanned plane is controlled by interference signal mode or catching net or shell mode；When using interference signal mode, counter
Emission system 4 is that high-gain wide-angle breaks through antenna 401, and the counter range for breaking through antenna is level angle 180 degree, vertical angle
120 degree, using powerful counter mould group；When using net mode is captured, counter emission system 4 is net rifle 402；When using big gun
When bullet mode, the counter emission system 4 is magnetic artillery 403.
[embodiment two]
As shown in figure 5, military unmanned air vehicle of the invention threatens managing and control system, by counter flat pad 1 and individual soldier portable
It controls emission system 2 to form, counter flat pad 1 is managed linkage turntable 1D by separate unit military unmanned air vehicle and formed, position formula peace
Dress, the advantage of this scheme is may be mounted on pillar or shelf, and height is adjustable, and separate unit military unmanned air vehicle control linkage turns
Platform 1D covers the control range of horizontal 360-degree in the horizontal plane, and individual soldier portable controls emission system 2 and is in counter flat pad
Near 1, individual soldier portable control emission system 2 and counter flat pad 1 are located in the plane of different height, are normally at counter
The lower section of flat pad 1, to avoid its coverage area, by wired or wirelessly turn with military unmanned air vehicle control linkage
Platform 1D linkage.Remaining is the same as example 1.
[embodiment three]
As shown in figure 5, military unmanned air vehicle of the invention threatens managing and control system, by counter flat pad 1 and individual soldier portable
It controls emission system 2 to form, counter flat pad 1 is managed linkage turntable 1E by separate unit military unmanned air vehicle and formed, by transport vehicle
Load, the advantage of this scheme is that mobility is good.Remaining is identical as embodiment two.
Application method and working principle of the invention is as follows: by taking embodiment one as an example, operator holds individual soldier portable
It controls emission system 2 and is in counter 1 middle position of flat pad, individual soldier portable controls attitude transducer built in emission system 2
201, individual soldier's level and pitch angle information can be acquired, the army of counter flat pad 1 is inputed to by wired or wireless communication
The turret systems 3 of linkage turntable 1A are managed (assuming that the direction of the emission system 2 of individual soldier portable control at this time is military with unmanned plane
The range of unmanned plane control linkage turntable 1A), trigger is detained, the counter transmitting on linkage military unmanned air vehicle control linkage turntable 1A
System 4 is emitted；Turret systems 3 can receive the sensing level and pitch angle of individual soldier portable control emission system 2, main
Dynamic response is horizontally diverted to be operated with pitching；Counter emission system 4 receives firing order and is emitted；It is logical to break through flat pad 1
Cross haulage vehicle load or position formula installation, turntable be equipped with physics limit, make operator far from counter weapon, with break through weapon
It does not contact, guarantee will not radiate National People's Congress's area.
It can understand the above description of the embodiments is intended to facilitate those skilled in the art and apply this specially
Benefit.Person skilled in the art obviously easily can make various modifications to these embodiments, and described herein
General Principle is applied in other embodiments without having to go through creative labor.Therefore, the present invention is not limited to implementations here
Example, those skilled in the art's announcement according to the present invention, improvement and modification made without departing from the scope of the present invention all should be
Within protection scope of the present invention.
Claims (6)
1. a kind of military unmanned air vehicle threatens managing and control system, it is characterised in that: including the counter flat pad and individual soldier's hand mutually separated
Formula control emission system is held, the counter flat pad is made of separate unit or more military unmanned air vehicle control linkage turntables；When
When for separate unit, the control range of the separate unit military unmanned air vehicle control linkage turntable monomer covering horizontal 360-degree；When being more
When, the more military unmanned air vehicles control linkage turntable collectively covers the control range of horizontal 360-degree；The individual soldier portable control
Emission system processed and separate unit military unmanned air vehicle control linkage turntable are in the plane of different height, or are in described more
Military unmanned air vehicle control linkage turntable middle position, by it is wired or wirelessly with military unmanned air vehicle control linkage turn
Platform linkage；After the sighted direction of individual soldier portable control emission system determines, the same time only manages range with corresponding
Interior military unmanned air vehicle control linkage turntable linkage；Every military unmanned air vehicle control linkage turntable includes turret systems and anti-
Emission system processed, wherein the turret systems and the sighted direction of individual soldier portable control emission system link, it is described anti-
The transmitting trigger of emission system processed and individual soldier portable control emission system links.
2. military unmanned air vehicle according to claim 1 threatens managing and control system, it is characterised in that: the individual soldier portable control
Attitude transducer built in emission system and wired or wireless communication module, attitude transducer acquire individual soldier portable control transmitting system
The level and pitch angle information of system, are sent by wired or wireless communication module to the turret systems.
3. military unmanned air vehicle according to claim 1 threatens managing and control system, it is characterised in that: the turret systems are holder
System, pitch angle is adjustable, and horizontal direction angle is adjustable, is equipped with fixed angle and limits.
4. military unmanned air vehicle according to claim 1 threatens managing and control system, it is characterised in that: main built in the turret systems
Machine and with wired or wireless communication module, wired or wireless communication module receives the water from individual soldier portable control emission system
Gentle pitch angle information controls the level and pitch angle that the turret systems move to setting by host.
5. military unmanned air vehicle according to claim 1 threatens managing and control system, it is characterised in that: the counter emission system is logical
It crosses interference aspect or catching net or shell mode controls unmanned plane；It is described anti-when using interference signal mode
Emission system processed is that high-gain wide-angle breaks through antenna, and counter antenna uses powerful counter mould group；When using catching net side
When formula, the counter emission system is net rifle；When using shell mode, the counter emission system is magnetic artillery.
6. military unmanned air vehicle according to claim 1 threatens managing and control system, it is characterised in that: the counter flat pad can
Haulage vehicle loads or the installation of position formula.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810866972.7A CN109164818A (en) | 2018-08-01 | 2018-08-01 | A kind of military unmanned air vehicle threat managing and control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810866972.7A CN109164818A (en) | 2018-08-01 | 2018-08-01 | A kind of military unmanned air vehicle threat managing and control system |
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| Publication Number | Publication Date |
|---|---|
| CN109164818A true CN109164818A (en) | 2019-01-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810866972.7A Pending CN109164818A (en) | 2018-08-01 | 2018-08-01 | A kind of military unmanned air vehicle threat managing and control system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109737818A (en) * | 2019-01-30 | 2019-05-10 | 纪伯文 | A kind of portable anti-unmanned machine equipment |
| CN111769898A (en) * | 2020-09-02 | 2020-10-13 | 长沙北斗产业安全技术研究院有限公司 | Method and system for defending unmanned aerial vehicle |
-
2018
- 2018-08-01 CN CN201810866972.7A patent/CN109164818A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109737818A (en) * | 2019-01-30 | 2019-05-10 | 纪伯文 | A kind of portable anti-unmanned machine equipment |
| CN111769898A (en) * | 2020-09-02 | 2020-10-13 | 长沙北斗产业安全技术研究院有限公司 | Method and system for defending unmanned aerial vehicle |
| CN111769898B (en) * | 2020-09-02 | 2020-12-01 | 长沙北斗产业安全技术研究院有限公司 | Method and system for defending unmanned aerial vehicle |
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Application publication date: 20190108 |