CN107152895B - A kind of conformal radar survey height/global location set composite - Google Patents
A kind of conformal radar survey height/global location set composite Download PDFInfo
- Publication number
- CN107152895B CN107152895B CN201710476753.3A CN201710476753A CN107152895B CN 107152895 B CN107152895 B CN 107152895B CN 201710476753 A CN201710476753 A CN 201710476753A CN 107152895 B CN107152895 B CN 107152895B
- Authority
- CN
- China
- Prior art keywords
- height
- global positioning
- conformal
- radar
- antenna
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 16
- 230000010365 information processing Effects 0.000 claims description 3
- 238000011897 real-time detection Methods 0.000 abstract description 3
- 230000037452 priming Effects 0.000 abstract description 2
- 230000009466 transformation Effects 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009172 bursting Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
A kind of conformal radar survey height/global location set composite, height finding radar, global location and priming device are integrated in inside the taper nacelle of rocket projectile head, highly integrated, complete function whole parts are formed.Height finding radar is located at front end, in distance of the Trajectory-terminal booting real-time detection rocket projectile apart from ground, calculates elevation information by missile-borne host computer when reaching setting height, sends out time break in real time, can ignite warhead in desired height and range；Global location antenna is wrapped on the external component shell of height finding radar, and processing circuit is located at rearmost end, can realize the real-time navigation capability of trajectory.Set composite topology layout proposed by the present invention is reasonable, small, light-weight, function is strong, flexible and convenient to use.
Description
Technical field
The present invention relates to a kind of detection device of rocket missile guidanceization transformation, it is that a kind of survey is high, positions compound integrating device.
Background technology
Requirement of the modern war for weapon attack precision is higher and higher, and the drop point essence of existing a large amount of traditional rocket projectiles
Degree distribution is big, Kill capability is relatively low, also often accidentally injure it is not guilty, it is difficult to meet future war demand.Rocket projectile is guided
Its attack precision and Kill capability can be improved by changing transformation, reduced and accidentally injured the common people.Due to the limitation of the prior art, current guidance
Change transformation and be simply added into the limited amendment component of function, impact dispersion can be reduced to a certain extent, without having in real time
Positioning, real-time detection correct and the ability ignited in real time in real time, cannot meet truly precise guidance, accurately injure
Strike demand.
Invention content
In order to solve the deficiencies in the prior art, the present invention proposes that a kind of conformal radar surveys height/global location set composite,
The device is formed by existing mature technology and system set, is had detection, positioning and real-time detonation power, can preferably be solved
The problem of certainly improving strike accuracy in the transformation of rocket missile guidanceization.
The object of the invention to solve the technical problems is realized using following technical scheme.It proposes according to the present invention
A kind of conformal radar survey height/global location set composite, is mounted in the conformal head-shield 5 on rocket projectile head.The set composite packet
Include global positioning system conformal antenna 1, height finding radar antenna 2, height finding radar signal-processing board 3, global positioning signal processing board
4, which is wrapped on conformal head-shield 5 and the two is conformal；The height finding radar antenna 2 is located at
Front end, global positioning signal processing board 4 are located at rearmost end, and height finding radar signal-processing board 3 is located at height finding radar antenna 2, complete
Between ball positioning signal processing board 4；
For receiving global positioning signal, global positioning signal processing board 4 is used for the global positioning system conformal antenna 1
The processing and resolving of location information, the two matching use, and collectively constitute high dynamic global positioning system；
The height finding radar antenna 2 is for receiving and emitting signal, and height finding radar signal-processing board 3 is for elevation information
Processing and resolving, the two matching use, and collectively constitute height finding radar；
The height finding radar signal-processing board 3, global positioning signal processing board 4 are all connected with missile-borne host computer.
The object of the invention to solve the technical problems is also further realized using following technical measures.
Further, the height finding radar antenna 2 is installed on the inside of global positioning system conformal antenna 1, and the two makes
With not interfereing with each other.
By above-mentioned technical proposal, height finding radar, global location and priming device are integrated in rocket projectile head by the present invention
Inside taper nacelle, highly integrated, complete function whole parts are formed.Height finding radar is located at front end, is opened in Trajectory-terminal
Distance of the machine real-time detection rocket projectile apart from ground, elevation information is calculated when reaching setting height by missile-borne host computer, real
When send out time break, warhead can be ignited in desired height and range；Global location antenna is wrapped in height finding radar
On external component shell, processing circuit is located at rearmost end, can realize the real-time navigation capability of trajectory.
Set composite topology layout proposed by the present invention is reasonable, small, light-weight, function is strong, flexible and convenient to use.It is logical
Cross installation set composite, the latter end that can be effectively completed apart from height detecting, body real-time resolving and setting height send out
The function of going out to ignite warhead in real time, an effective solution scheme is provided for the distal probe and guidance of guided rocket bullet.
Above description is only the general introduction of technical solution of the present invention, in order to better understand the technical means of the present invention,
And can be implemented in accordance with the contents of the specification, and in order to allow the above and other objects, features and advantages of the present invention can
It is clearer and more comprehensible, it is special below to lift preferred embodiment, and coordinate attached drawing, detailed description are as follows.
Description of the drawings
Fig. 1 is the schematic diagram that a kind of conformal radar of the present invention surveys height/global location set composite.
【Main element symbol description】
1：Global positioning system conformal antenna
2：Height finding radar antenna
3：Height finding radar signal-processing board
4：Global positioning signal processing board
5：Conformal head-shield
Specific implementation mode
In conjunction with Fig. 1, the invention will be further described：
A kind of conformal radar of the present invention surveys height/global location set composite, is mounted on the conformal head-shield 5 on rocket projectile head
It is interior.The set composite includes global positioning system conformal antenna 1, height finding radar antenna 2, height finding radar signal-processing board 3, the whole world
Positioning signal processing board 4, which is wrapped on conformal head-shield 5 and the two is conformal；The survey is high
Radar antenna 2 is located at front end, global positioning signal processing board 4 is located at rearmost end, and height finding radar signal-processing board 3, which is located at, surveys height
Between radar antenna 2, global positioning signal processing board 4；
For receiving global positioning signal, global positioning signal processing board 4 is used for the global positioning system conformal antenna 1
The processing and resolving of location information, the two matching use, and collectively constitute high dynamic global positioning system；
The height finding radar antenna 2 is for receiving and emitting signal, and height finding radar signal-processing board 3 is for elevation information
Processing and resolving, the two matching use, and collectively constitute height finding radar；
The height finding radar signal-processing board 3, global positioning signal processing board 4 are all connected with missile-borne host computer.
Further, the height finding radar antenna 2 is installed on the inside of global positioning system conformal antenna 1, and the two makes
With not interfereing with each other.
The operation principle that a kind of conformal radar of the present invention surveys height/global location set composite is：
Whole device combination is mounted in the conformal head-shield in head 5, forms a highly integrated independent bay section, will detection,
It positions, survey high function set and be integrated.When using the device, rocket projectile head, global positioning system blanket insurance can be installed in
Shape antenna 1 and global positioning signal processing board 4 can position and resolve trajectory message in real time；2 launching beam of height finding radar antenna
Ground is detected, when echo-signal reaches the Height of setting, it is upper that height finding radar signal-processing board 3 is uploaded to missile-borne
Machine sends out time break by it, activates apparatus to cause bursting, ignites warhead.
The present invention does not limit the purposes of warhead, such as when the warhead of rocket projectile being changed to extinguishing chemical launching unit,
The rocket projectile is converted into long-range fire extinguisher bomb.
The above is only the preferred embodiment of patent of the present invention, any person skilled in the art, not
It is detached from the art of this patent aspects, any simple modification made to the above embodiment of the technical spirit according to this patent,
Equivalent variations and modification, in the range of still falling within the art of this patent scheme.
Claims (2)
1. a kind of conformal radar surveys height/global location set composite, it is characterised in that：The set composite is mounted on rocket projectile head
Conformal head-shield (5) in, including global positioning system conformal antenna (1), height finding radar antenna (2), height finding radar signal processing
Plate (3), global positioning signal processing board (4), the global positioning system conformal antenna (1) are wrapped on conformal head-shield (5) and two
Person is conformal；The height finding radar antenna (2) is located at front end, global positioning signal processing board (4) is located at rearmost end, surveys Gao Lei
It is located between height finding radar antenna (2), global positioning signal processing board (4) up to signal-processing board (3)；
For receiving global positioning signal, global positioning signal processing board (4) is used for the global positioning system conformal antenna (1)
The processing and resolving of location information, the two matching use, and collectively constitute high dynamic global positioning system；
The height finding radar antenna (2) is for receiving and emitting signal, and height finding radar signal-processing board (3) is for elevation information
Processing and resolving, the two matching use, and collectively constitute height finding radar；
The height finding radar signal-processing board (3), global positioning signal processing board (4) are all connected with missile-borne host computer.
2. a kind of conformal radar according to claim 1 surveys height/global location set composite, it is characterised in that：The survey
High radar antenna (2) is installed on the inside of global positioning system conformal antenna (1), and the use of the two is not interfere with each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710476753.3A CN107152895B (en) | 2017-06-21 | 2017-06-21 | A kind of conformal radar survey height/global location set composite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710476753.3A CN107152895B (en) | 2017-06-21 | 2017-06-21 | A kind of conformal radar survey height/global location set composite |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107152895A CN107152895A (en) | 2017-09-12 |
| CN107152895B true CN107152895B (en) | 2018-08-17 |
Family
ID=59796020
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710476753.3A Active CN107152895B (en) | 2017-06-21 | 2017-06-21 | A kind of conformal radar survey height/global location set composite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107152895B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017170B (en) * | 2019-12-30 | 2022-02-11 | 西安智荣机电科技有限公司 | High-efficient built-in antenna glider under water |
| CN111337921B (en) * | 2020-03-13 | 2022-04-26 | 成都金宇防务科技有限公司 | Missile-borne millimeter wave radar height measurement device to ground |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6779752B1 (en) * | 2003-03-25 | 2004-08-24 | Northrop Grumman Corporation | Projectile guidance with accelerometers and a GPS receiver |
| US8138982B1 (en) * | 2007-06-26 | 2012-03-20 | Rockwell Collins, Inc. | Munitions/artillery shell GPS multi-edge slot anti-jamming array |
| CN107529370B (en) * | 2011-03-31 | 2014-04-30 | 北京理工大学 | A kind of extreme low-altitude supersonic cruise target missile |
| CN104266555A (en) * | 2014-09-30 | 2015-01-07 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
| CN106025541A (en) * | 2016-07-12 | 2016-10-12 | 成都泰格微电子研究所有限责任公司 | Conformal spherical antenna array with good shielding effect |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2014214927A (en) * | 2013-04-24 | 2014-11-17 | 株式会社Ｉｈｉエアロスペース | Rocket ammunition and control method for the same |
-
2017
- 2017-06-21 CN CN201710476753.3A patent/CN107152895B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6779752B1 (en) * | 2003-03-25 | 2004-08-24 | Northrop Grumman Corporation | Projectile guidance with accelerometers and a GPS receiver |
| US8138982B1 (en) * | 2007-06-26 | 2012-03-20 | Rockwell Collins, Inc. | Munitions/artillery shell GPS multi-edge slot anti-jamming array |
| CN107529370B (en) * | 2011-03-31 | 2014-04-30 | 北京理工大学 | A kind of extreme low-altitude supersonic cruise target missile |
| CN104266555A (en) * | 2014-09-30 | 2015-01-07 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
| CN106025541A (en) * | 2016-07-12 | 2016-10-12 | 成都泰格微电子研究所有限责任公司 | Conformal spherical antenna array with good shielding effect |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107152895A (en) | 2017-09-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107152895B (en) | A kind of conformal radar survey height/global location set composite | |
| SE465389B (en) | AMMUNITION UNIT WITH ADAPTIVE FUNCTIONS TO PROMOTE THE HARDNESS OF A TARGET / TARGET PARTY | |
| US8120992B2 (en) | Method for finding range and bearing to underwater object | |
| US11906274B2 (en) | Reconnaissance and communication assembly | |
| CN207365828U (en) | A kind of inexpensive recombination laser influence fuse device of fusion distance and attitude information | |
| CN113406966A (en) | Unmanned aerial vehicle counter-braking method and unmanned aerial vehicle counter-braking system | |
| RU2527610C2 (en) | Two-stage antitank guided missile | |
| US6012393A (en) | Asymmetric penetration warhead | |
| RU2010118389A (en) | REACTIVE ANTI-BOAT APPARATUS (OPTIONS) | |
| DE102007049438B4 (en) | Method for the defense of ballistic missiles with the help of guided missiles | |
| CN108131989A (en) | A kind of repeatedly continuous driving formula depth Penetrating Warhead structure | |
| CN207881558U (en) | A kind of repeatedly continuous driving formula depth Penetrating Warhead structure | |
| KR101907799B1 (en) | Fuse and firing device using side jet and firing method thereof | |
| US4420129A (en) | Guided missile and fuze system therefor | |
| CN109357578A (en) | School shooting method is aimed at based on the calibration shell of Beidou navigation technology and artilleryman | |
| EP0760458B1 (en) | Asymmetric penetration warhead | |
| RU2356008C2 (en) | Contact explosive | |
| RU2681826C2 (en) | Unmanned missile strike system | |
| US10234255B2 (en) | Proximity fuze, and projectile provided with such a proximity fuze | |
| CN203163617U (en) | Novel bomb | |
| RU2566707C2 (en) | Adjustable mortar bomb | |
| RU183366U1 (en) | Mortar Mine | |
| CN202485567U (en) | Pre-split warhead | |
| CN103292638A (en) | Pre-splitting warhead | |
| RU2427789C2 (en) | Tverich-5 fragmentation-beam shell |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Liang Xiaogeng Inventor after: Liu Xudong Inventor after: Lv Zhao Inventor before: Liang Xiaogeng Inventor before: Liu Xudong Inventor before: Lv Zhao Inventor before: Chen Wenguo Inventor before: Liu Xiangdong Inventor before: Qi Erying Inventor before: Chen Zhengyuan Inventor before: Zhao Guoqiang |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 471000 China (Henan) Pilot Free Trade Zone Luoyang Area (High tech) Zhongdian Optics Valley (Luoyang) Digital Economy Industrial Park, Building 3, Building B, Floors 1-5 Patentee after: Henan Ruiji Intelligent Equipment Technology Co.,Ltd. Country or region after: China Address before: Room 078, 12th Floor, VIA Building, No. 29 Suzhou Street, Haidian District, Beijing 100089 Patentee before: BEIJING CLOUDTEK TECHNOLOGY CO.,LTD. Country or region before: China |