CN206891273U - Unmanned plane breaks through system - Google Patents
Unmanned plane breaks through system Download PDFInfo
- Publication number
- CN206891273U CN206891273U CN201720703801.3U CN201720703801U CN206891273U CN 206891273 U CN206891273 U CN 206891273U CN 201720703801 U CN201720703801 U CN 201720703801U CN 206891273 U CN206891273 U CN 206891273U
- Authority
- CN
- China
- Prior art keywords
- shafting structure
- target
- laser
- vertical
- unit
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B23/00—Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Telescopes (AREA)
- Optical Radar Systems And Details Thereof (AREA)
Abstract
Unmanned plane counter system is the utility model is related to, the system includes transmitting includes common optical pathways optical module, laser cell and imaging unit, the laser cell, for launching the laser beam to strike target with receiving the optical system of common optical pathways, the optical system；The common optical pathways optical module, for the radiating laser beams to be gone out, or the light receiver from target is come in；The imaging unit, for by the image formation by rays of the target received.The utility model is using receiving light path and transmitting light path sharing method, after target tracked locking, launch laser to it along same paths to hit, it can ensure that target is met, the system is broken through for unmanned plane, it can not only hit the mark, and the third party of an innocent person will not be damaged, also proper communication not interfered.
Description
Technical field
Unmanned plane counter field is the utility model is related to, it is particularly a kind of to be used to prevent unmanned plane from causing the nothing of adverse consequences
It is man-machine to snipe system.
Background technology
Unmanned plane is push-button aircraft, refers to utilize radio robot or the presetting apparatus provided for oneself manipulation
Not man-carrying aircraft.The advantage such as stand high, look far because unmanned plane has, be adaptable, can arrange in pairs or groups different appoint
Business load, is widely used in the fields such as aeroplane photography, the monitoring of ring mirror, the monitoring of side mirror, disaster search and rescue, geological mapping.
But the management and control of unmanned plane does not keep up with the paces of technology development, and flight is to national public safety, flight safety in violation of rules and regulations
Even air defence constitutes a threat to safely.For example taken on the sly using unmanned plane and steal information, carry the thing to endanger public security
Matter, for another example, there is the black winged event of unmanned plane in many airports recently, cause a large amount of flights to be delayed, generate heavy losses.
The system of unmanned plane counter at present, generally using means of electromagnetic waves, to disturb the flight of unmanned plane, but such a mode
Also have impact on simultaneously by the normal communication in management and control region.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane counter system.
In order to realize above-mentioned purpose of utility model, the utility model embodiment provides following technical scheme：
A kind of unmanned plane breaks through system, including transmitting and the optical system of reception common optical pathways, the optical system include
Common optical pathways optical module, laser cell and imaging unit, wherein,
The laser cell, for launching the laser beam to strike target；
The common optical pathways optical module, for the radiating laser beams to be gone out, or the light from target is connect
Take in；
The imaging unit, for by the image formation by rays of the target received.
According to the utility model embodiment, the common optical pathways optical module includes telescope lens unit, relaying microscope group
Unit and spectrophotometric unit, wherein,
The telescope lens unit, the radiating laser beams for the laser cell to be launched are gone out, or will be come from
The light receiver of target is come in；
The relaying lens unit, for changing the transmission of the light from target or the laser beam of laser cell transmitting
Direction, to cause the laser beam by spectrophotometric unit transmission to enter telescope lens unit, and telescope lens unit receives
The light for the target come in enters spectrophotometric unit；Relaying lens unit includes at least one tracking executive component, for real-time
Change beam direction to track target；
The spectrophotometric unit, for the laser beam of the light from target and laser cell transmitting to be separated, so that
Obtaining the laser beam of laser cell transmitting can transmit to relaying lens unit, and the light of the target received and can enter
Imaging unit.
The space layout of system is easy in the setting of relaying lens unit, and tracking executive component can change orientation in real time and bow
Position is faced upward to adapt to the change in location of target, effective guarantee target is locked by real-time tracking.
In the scheme further optimized, telescope lens unit includes primary mirror and secondary mirror, and the secondary mirror is where primary mirror
The projection of plane and primary mirror are misaligned.The outgoing that secondary mirror can be avoided to hinder primary mirror light is so set, that is, avoids secondary mirror from weakening
For the laser beam to strike target, ensure that target is effectively destroyed.
In further perfect scheme, unmanned plane counter system also includes frame and drive device；The frame is used for
Supporting forms the part or all of unit of the optical system, and under the driving of the drive device, drives described in composition
The part or all of unit of optical system is rotated around trunnion axis and/or vertical axes rotation.
According to the utility model embodiment, in an arrangement, the frame includes horizontal shafting structure and vertical shafting
Structure, the telescope lens unit are arranged in lens barrel, and lens barrel is connected with horizontal shafting structure, and can be rotated around trunnion axis；
The vertical shafting structure is connected with horizontal shafting structure, and positioned at the side of the lens barrel, and horizontal shafting structure can be driven
Rotated with lens barrel around vertical axes；Transmitting beam between secondary mirror and spectroscope is located at trunnion axis and vertical axes.
According to the utility model embodiment, in another scheme, the frame includes horizontal shafting structure and vertical axes
Architecture, the telescope lens unit are arranged in lens barrel, and lens barrel is connected with horizontal shafting structure, and can be revolved around trunnion axis
Turn；The vertical shafting structure is connected with horizontal shafting structure, and the center of gravity of vertical shafting structure and the center of gravity position of the lens barrel
In on same vertical curve, vertical shafting structure can drive horizontal shafting structure and lens barrel to be rotated around vertical axes；Secondary mirror and spectroscope
Between transmitting beam be located at trunnion axis and vertical axes.
According to the utility model embodiment, in another scheme, the frame includes horizontal shafting structure and vertical axes
Architecture, the optical system are arranged in casing, and casing is connected with horizontal shafting structure, and can be rotated around trunnion axis；It is described
Vertical shafting structure is connected with horizontal shafting structure, and vertical shafting structure can drive horizontal shafting structure and casing to be revolved around vertical axes
Turn.
Compared with prior art, the beneficial effects of the utility model：The utility model is launched with receiving common optical pathways mode,
I.e. target following detection light path is identical with laser hits light path, after target tracked locking, it is launched along same paths sharp
Light is hit, and can ensure that target is met, and will not damage the third party of an innocent person, also normal communication will not be caused to do
Disturb.In addition, by way of hitting the mark, the expansion of terrified consequence can be effectively prevented from.
Brief description of the drawings
, below will be to required use in embodiment in order to illustrate more clearly of the technical scheme of the utility model embodiment
Accompanying drawing be briefly described, it will be appreciated that the following drawings illustrate only some embodiments of the present utility model, therefore should not be by
Regard the restriction to scope as, for those of ordinary skill in the art, on the premise of not paying creative work, may be used also
To obtain other related accompanying drawings according to these accompanying drawings.
Fig. 1 is the structural representation frame of optical system of the transmitting described in the utility model embodiment with receiving common optical pathways
Figure.
Fig. 2 is the structural representation that unmanned plane breaks through system described in the utility model embodiment 1.
Fig. 3 is that target following detects light path schematic diagram in unmanned plane counter system described in the utility model embodiment 1.
Fig. 4 is Laser emission light path schematic diagram described in the utility model embodiment 1.
Fig. 5 is the structural representation that unmanned plane breaks through system described in the utility model embodiment 2.
Fig. 6 is that target following detects light path schematic diagram in unmanned plane counter system described in the utility model embodiment 2.
Fig. 7 is Laser emission light path schematic diagram described in the utility model embodiment 2.
Fig. 8 is the structural representation that unmanned plane breaks through system described in the utility model embodiment 3.
Fig. 9 is that target following detects light path schematic diagram in unmanned plane counter system described in the utility model embodiment 3.
Figure 10 is Laser emission light path schematic diagram described in the utility model embodiment 3.
Figure 11 is the structural representation that unmanned plane breaks through system described in the utility model embodiment 4.
Figure 12 is that target following detects light path schematic diagram in unmanned plane counter system described in the utility model embodiment 4.
Figure 13 is Laser emission light path schematic diagram described in the utility model embodiment 4.
Description of symbols in figure
10- laser cells；20- imaging units；30- common optical pathways optical modules；31- telescope lens units；32- is relayed
Lens unit；33- spectrophotometric units；40- lens barrels；50- trunnion axis；60- vertical axes；The vertical shafting structures of 70-；80- base frame casings；
90- casings；311- primary mirrors；312- secondary mirrors；313- plane mirrors；320- tracks executive component；321~325- speculums.
Embodiment
Below in conjunction with accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out clear
Chu, it is fully described by, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole realities
Apply example.The component of the utility model embodiment being generally described and illustrated herein in the accompanying drawings can be come with a variety of configurations
Arrangement and design.Therefore, the detailed description of the embodiment of the present utility model to providing in the accompanying drawings is not intended to limit below
Claimed the scope of the utility model, but it is merely representative of selected embodiment of the present utility model.Based on the utility model
Embodiment, the every other embodiment that those skilled in the art are obtained on the premise of creative work is not made, all
Belong to the scope of the utility model protection.
Referring to Fig. 1, a kind of optical system launched and receive common optical pathways is provided in the utility model embodiment, should
Optical system includes common optical pathways optical module 30, laser cell 10 and imaging unit 20, wherein,
Laser cell 10, for launching the laser beam to strike target；
Common optical pathways optical module 30, come in for radiating laser beams to be gone out, or by the light receiver from target；
Imaging unit 20, for by the image formation by rays of the target received.
In above-mentioned optical system, the shared path optics component 30 of light of target receives, and is transferred to imaging unit 20, warp
Imaging unit 20 is imaged, and realizes tracking and locking to target；After strike instruction is received, laser cell 10, which is launched, to be used for
The laser beam of the locked target of strike, the laser beam are launched along with receiving target light identical light path, hit the mark, by
It is that the same optical path being locked along target is launched in laser beam, therefore can ensures that target is met, avoids
The third party of an innocent person is caused to damage, in addition, by laser hits mode, existing electromagnetic wave is avoided and hits mode to airport just
Interference caused by normal open is interrogated.
As a kind of citing of embodiment, the common optical pathways optical module 30 include telescope lens unit 31,
Relay lens unit 32 and spectrophotometric unit 33.Wherein,
Telescope lens unit 31, the radiating laser beams for laser cell 10 to be launched are gone out, or will come from target
Light receiver come in.Telescope lens unit 31 can include primary mirror 311 and secondary mirror 312, as a kind of preferably embodiment party
Formula, secondary mirror 312 is misaligned (such as shown in Fig. 2-13) with primary mirror 311 in the projection of the place plane of primary mirror 311, can so ensure
Secondary mirror 312 does not hinder the outgoing and reception of light in primary mirror 311 so that laser beam can all hit the mark, and ensure target quilt
Beating Strength.
Lens unit 32 is relayed, one or more speculums can be included, for changing the light from target or swashing
The transmission direction for the laser beam that light unit 10 is launched, to adapt to different space layouts so that transmitted by spectrophotometric unit 33
Laser beam enters telescope lens unit 31, and to enter light splitting single for the light of target that receives of telescope lens unit 31
Member 33.Relaying lens unit 32 includes at least one tracking executive component 320, changes beam direction for real-time to track mesh
Mark, the tracking executive component 320 can be a speculum with planar scan function, or two have respectively
The speculum of one-dimensional scanning function, two speculums, which coordinate, can realize two-dimensional scan function, when target is subjected to displacement, tracking
Identical displacement occurs therewith for executive component 320, realizes the real-time tracking locking to target.
Spectrophotometric unit 33, the laser beam for the light from target and laser cell 10 to be launched are separated, so that
The laser beam launched of laser cell 10 can be transmitted to relaying lens unit 32, and the light of the target received can be with
Into imaging unit 20.For example, spectrophotometric unit 33 includes a spectroscope, by the way of spectrum, make laser cell 10
The laser beam of transmitting be split mirror reflection, then by relaying lens unit 32 and telescope lens unit 31 launch, make mesh
After mark tracking light beam passes through spectroscope with transmission mode, into imaging unit 20.
Embodiment 1
Fig. 1-4 are referred to, a kind of unmanned plane counter system is provided in the present embodiment, the system is included shown in Fig. 1
Optical system, and frame, drive device (not shown), wherein, frame is used to support the portion for forming the optical system
Point or whole units, and under the driving of drive device, drive part or complete of its composition optical system supported
Portion's unit rotates around trunnion axis 50 and/or vertical axes 60 rotate.
In the present embodiment, the relaying lens unit 32 in the optical system include three speculums (321~323) and
One tracking executive component 320 with two-dimensional scan function, the transmission ray between secondary mirror 312 and spectrophotometric unit 33 is through excessive
Vertical incidence to secondary mirror 312 or spectrophotometric unit 33, primary mirror 311, secondary mirror 312, one of speculum (323) is set after secondary reflection
In in lens barrel 40, two other speculum in laser cell 10, imaging unit 20, spectrophotometric unit 33 and relaying lens unit 32
(321,322) it is integrated in base frame casing 80.
The frame includes horizontal shafting structure and vertical shafting structure 70, in the present embodiment, lens barrel 40 and trunnion axis
Architecture connects, and can be rotated around trunnion axis 50；Vertical shafting structure 70 is connected with horizontal shafting structure, and positioned at lens barrel 40
Side, and horizontal shafting structure and lens barrel 40 can be driven to be rotated around vertical axes 60.Transmitting beam between secondary mirror 312 and spectroscope
Positioned at trunnion axis 50 (also referred to as horizontal axis, horizontal axis of rotation) and vertical axes 60 (also referred to as vertical axis, vertical rotation
Shaft axis), as in Figure 2-4, when realizing, the speculum (322) relayed in lens unit is arranged at vertical shafting structure
In 70 and in vertical axes 60, and the speculum (322) is respectively positioned on another speculum (323) in relaying lens unit
On trunnion axis 50, to ensure the transmission direction for not changing light path during frame rotates with moving lens barrel 40, target quilt is realized
Real-time lock.
In unmanned plane counter system described in the present embodiment, the transmission path such as Fig. 4 for the laser beam that laser cell 10 is launched
Shown, target following detection light path is as shown in Figure 3.
In the present embodiment, vertical shafting structure 70 is arranged to the side of lens barrel 40, it is possible to reduce relaying lens unit 32
The use number of middle speculum., can be in vertical shafting structure in order to keep the stability of total system in frame rotary course
70 opposite side sets bascule.
Embodiment 2
Fig. 5-7 are referred to, the unmanned plane counter system provided in the present embodiment, compared with Example 1, difference exists
It is located in, the center of gravity of vertical shafting structure 70 with the center of gravity of lens barrel 40 on same vertical curve, whole frame is U-shape structure, lens barrel
40 in the U-shaped groove of U-shaped support, based on the setting of U-shaped rack construction, is rotated horizontally in frame band moving lens barrel 40
And/or during vertical rotation, good balance can be kept, still, now then need more (relative to embodiment
Described in 1 for system) relay mirror (321~325) realize that the transmitting beam between secondary mirror 312 and spectroscope is located at
Trunnion axis 50 and vertical axes 60, as illustrated in figs. 5-7.In unmanned plane counter system described in the present embodiment, laser cell 10 is launched
Laser beam transmission path as shown in fig. 7, target following detection light path it is as shown in Figure 6.
Embodiment 3
Fig. 8-10 are referred to, the unmanned plane counter system provided in the present embodiment, compared with Example 2, difference exists
In, form optical system all units (including telescope lens unit 31, relaying lens unit 32, spectrophotometric unit 33, laser
Unit 10, imaging unit 20) it is integrated in a casing 90, frame is U-shaped head frame, and the casing 90 is positioned over U-shaped head
In frame, casing 90 is connected with horizontal shafting structure, and can be rotated around trunnion axis 50, and vertical shafting structure 70 can drive trunnion axis
Architecture and casing 90 rotate around vertical axes 60.In order to keep the stability of total system in frame rotary course, can set
It is located at for the center of gravity of vertical shafting structure 70 and the center of gravity of casing 90 on same vertical curve.
Because whole optical system is all integrated in casing 90, all units of optical system produce position of orientation simultaneously
And/or the change of pitch position, i.e., change between each other without relative position, therefore, between secondary mirror 312 and spectrophotometric unit 33
For transmitting beam without being necessarily limited on trunnion axis 50 and vertical axes 60, the number for relaying speculum in lens unit 32 can also
It is relatively fewer, as seen in figs. 8-10, it is only necessary to which a speculum (321) and a tracking executive component 320 can be achieved.
Can be in embodiment at another, laser cell 10 can include laser and optical fiber, can be placed in laser
Outside casing 90, the laser beam of laser transmitting is delivered to spectrophotometric unit 33 by optical fiber.
Embodiment 4
Figure 11-13 are referred to, the unmanned plane counter system provided in the present embodiment, compared with Example 3, difference exists
In telescope lens unit 31 also includes plane mirror 313, for realizing transmission ray between primary mirror 311 and secondary mirror 312
Turn back, reduce the length between primary mirror 311 and secondary mirror 312, and then reduce the size of casing 90.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art can readily occur in change in the technical scope that the utility model discloses
Or replace, it should all cover within the scope of protection of the utility model.
Claims (10)
1. a kind of unmanned plane breaks through system, it is characterised in that including launching the optical system with receiving common optical pathways, the optics
System includes common optical pathways optical module, laser cell and imaging unit, wherein,
The laser cell, for launching the laser beam to strike target；
The common optical pathways optical module, for the radiating laser beams to be gone out, or the light receiver from target is entered
Come；
The imaging unit, for by the image formation by rays of the target received.
2. unmanned plane according to claim 1 breaks through system, it is characterised in that the common optical pathways optical module includes hoping
Remote mirror lens unit, relaying lens unit and spectrophotometric unit, wherein,
The telescope lens unit, the radiating laser beams for the laser cell to be launched are gone out, or will come from target
Light receiver come in；
The relaying lens unit, for changing the transmission side of the light from target or the laser beam of laser cell transmitting
To, to cause the laser beam by spectrophotometric unit transmission to enter telescope lens unit, and telescope lens unit receive into
The light for the target come enters spectrophotometric unit；Relaying lens unit includes at least one tracking executive component, for changing in real time
Become beam direction to track target；
The spectrophotometric unit, for the laser beam of the light from target and laser cell transmitting to be separated, to swash
The laser beam of light unit transmitting, which can be transmitted to relaying lens unit, and the light of the target received, can enter imaging
Unit.
3. unmanned plane according to claim 2 breaks through system, it is characterised in that the telescope lens unit includes primary mirror
And secondary mirror, the secondary mirror projection of plane and primary mirror where primary mirror are misaligned.
4. system is broken through according to any described unmanned planes of claim 2-3, it is characterised in that also including frame and driving dress
Put；The frame is used to support the part or all of unit for forming the optical system, and the driving in the drive device
Under, the part or all of unit of the drive composition optical system is rotated around trunnion axis and/or vertical axes rotation.
5. unmanned plane according to claim 4 breaks through system, it is characterised in that the frame include horizontal shafting structure and
Vertical shafting structure, the telescope lens unit are arranged in lens barrel, and lens barrel is connected with horizontal shafting structure, and can be around level
Axle rotates；The vertical shafting structure is connected with horizontal shafting structure, and positioned at the side of the lens barrel, and trunnion axis can be driven
Architecture and lens barrel rotate around vertical axes；Transmitting beam between secondary mirror and spectroscope is located at trunnion axis and vertical axes.
6. unmanned plane according to claim 4 breaks through system, it is characterised in that the frame include horizontal shafting structure and
Vertical shafting structure, the telescope lens unit are arranged in lens barrel, and lens barrel is connected with horizontal shafting structure, and can be around level
Axle rotates；The vertical shafting structure is connected with horizontal shafting structure, and the center of gravity and the weight of the lens barrel of vertical shafting structure
The heart is located on same vertical curve, and vertical shafting structure can drive horizontal shafting structure and lens barrel to be rotated around vertical axes；Secondary mirror is with dividing
Transmitting beam between light microscopic is located at trunnion axis and vertical axes.
7. unmanned plane according to claim 4 breaks through system, it is characterised in that the frame include horizontal shafting structure and
Vertical shafting structure, the optical system are arranged in casing, and casing is connected with horizontal shafting structure, and can be revolved around trunnion axis
Turn；The vertical shafting structure is connected with horizontal shafting structure, vertical shafting structure can drive horizontal shafting structure and casing around
Vertical axes rotate.
8. unmanned plane according to claim 7 breaks through system, it is characterised in that the center of gravity of vertical shafting structure and the case
The center of gravity of body is located on same vertical curve.
9. unmanned plane according to claim 7 breaks through system, it is characterised in that the telescope lens unit also includes flat
Face speculum, for realizing turning back for transmission ray between primary mirror and secondary mirror.
10. unmanned plane according to claim 7 breaks through system, it is characterised in that laser cell includes laser and optical fiber,
The laser is located at outside the casing, and the laser beam of laser transmitting is delivered to spectrophotometric unit by optical fiber.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710309088 | 2017-05-04 | ||
| CN2017103090889 | 2017-05-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206891273U true CN206891273U (en) | 2018-01-16 |
Family
ID=60332413
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720703801.3U Active CN206891273U (en) | 2017-05-04 | 2017-06-16 | Unmanned plane breaks through system |
| CN201710457829.8A Active CN107388900B (en) | 2017-05-04 | 2017-06-16 | Unmanned aerial vehicle reaction system |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710457829.8A Active CN107388900B (en) | 2017-05-04 | 2017-06-16 | Unmanned aerial vehicle reaction system |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN206891273U (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109539888A (en) * | 2018-12-17 | 2019-03-29 | 科立讯通信股份有限公司 | Anti- unmanned plane supervisory device |
| CN110345818A (en) * | 2019-07-24 | 2019-10-18 | 合肥正阳光电科技有限责任公司 | 360 degree of one kind is without dead angle short-range laser system of defense |
| CN111854534B (en) * | 2020-08-07 | 2023-03-03 | 广东电网有限责任公司 | Unmanned aerial vehicle drives device |
| CN112648887B (en) * | 2020-12-16 | 2022-08-16 | 航天科工微电子系统研究院有限公司 | Photoelectric tracking and control method based on common-frame radar composite detection |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2356317Y (en) * | 1999-01-08 | 1999-12-29 | 陆建红 | Aimed semiconductor pulse laser distance measurer |
| CN100487433C (en) * | 2005-06-07 | 2009-05-13 | 中国科学院安徽光学精密机械研究所 | Vehicular pollution-motoring lidar device based on Raman light source |
| US7742151B2 (en) * | 2005-07-08 | 2010-06-22 | Lockheed Martin Corporation | Laser-based system with LADAR and SAL capabilities |
| CN100587389C (en) * | 2006-08-17 | 2010-02-03 | 中国科学院光电技术研究所 | Photoelectric telescope with high-acuity imaging and luminosity measurement functions |
| CN101963665B (en) * | 2010-08-23 | 2013-11-06 | 西安理工大学 | Laser radar geometric overlap factor automatic regulation method |
| CN106134466B (en) * | 2011-12-30 | 2015-02-25 | 中国兵器装备研究院 | A kind of laser beam directional transmitter from axle |
| CN103197306A (en) * | 2013-04-18 | 2013-07-10 | 中国科学院光电技术研究所 | Full-aperture coaxial laser transmitting and echo receiving system |
| CN104155747B (en) * | 2014-07-29 | 2016-12-07 | 中国科学院长春光学精密机械与物理研究所 | Sharp combiner space junk scavenging system based on the many telescopic manner of separate type |
| CN106483529A (en) * | 2016-09-30 | 2017-03-08 | 深圳市镭神智能系统有限公司 | A kind of optical system |
-
2017
- 2017-06-16 CN CN201720703801.3U patent/CN206891273U/en active Active
- 2017-06-16 CN CN201710457829.8A patent/CN107388900B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN107388900B (en) | 2023-06-16 |
| CN107388900A (en) | 2017-11-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206891273U (en) | Unmanned plane breaks through system | |
| DK2527865T3 (en) | System, device and method of protecting aircraft against incoming missiles and threats | |
| WO2023040257A1 (en) | Communication and remote sensing integrated satellite system | |
| DE602005001624T2 (en) | AIRCRAFT ANTI-MISSILE SYSTEM PROTECTION | |
| EP1556929B1 (en) | Phase conjugate relay mirror apparatus for high energy laser system and method | |
| CN103792652B (en) | Zigzag type optical system in conjunction with active/passive detection | |
| CN104570146B (en) | space debris detection imaging and communication system | |
| CN109787686A (en) | A kind of satellite optical communication terminal on-orbit calibration and transmitting-receiving coaxiality correcting device and method | |
| CN107515391A (en) | Full frequency band unmanned plane signal accurately identifies, laterally with alignment system and method | |
| WO2004109323A2 (en) | Fiber laser based directional infrared countermeasure (dircm) system | |
| CN107514936A (en) | A kind of short-range laser system of defense | |
| CN108919289A (en) | Laser relay redirection energy transmission device for unmanned aerial vehicle | |
| Fischer et al. | Development, integration and test of a transportable adaptive optical ground station | |
| CN107422321A (en) | Microwave stares relevance imaging earth observation method | |
| Smith et al. | Trends in electro-optical electronic warfare | |
| CN206960792U (en) | Laser beam expander and unmanned plane laser snipe system | |
| CN107065165A (en) | Lens cone for telescope, telescope and unmanned plane laser snipe system | |
| KR20130009893A (en) | Auto-docking system for complex unmanned aeriel vehicle | |
| CN112577694A (en) | Infrared pneumatic optical distortion wind tunnel test system | |
| CN207439271U (en) | A kind of short-range laser system of defense | |
| Ji et al. | Application and development trend of laser technology in military field | |
| CN207051580U (en) | Lens cone for telescope, telescope and unmanned plane laser snipe system | |
| CN206891272U (en) | Window device and unmanned plane laser for laser transmitting telescope snipe system | |
| CN201788022U (en) | Full-automatic driving/driven type infrared early warning tracking guidance system | |
| US20240060748A1 (en) | Omnidirectional optronic system having two rotation axes |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |