CN107356154A - A kind of semi-active type missije laser guidance system based on unmanned plane - Google Patents
A kind of semi-active type missije laser guidance system based on unmanned plane Download PDFInfo
- Publication number
- CN107356154A CN107356154A CN201710601947.1A CN201710601947A CN107356154A CN 107356154 A CN107356154 A CN 107356154A CN 201710601947 A CN201710601947 A CN 201710601947A CN 107356154 A CN107356154 A CN 107356154A
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- Prior art keywords
- laser
- unmanned plane
- target
- platform
- aerial vehicle
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/24—Beam riding guidance systems
- F41G7/26—Optical guidance systems
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a kind of semi-active type missije laser guidance system based on unmanned plane, it is related to unmanned plane laser-guided bomb technical field, including unmanned plane body, control station, command centre and MISSILE LAUNCHING and carrying platform, the unmanned plane body is provided with unmanned aerial vehicle platform, the lower section of the unmanned aerial vehicle platform is provided with gondola, the gondola is equipped with laser irradiation device and video camera, the MISSILE LAUNCHING is provided with laser-guided bomb module with carrying platform, the control station and command centre pass through the video camera and MISSILE LAUNCHING of communication link wireless connection unmanned aerial vehicle platform and the laser-guided bomb module of carrying platform, this invention addresses the dangerous problem for needing target and bringing, solves the potential problem for being easily found and bringing when own vol excessive target run overhead irradiation target, it is low to lose cost.
Description
Technical field
The present invention relates to unmanned plane laser-guided bomb technical field, more particularly to a kind of semi-active type based on unmanned plane
Missije laser guidance system.
Background technology
Existing to guide field in semi-active type missije laser, the first is to hold laser irradiation device using special personnel to hide
After the target, irradiate target with laser irradiating machine, distant place base transmitting laser-guided bomb or carry laser-guided bomb or
The aircraft target run overhead of bomb is projected.The laser that laser-guided bomb or bomb reflect according to the target received is believed
Number carry out adjustment position, finally concentrate target；Second is aircraft target run overhead, and self-contained laser irradiating machine irradiates target
Launch laser-guided bomb or bomb simultaneously, but have the following disadvantages：
The first, it is all very tight to generally require the warning of the target smashed at one's side, and special personnel wants accurately irradiation
To target, it is necessary to what must be leaned on is close, and for a long time irradiation target until guided missile or bomb receive signal and finally hit
Target.Special personnel is in high-risk environment in this process, is easy to be found by other side, to itself bringing danger, and mesh
Mark transfer is guarded against, and is unfavorable for the completion of task.
Second：Due to needing aircraft itself to irradiate target, therefore obtain and rest on target overhead for a long time, fly plus fighting
The general own vol of machine is very big, by target side find probability it is very big, target side can be caused to have defence, to itself safety and
The completion of task brings very big hidden danger.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of semi-active type missije laser guidance system based on unmanned plane
System, to solve caused above-mentioned multinomial defect in the prior art.
To achieve the above object, the present invention provides following technical scheme：A kind of semi-active type guided missile based on unmanned plane
Laser guidance system, including unmanned plane body, control station, command centre and MISSILE LAUNCHING and carrying platform, the unmanned plane
Body is provided with unmanned aerial vehicle platform, and the lower section of the unmanned aerial vehicle platform is provided with gondola, and the gondola is equipped with laser irradiation device and takes the photograph
Camera, the MISSILE LAUNCHING and carrying platform, which are provided with laser-guided bomb module, the control station and command centre and passed through, to be led to
Interrogate the video camera and MISSILE LAUNCHING and the laser-guided bomb module of carrying platform of link wireless connection unmanned aerial vehicle platform.
Preferably, the laser irradiation device and video camera are hung in the streamlined nacelle in the lower section of unmanned aerial vehicle platform by gondola
Section.
Compared with prior art, it is using the beneficial effect of above technical scheme：Special personnel is solved in order to allow laser to shine
Penetrate machine and accurately irradiate target, it is necessary to the dangerous problem pressed close to target and brought；Solves to carry laser-guided bomb aircraft because of itself
The potential problem for being easily found and bringing during target is irradiated in the excessive target run overhead of volume, passes through the guidance system, guided missile
It can be launched in the stand-off missle of target side, the video camera carried after target by remote control unmanned plane accurately irradiates
Target, only have MAV to press close to target in whole task process, even if being hit back after target detection, at most can only
Unmanned plane is smashed, loss cost is low.
Brief description of the drawings
Fig. 1 is the theory diagram of the present invention.
Embodiment
The preferred embodiment that the invention will now be described in detail with reference to the accompanying drawings.
Fig. 1 shows the embodiment of the present invention：A kind of semi-active type missije laser guidance system based on unmanned plane,
Including unmanned plane body, control station, command centre and MISSILE LAUNCHING and carrying platform, the unmanned plane body is provided with nobody
Machine platform, the lower section of the unmanned aerial vehicle platform are provided with gondola, and the gondola is equipped with laser irradiation device and video camera, the guided missile hair
Penetrate with carrying platform be provided with laser-guided bomb module, the control station and command centre by communication link wireless connection without
The video camera and MISSILE LAUNCHING of people's machine platform and the laser-guided bomb module of carrying platform.
Command centre, it is commander's maincenter of whole system, is in network center, information centre, information distribution center, communication
The heart, control centre, the function of Surveillance center are collected.
Control station, control flight control, mission payload control, data link control and the traffic guidance of unmanned plane.
Unmanned aerial vehicle platform, laser irradiation device and video camera are carried, be the flying platform that carries out Mission Operations, can hover.
Gondola, it is equipped with laser irradiation device and video camera and hang the streamlined nacelle section below unmanned plane.
Video camera, unmanned plane surrounding enviroment are recorded a video and taken pictures and are transferred in the control station and commander of earth station
The heart.
Laser irradiation device is mainly used in irradiating target.
MISSILE LAUNCHING and carrying platform, transport the platform of laser-guided bomb module.
Laser-guided bomb module, inside have laser seeker and reflected to receive after laser irradiating machine irradiates target
Laser beam out, then electric signal is formed through light-to-current inversion, missile control module is inputted, controls guided missile control surface deflection, smart missiles
Target.
Semi-active type missije laser guidance system based on above-mentioned, of the invention unmanned plane, utilizes UAV flight's laser
Irradiate the laser irradiating machine to substitute special personnel or large-scale operational aircraft is held and irradiate target, solve problems with：
1st, because special personnel will press close to dangerous problem caused by target for accurate irradiation target.Special personnel passes through
Unmanned plane is manipulated, target can be irradiated outside from target overlength distance, so as to allow itself away from danger.
2nd, due to unmanned plane small volume, can hover, be not easy to be found by people at the same can be stable irradiation target without inclined
From.
3rd, can be launched by the guidance system, guided missile in the stand-off missle of target side, by remotely grasping after target
The video camera that control unmanned plane carries accurately irradiates target, only has unmanned plane to press close to target in whole task process, even if by
Hit back after target detection, can only at most smash unmanned plane, loss cost is low.
Above-described is only the preferred embodiment of the present invention, it is noted that for one of ordinary skill in the art
For, without departing from the concept of the premise of the invention, various modifications and improvements can be made, these belong to the present invention
Protection domain.
Claims (2)
1. a kind of semi-active type missije laser guidance system based on unmanned plane, including unmanned plane body, control station, command centre
And MISSILE LAUNCHING and carrying platform, it is characterised in that：The unmanned plane body is provided with unmanned aerial vehicle platform, and the unmanned plane is put down
The lower section of platform is provided with gondola, and the gondola is equipped with laser irradiation device and video camera, and the MISSILE LAUNCHING is provided with carrying platform
Laser-guided bomb module, the control station and command centre by the video camera of communication link wireless connection unmanned aerial vehicle platform and
The laser-guided bomb module of MISSILE LAUNCHING and carrying platform.
A kind of 2. semi-active type missije laser guidance system based on unmanned plane according to claim 1, it is characterised in that：
The laser irradiation device and video camera are hung in the streamlined nacelle section in the lower section of unmanned aerial vehicle platform by gondola.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710601947.1A CN107356154A (en) | 2017-07-21 | 2017-07-21 | A kind of semi-active type missije laser guidance system based on unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710601947.1A CN107356154A (en) | 2017-07-21 | 2017-07-21 | A kind of semi-active type missije laser guidance system based on unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107356154A true CN107356154A (en) | 2017-11-17 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710601947.1A Pending CN107356154A (en) | 2017-07-21 | 2017-07-21 | A kind of semi-active type missije laser guidance system based on unmanned plane |
Country Status (1)
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| CN (1) | CN107356154A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108548452A (en) * | 2018-04-28 | 2018-09-18 | 施新红 | A kind of novel optical transmission equipment |
| CN109885101A (en) * | 2019-01-04 | 2019-06-14 | 北京测威科技有限公司 | A kind of method and system using unmanned vehicle simulated missile terminal guidance |
| CN110988819A (en) * | 2019-12-30 | 2020-04-10 | 中国人民解放军火箭军工程大学 | Laser decoy jamming device trapping effect evaluation system based on unmanned aerial vehicle formation |
| CN111044989A (en) * | 2019-12-30 | 2020-04-21 | 中国人民解放军火箭军工程大学 | Laser decoy interference equipment lures partial effect outfield evaluation system |
| CN111272015A (en) * | 2020-03-23 | 2020-06-12 | 西安深瞳智控技术有限公司 | System and method for evaluating dynamic tracking performance of laser seeker |
| CN112212744A (en) * | 2020-10-10 | 2021-01-12 | 江西洪都航空工业集团有限责任公司 | Method for sending laser-guided missile irradiation instruction based on Beidou short message |
| CN113424013A (en) * | 2019-02-12 | 2021-09-21 | Bae系统信息和电子系统集成有限公司 | Projectile guidance system |
| CN113671981A (en) * | 2020-05-14 | 2021-11-19 | 北京理工大学 | Remote laser guidance aircraft control system and control method thereof |
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| EP2687809A1 (en) * | 2012-07-18 | 2014-01-22 | Thales Holdings UK Plc | Missile Guidance |
| CN103983145A (en) * | 2014-05-21 | 2014-08-13 | 中国航天空气动力技术研究院 | Method for capturing object by using last pulse policy of laser seeker of unmanned aerial vehicle |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108548452A (en) * | 2018-04-28 | 2018-09-18 | 施新红 | A kind of novel optical transmission equipment |
| CN109885101A (en) * | 2019-01-04 | 2019-06-14 | 北京测威科技有限公司 | A kind of method and system using unmanned vehicle simulated missile terminal guidance |
| CN109885101B (en) * | 2019-01-04 | 2022-02-22 | 北京测威科技有限公司 | Method and system for simulating missile terminal guidance by using unmanned aerial vehicle |
| CN113424013A (en) * | 2019-02-12 | 2021-09-21 | Bae系统信息和电子系统集成有限公司 | Projectile guidance system |
| CN110988819A (en) * | 2019-12-30 | 2020-04-10 | 中国人民解放军火箭军工程大学 | Laser decoy jamming device trapping effect evaluation system based on unmanned aerial vehicle formation |
| CN111044989A (en) * | 2019-12-30 | 2020-04-21 | 中国人民解放军火箭军工程大学 | Laser decoy interference equipment lures partial effect outfield evaluation system |
| CN111044989B (en) * | 2019-12-30 | 2020-10-30 | 中国人民解放军火箭军工程大学 | Laser decoy interference equipment lures partial effect outfield evaluation system |
| CN110988819B (en) * | 2019-12-30 | 2020-12-08 | 中国人民解放军火箭军工程大学 | Laser decoy jamming device trapping effect evaluation system based on unmanned aerial vehicle formation |
| CN111272015A (en) * | 2020-03-23 | 2020-06-12 | 西安深瞳智控技术有限公司 | System and method for evaluating dynamic tracking performance of laser seeker |
| CN113671981A (en) * | 2020-05-14 | 2021-11-19 | 北京理工大学 | Remote laser guidance aircraft control system and control method thereof |
| CN112212744A (en) * | 2020-10-10 | 2021-01-12 | 江西洪都航空工业集团有限责任公司 | Method for sending laser-guided missile irradiation instruction based on Beidou short message |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171117 |
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| RJ01 | Rejection of invention patent application after publication |