CN208477380U - 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
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- CN208477380U CN208477380U CN201821237726.7U CN201821237726U CN208477380U CN 208477380 U CN208477380 U CN 208477380U CN 201821237726 U CN201821237726 U CN 201821237726U CN 208477380 U CN208477380 U CN 208477380U
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- unmanned air
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- emission system
- air vehicle
- military unmanned
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Abstract
The utility model 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.Tthe utility model 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 utility model belongs to military issue weapons equipment field, be related to it is a kind of specifically for military unmanned air vehicle threaten control be
System.
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.
Utility model content
In view of the above-mentioned problems, the utility model provides a kind of military unmanned air vehicle threat managing and control system, it is therefore an objective to can make to grasp
Make unmanned plane counter weapon of the personnel far from high radiation, still with fine sight and unmanned plane threat can be broken through, and can grow
Continuation of the journey uses.
To achieve the above object, the utility model provides the following technical solutions:
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 the one aspect of the utility model, the individual soldier portable controls attitude transducer built in emission system and has
Line or wireless communication module, attitude transducer acquire the level and pitch angle information of individual soldier portable control emission system, lead to
Wired or wireless communication module is crossed to send to the turret systems.
According to the one aspect of the utility model, the turret systems are clouds terrace system, and pitch angle is adjustable, horizontal direction angle
It is adjustable, it is equipped with fixed angle and limits.
According to the one aspect of the utility model, host built in the turret systems and with wired or wireless communication module,
Wired or wireless communication module receives level and pitch angle information from individual soldier portable control emission system, passes through host
Control level and pitch angle that the turret systems move to setting.
According to the one aspect of the utility model, the counter emission system passes through interference signal mode or catching net or big gun
Bullet mode controls unmanned plane；When using interference signal mode, the counter emission system is that high-gain wide-angle is anti-
Antenna processed, counter antenna use powerful counter mould group；When using net mode is captured, the counter emission system is net
Rifle；When using shell mode, the counter emission system is magnetic artillery.
According to the one aspect of the utility model, the counter flat pad can haulage vehicle loading or the installation of position formula.
Compared with prior art, the utility model has the beneficial effects that
The system for threatening control designed for military unmanned air vehicle of the utility model, including separate unit or three Taiwan army's nothings
Man-machine control linkage turntable and an individual soldier portable control emission system；Military unmanned air vehicle control linkage turret systems, turntable
Pitch angle, horizontal direction angle is adjustable, is equipped with fixed angle and limits；It breaks through antenna and selects high-gain wide-angle antenna, horizontal angle
Degree 180 degree, 120 degree of vertical angle, using powerful counter mould group；Individual soldier portable controls emission system, and built-in posture passes
Sensor IMU can acquire individual soldier's level and pitch angle information, input to linkage turntable, and trigger is detained, and be emitted；Linkage
Turntable can receive the sensing level and pitch angle of individual soldier's emission system, and active response is horizontally diverted and pitching operates, and is received
To firing order, transmitting；This system can haulage vehicle load or the installation of position formula, operator be in system middle position, turn
Platform is limited equipped with physics, guarantees not radiate National People's Congress's area.
In addition, the utility model breaks through flat pad and the separation of hand-held launch control system, hand-held individual soldier due to ground
Hand-held 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
The requirement that do not carry can directly power from ground or vehicle, therefore power-on time can accomplish to grow very much, realize Gao Xu
Boat.
Detailed description of the invention
Fig. 1 is the stereoscopic schematic diagram of the first embodiment of the utility model.
Fig. 2 is the schematic top plan view of the first embodiment of the utility model.
Fig. 3 is the partial enlarged view of Fig. 1.
Fig. 4 is the Composition and control of system schematic diagram of the utility model.
Fig. 5 is the stereoscopic schematic diagram of second of embodiment of the utility model.
Fig. 6 is the stereoscopic schematic diagram of the third embodiment of the utility model.
Specific embodiment
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
Every other embodiment obtained, fall within the protection scope of the utility model.
[embodiment one]
As shown in Figure 1 to Figure 3, the military unmanned air vehicle of the utility model threatens managing and control system, by counter flat pad 1 and list
Soldier's hand-held controls emission system 2 and forms, and counter flat pad 1 is by three military unmanned air vehicle control linkages turntable 1A, 1B, 1C
Composition, the installation of position formula, the control linkage of three military unmanned air vehicles turntable 1A, 1B, 1C in the horizontal plane with 3 equidistant placements from
And 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 anti-
The sky of one of the central point trisection of flat pad 1 processed.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
Be after the sighted direction of individual soldier portable control emission system 2 determines, the same time only with one in corresponding control range
Military unmanned air vehicle control linkage turntable linkage.Military unmanned air vehicle control linkage turntable 1A, 1B, 1C include turret systems 3 and counter
Emission system 4, wherein turret systems 3 and the sighted direction of individual soldier portable control emission system 2 link, and break through emission system 4
It links with the transmitting trigger of individual soldier portable control 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, the military unmanned air vehicle of the utility model 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 managed linkage turntable 1D by separate unit military unmanned air vehicle and formed, position
Formula installation, the advantage of this scheme is may be mounted on pillar or shelf, and height is adjustable, separate unit military unmanned air vehicle control connection
Turn 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 transmitting
Near platform 1, individual soldier portable control emission system 2 and counter flat pad 1 are located in the plane of different height, are normally at
The lower section of flat pad 1 is broken through, to avoid its coverage area, by wired or wirelessly manage and join with military unmanned air vehicle
Turn platform 1D linkage.Remaining is the same as example 1.
[embodiment three]
As shown in figure 5, the military unmanned air vehicle of the utility model 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 managed linkage turntable 1E by separate unit military unmanned air vehicle and formed, by transporting
Defeated vehicle loading, the advantage of this scheme are that mobility is good.Remaining is identical as embodiment two.
The application method and working principle of the utility model are as follows: by taking embodiment one as an example, operator holds individual soldier's hand
It holds formula control emission system 2 and is in counter 1 middle position of flat pad, individual soldier portable controls posture built in emission system 2 and passes
Sensor 201 can acquire individual soldier's level and pitch angle information, input to counter flat pad 1 by wired or wireless communication
Military unmanned air vehicle control linkage turntable 1A turret systems 3 (assuming that at this time individual soldier portable control emission system 2 direction be
The range of military unmanned air vehicle control linkage turntable 1A), trigger is detained, the counter on linkage military unmanned air vehicle control linkage turntable 1A
Emission system 4 is emitted；Turret systems 3 can receive the sensing level and pitch angle of individual soldier portable control emission system 2
Degree, active response is horizontally diverted to be operated with pitching；Counter emission system 4 receives firing order and is emitted；Counter transmitting is flat
Platform 1 is loaded by haulage vehicle or position formula is installed, and turntable is equipped with physics and limits, and makes operator far from breaking through weapon, and anti-
Weapon processed does not contact, and 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 utility model is not limited to here
Embodiment, those skilled in the art's announcement according to the present utility model, do not depart from improvement that the utility model scope is made and
Modification should be all within the protection scope of the utility model.
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 |
|---|---|---|---|
| CN201821237726.7U CN208477380U (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 |
|---|---|---|---|
| CN201821237726.7U CN208477380U (en) | 2018-08-01 | 2018-08-01 | A kind of military unmanned air vehicle threat managing and control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208477380U true CN208477380U (en) | 2019-02-05 |
Family
ID=65208081
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821237726.7U Active CN208477380U (en) | 2018-08-01 | 2018-08-01 | A kind of military unmanned air vehicle threat managing and control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208477380U (en) |
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2018
- 2018-08-01 CN CN201821237726.7U patent/CN208477380U/en active Active
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