CN207763580U - Missile intercept system based on unmanned plane - Google Patents
Missile intercept system based on unmanned plane Download PDFInfo
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- CN207763580U CN207763580U CN201721755288.9U CN201721755288U CN207763580U CN 207763580 U CN207763580 U CN 207763580U CN 201721755288 U CN201721755288 U CN 201721755288U CN 207763580 U CN207763580 U CN 207763580U
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- missile
- unmanned plane
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- end radar
- defence line
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Abstract
The utility model is related to the missile intercept systems based on unmanned plane, including unmanned plane defence line, distal end radar, proximal end radar and monitoring center；The distal end radar is built up in the periphery easily to strike target from military affairs, and proximal end radar is built up at the military position that easily strikes target, and distal end radar is used to monitor the offensive missile of enemy, and proximal end radar is for monitoring interception guided missile；The bearing data library that offensive missile is easiest to strike is stored in the host of the monitoring center；The unmanned plane defence line includes multiple defence line units, it is densely arranged multiple defence line units in the orientation most easily hit, defence line unit includes multiple miniature drone, intercept net, multiple miniature drone play intercept net stay bolt, strong magnetic module and GPS positioning module have been installed in intercept net, coordinate setting module is installed, each locating module corresponds to a coordinate in miniature drone.The advantageous effect that the utility model reaches is：Registration, interception effect are good, safe.
Description
Technical field
The utility model is related to air vehicle technique fields, more particularly to the missile intercept system based on unmanned plane.
Background technology
There is maneuverability, rapid reaction, unmanned flight, operation to want for UAV, abbreviation unmanned plane (UAV)
Seek low advantage.Image real-time Transmission, high-risk areas detecting function may be implemented by carrying multiclass sensor in unmanned plane.
In missile intercept system, commonly using Electromagnetic Interference influences the positioning of guided missile, and guided missile is allowed to train off, but if surrounding has
When the common people, can only it hurt innocent persons in this way, therefore the mode for directly destroying guided missile in the air also occur, it is common
Mode is transmitting interception guided missile, and interception guided missile distance objective certain distance after-explosion is released shrapnel, hit by shrapnel
Target, but the guided missile for having can not still destroy, and also still there are many shrapnels to fall through, and these not quick-fried bombs are fallen on
When in soil, it is difficult to remove one by one, harmful effect is caused to safety later.
Utility model content
The shortcomings that the purpose of the utility model is to overcome the prior arts, provides that registration, interception effect be good, safety
The high missile intercept system based on unmanned plane.
The purpose of this utility model is achieved through the following technical solutions：Missile intercept system based on unmanned plane, including
Unmanned plane defence line, distal end radar, proximal end radar and monitoring center；
The distal end radar is built up in the periphery easily to strike target from military affairs, and proximal end radar is built up in military easily strike mesh
At cursor position, distal end radar is used to monitor the offensive missile of enemy, and proximal end radar is for monitoring interception guided missile；
The bearing data library that offensive missile is easiest to strike is stored in the host of the monitoring center；
The unmanned plane defence line includes multiple defence line units, and it is single to be densely arranged multiple defence lines in the orientation most easily hit
Member, the defence line unit include multiple miniature drone, intercept net, and multiple miniature drone play intercept net stay bolt, intercept
Strong magnetic module and GPS positioning module have been installed on the net, coordinate setting module, Mei Geding are installed in the miniature drone
Position module corresponds to a coordinate, and locating alarming module is provided at monitoring center, the locating alarming module and interception guided missile
Control unit is electrically connected；
When the target of the coordinate setting module substantial deviation in miniature drone itself, then explanation has guided missile to fly over, and blocks
The control unit for cutting guided missile emits interception guided missile towards the orientation.
The strong magnetic module is adsorbed on offensive missile, and GPS positioning module Induct and interception guided missile is collided with offensive missile.
The corresponding position that the bearing data library is not stored with most pregnable bearing data is provided with shrapnel transmitting
Equipment.
Data in the bearing data library are got by analogue simulation system, and analogue simulation system includes military easy
The intensity for all directions that strike target, the rupture factor of the common guided missile of enemy, the common flight strike tactical data of enemy.
Data in the bearing data library are also corrected by air battle combat practice simulator.
The utility model has the following advantages：By being arranged unmanned plane defence line, especially strong magnetic module, intercept net and miniature
The setting of machine can effectively destroy offensive missile；Strong magnetic module can be adsorbed on offensive missile, GPS locator energy
Offensive missile is accurately positioned, even and if falling and will not lead to subsequent safety problem.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of defence line unit.
Specific implementation mode
The utility model is further described below in conjunction with the accompanying drawings, but the scope of protection of the utility model is not limited to
It is as described below.
As shown in Figure 1, the missile intercept system based on unmanned plane, including unmanned plane defence line 1, distal end radar 2, proximal end radar
3 and monitoring center 4；
The distal end radar 2 is built up in the periphery easily to strike target from military affairs, and proximal end radar is built up in military easily strike
Target location, distal end radar 2 are used to monitor the offensive missile of enemy, and proximal end radar 3 is for monitoring interception guided missile；
The monitoring center 4 is located in easy strike target, and is stored with offensive missile in the host of monitoring center 4 and is easiest to
The bearing data library of strike；
The unmanned plane defence line 1 includes multiple defence line units 5, and multiple defence lines are densely arranged in the orientation most easily hit
Unit 5, the defence line unit include multiple miniature drone 6, intercept net 7, and multiple miniature drone 6 are by 7 stay bolt of intercept net
It rises, strong magnetic module 8 and GPS positioning module 9 has been installed in intercept net 7, coordinate setting is installed in the miniature drone 6
Module, each locating module correspond to a coordinate, locating alarming module are provided at monitoring center, the locating alarming module with
The control unit of interception guided missile is electrically connected；
When the target of the coordinate setting module substantial deviation in miniature drone 6 itself, then explanation has guided missile to fly over, and blocks
The control unit for cutting guided missile emits interception guided missile towards the orientation.
In the present embodiment, the strong magnetic module 8 is adsorbed on offensive missile, 9 Induct and interception guided missile of GPS positioning module with
Offensive missile collides.
Further, the bearing data library is not stored with the corresponding position of most pregnable bearing data and is provided with son
Female bullet emits equipment.
In the present embodiment, the data in the bearing data library are got by analogue simulation system, analogue simulation system
Include the military intensity of all directions that easily strikes target, the rupture factor of the common guided missile of enemy, the common flight strike campaign of enemy
Art data.
Further, the data in the bearing data library are also corrected by air battle combat practice simulator.
Claims (5)
1. the missile intercept system based on unmanned plane, it is characterised in that：Including unmanned plane defence line, distal end radar, proximal end radar and
Monitoring center；
The distal end radar is built up in the periphery easily to strike target from military affairs, and proximal end radar is built up in the military position that easily strikes target
Place is set, distal end radar is used to monitor the offensive missile of enemy, and proximal end radar is for monitoring interception guided missile；
The bearing data library that offensive missile is easiest to strike is stored in the host of the monitoring center；
The unmanned plane defence line includes multiple defence line units, and multiple defence line units are densely arranged in the orientation most easily hit,
The defence line unit includes multiple miniature drone, intercept net, and multiple miniature drone play intercept net stay bolt, in intercept net
Strong magnetic module and GPS positioning module are installed, coordinate setting module, each locating module are installed in the miniature drone
A corresponding coordinate, is provided with locating alarming module, the control list of the locating alarming module and interception guided missile at monitoring center
Member electrical connection；
When the target of the coordinate setting module substantial deviation in miniature drone itself, then explanation has guided missile to fly over, and interception is led
The control unit of bullet emits interception guided missile towards the orientation.
2. the missile intercept system according to claim 1 based on unmanned plane, it is characterised in that：The strong magnetic module is inhaled
It is attached on offensive missile, GPS positioning module Induct and interception guided missile is collided with offensive missile.
3. the missile intercept system according to claim 2 based on unmanned plane, it is characterised in that：The bearing data library
The corresponding position for not being stored with most pregnable bearing data is provided with shrapnel transmitting equipment.
4. the missile intercept system according to claim 1 based on unmanned plane, it is characterised in that：The bearing data library
In data got by analogue simulation system, analogue simulation system include the military all directions that easily strike target intensity,
The rupture factor of the common guided missile of enemy, the common flight strike tactical data of enemy.
5. the missile intercept system according to claim 4 based on unmanned plane, it is characterised in that：The bearing data library
In data also corrected by air battle combat practice simulator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721755288.9U CN207763580U (en) | 2017-12-15 | 2017-12-15 | Missile intercept system based on unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721755288.9U CN207763580U (en) | 2017-12-15 | 2017-12-15 | Missile intercept system based on unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207763580U true CN207763580U (en) | 2018-08-24 |
Family
ID=63187062
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721755288.9U Active CN207763580U (en) | 2017-12-15 | 2017-12-15 | Missile intercept system based on unmanned plane |
Country Status (1)
| Country | Link |
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| CN (1) | CN207763580U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113091513A (en) * | 2021-03-03 | 2021-07-09 | 上海机电工程研究所 | Real-time dynamic calibration method, system and medium for ship-based missile weapon system |
| CN115342689A (en) * | 2022-08-12 | 2022-11-15 | 广州海洋地质调查局 | Quick interference and maneuvering destruction method for sea battlefield enemy reconnaissance system |
| CN115355763A (en) * | 2022-08-26 | 2022-11-18 | 陈长仁 | Military defense type interception system |
-
2017
- 2017-12-15 CN CN201721755288.9U patent/CN207763580U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113091513A (en) * | 2021-03-03 | 2021-07-09 | 上海机电工程研究所 | Real-time dynamic calibration method, system and medium for ship-based missile weapon system |
| CN113091513B (en) * | 2021-03-03 | 2023-02-28 | 上海机电工程研究所 | Real-time dynamic calibration method, system and medium for ship-based missile weapon system |
| CN115342689A (en) * | 2022-08-12 | 2022-11-15 | 广州海洋地质调查局 | Quick interference and maneuvering destruction method for sea battlefield enemy reconnaissance system |
| CN115355763A (en) * | 2022-08-26 | 2022-11-18 | 陈长仁 | Military defense type interception system |
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