CN107152895A - A kind of conformal radar surveys height/global location set composite - Google Patents
A kind of conformal radar surveys height/global location set composite Download PDFInfo
- Publication number
- CN107152895A CN107152895A CN201710476753.3A CN201710476753A CN107152895A CN 107152895 A CN107152895 A CN 107152895A CN 201710476753 A CN201710476753 A CN 201710476753A CN 107152895 A CN107152895 A CN 107152895A
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- Prior art keywords
- height
- global positioning
- conformal
- antenna
- radar
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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
Abstract
A kind of conformal radar surveys height/global location set composite, and height finding radar, global location and priming device are integrated in inside rocket projectile head taper nacelle, forms highly integrated, complete function whole parts.Height finding radar is located at foremost, starts shooting real-time detection rocket projectile apart from the distance on ground in Trajectory-terminal, calculates elevation information by missile-borne host computer when reaching setting height, time break is sent in real time, can ignite warhead in desired height and scope；Global location antenna is wrapped on the external component housing of height finding radar, and process circuit is located at rearmost end, can realize the real-time navigation capability of trajectory.Set composite topology layout proposed by the present invention rationally, small volume, lightweight, function it 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
Modern war is for the requirement more and more higher of weapon attack precision, and the drop point of existing a large amount of traditional rocket projectiles essence
Degree distribution is big, Kill capability is relatively low, also often accidentally injures not guilty, it is difficult to meet future war demand.Guided for rocket projectile
Its attack precision and Kill capability can be improved by changing transformation, reduced and accidentally injured the common people.Due to the limitation of 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 possessing in real time
Positioning, real-time detection, correct in real time and the ability ignited in real time, it is impossible to meet truly precise guidance, accurately injure
Strike demand.
The content of the invention
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 possessed 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.According to proposed by the present invention
A kind of conformal radar surveys height/global location set composite, in the conformal head-shield 5 on rocket projectile head.The set composite bag
Include global positioning system conformal antenna 1, height finding radar antenna 2, height finding radar signal-processing board 3, global positioning signal process plate
4, the global positioning system conformal antenna 1 is wrapped on conformal head-shield 5 and the two is conformal；The height finding radar antenna 2 is located at
Foremost, global positioning signal process plate 4 is 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 process plate 4；
The global positioning system conformal antenna 1 is used to receive global positioning signal, and global positioning signal process plate 4 is used for
The processing and resolving of location information, the two matching are used, and collectively constitute high dynamic global positioning system；
The height finding radar antenna 2 is used to receive and transmission signal, and height finding radar signal-processing board 3 is used for elevation information
Processing and clearing, the two matching are used, and collectively constitute height finding radar；
The height finding radar signal-processing board 3, global positioning signal process plate 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 foremost, is opened in Trajectory-terminal
Machine real-time detection rocket projectile calculates elevation information when reaching setting height apart from the distance on ground by missile-borne host computer, real
When send time break, warhead can be ignited in desired height and scope；Global location antenna is wrapped in height finding radar
On external component housing, process circuit is located at rearmost end, can realize the real-time navigation capability of trajectory.
Set composite topology layout proposed by the present invention rationally, small volume, lightweight, function it 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 settlement and setting height send out
Go out to ignite the function of warhead in real time, an effective solution is provided for the distal probe and guidance of guided rocket bullet.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention,
And can be practiced according to the content of specification, and in order to allow the above and other objects, features and advantages of the present invention can
Become apparent, below especially exemplified by preferred embodiment, and coordinate accompanying drawing, describe in detail as follows.
Brief 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 process plate
5：Conformal head-shield
Embodiment
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, the conformal head-shield 5 installed in 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 process plate 4, the global positioning system conformal antenna 1 is wrapped on conformal head-shield 5 and the two is conformal；The survey is high
Radar antenna 2 be located at foremost, global positioning signal process plate 4 be located at rearmost end, height finding radar signal-processing board 3, which is located at, surveys high
Between radar antenna 2, global positioning signal process plate 4；
The global positioning system conformal antenna 1 is used to receive global positioning signal, and global positioning signal process plate 4 is used for
The processing and resolving of location information, the two matching are used, and collectively constitute high dynamic global positioning system；
The height finding radar antenna 2 is used to receive and transmission signal, and height finding radar signal-processing board 3 is used for elevation information
Processing and clearing, the two matching are used, and collectively constitute height finding radar；
The height finding radar signal-processing board 3, global positioning signal process plate 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 arranged in the conformal head-shield 5 in head, forms a highly integrated independent bay section, will detect,
Position, survey high function collection and be integrated.During using the device, rocket projectile head, global positioning system blanket insurance can be installed in
Shape antenna 1 and global positioning signal process plate 4 can in real time position and resolve trajectory message；The launching beam of height finding radar antenna 2
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, time break is sent 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 replaced by into extinguishing chemical dispensing unit,
The rocket projectile is to be converted into long-range fire extinguisher bomb.
It is described above, only it is the preferred embodiment of patent of the present invention, any those skilled in the art, not
Depart from the art of this patent aspects in, according to this patent technical spirit to it is made for any of the above embodiments it is any it is simple modification,
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 arranged 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 transacting
Plate (3), global positioning signal process plate (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) be located at foremost, global positioning signal process plate (4) be located at rearmost end, survey Gao Lei
It is located at up to signal-processing board (3) between height finding radar antenna (2), global positioning signal process plate (4)；
The global positioning system conformal antenna (1) is used to receive global positioning signal, and global positioning signal process plate (4) is used for
The processing and resolving of location information, the two matching are used, and collectively constitute high dynamic global positioning system；
The height finding radar antenna (2) is used to receive and transmission signal, and height finding radar signal-processing board (3) is used for elevation information
Processing and clearing, the two matching are used, and collectively constitute height finding radar；
The height finding radar signal-processing board (3), global positioning signal process plate (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：It is described to 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 true CN107152895A (en) | 2017-09-12 |
| CN107152895B CN107152895B (en) | 2018-08-17 |
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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 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017170A (en) * | 2019-12-30 | 2020-04-17 | 西安智荣机电科技有限公司 | High-efficient built-in antenna glider under water |
| CN111337921A (en) * | 2020-03-13 | 2020-06-26 | 成都金宇防务科技有限公司 | Missile-borne millimeter wave radar height measurement device to ground |
Citations (6)
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|---|---|---|---|---|
| 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 |
| 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 |
| 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 |
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2017
- 2017-06-21 CN CN201710476753.3A patent/CN107152895B/en active Active
Patent Citations (6)
| 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 |
| 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 |
| 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 |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017170A (en) * | 2019-12-30 | 2020-04-17 | 西安智荣机电科技有限公司 | High-efficient built-in antenna glider under water |
| 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 |
| CN111337921A (en) * | 2020-03-13 | 2020-06-26 | 成都金宇防务科技有限公司 | Missile-borne millimeter wave radar height measurement device to ground |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107152895B (en) | 2018-08-17 |
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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 |
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